Garmin | G1000: Cessna Corvalis/Corvalis TT | Garmin G1000: Cessna Corvalis/Corvalis TT G1000 Pilot's Guide for the Cessna Corvalis/Corvalis TT

Garmin G1000: Cessna Corvalis/Corvalis TT G1000 Pilot's Guide for the Cessna Corvalis/Corvalis TT
G1000
®
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099
www.garmin.com
Cessna
Corvalis/Corvalis TT
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251
®
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138
G1000 Pilot’s Guide
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
190-00552-05
Revision A
Integrated Flight Deck
Pilot’s Guide
SYSTEM OVERVIEW
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
AUDIO PANEL & CNS
FLIGHT MANAGEMENT
HAZARD AVOIDANCE
AUTOMATIC FLIGHT CONTROL SYSTEM
ADDITIONAL FEATURES
APPENDICES
INDEX
Copyright © 2008-2010, 2012 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0534.18 or later for the Cessna Corvalis/Corvalis TT. Some differences in
operation may be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411Fax 503/364.2138
Garmin (Europe) Ltd., Liberty House, Hounsdown Business Park, Southampton, SO40 9RB, U.K.
Tel: 44/0870.851241
Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please
contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored
in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download
a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for
personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice
and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.
Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH®, FliteCharts®, and SafeTaxi® are trademarks of
Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.
Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc.; Becker® is a registered trademark of
Becker Flugfunkwerk GmbH; NavData® is a registered trademark of Jeppesen, Inc; Stormscope® is a registered trademark of L-3
Communications.
SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc.
AC-U-KWIK® is a registered trademark of Penton Business Media Inc.
AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties,
with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties
of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any
representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any
incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if
AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to
the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual
or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for
incidental or consequential damages so the above limitations or exclusions may not apply to you.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with
respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of
merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or
make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the
maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related
to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions
do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations
or exclusions may not apply to licensee.
August 2012
190-00552-05 Rev. A
Printed in the U.S.A.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
LIMITED WARRANTY
LIMITED WARRANTY
Within the warranty period, Garmin will, at its sole discretion, repair or replace any components that fail in normal use. Such repairs or
replacement will be made at no charge to the customer for parts and/or labor incidental to the direct repair of said product. Garmin may,
at its discretion with prior approval, reimburse an authorized Garmin Service Center for associated labor costs incurred for removal and
replacement of the panel mount product installed in an aircraft. The customer shall be responsible for any transportation or other cost. This
warranty does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product
damage has occurred due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse, water, flood, fire, or
other acts of nature or external causes; (iv) damage caused by service performed by anyone who is not an authorized service provider
of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin. In addition, Garmin
reserves the right to refuse warranty claims against products or services that are obtained and/or used in contravention of the laws of any
country.
THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS,
IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A
PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM
STATE TO STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER
RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not
allow the exclusion of incidental or consequential damages, so the above limitations may not apply in every case.
Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or offer a full
refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF
WARRANTY.
To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating the nearest Service Center, call
Garmin Customer Service at one of the numbers listed below.
Products sold through online auctions are not eligible for warranty coverage or rebates or other special offers from Garmin. Online auction
confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from the original
retailer is required. Garmin will not replace missing components from any package purchased through an online auction.
Garmin International Inc.
1200 East 151st Street, Olathe, Kansas 66062
Telephone:
(913)397-8200
Telephone Toll Free:
(888)606-5482
Facsimile:
(913)397-8282
Facsimile Toll Free:
(800)801-4670
E-mail: orders@garmin.com
avionics@garmin.com
warranty@garmin.com
D
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road, Southampton, SO40
9RB, UK
Telephone:
++44 (0) 870-8501243
Telephone Toll Free:
++44 (0) 0808 238 0000
(option 5)
Facsimile:
++44 (0) 238052004
E-mail: avionics.europe@garmin.com
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
WARNINGS, CAUTIONS, AND NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance
feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance
and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The
terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from
third party sources. Garmin is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be
relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current
aeronautical charts for appropriate minimum clearance altitudes.
WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated
regularly in order to ensure that the information remains current. Pilots using any outdated database do so
entirely at their own risk.
WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data
is intended only to supplement other approved navigation data sources and should be considered as an aid
to enhance situational awareness.
WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic.
Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting
traffic.
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous
weather. Information contained within data link weather products may not accurately depict current
weather conditions.
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be significantly older than the indicated weather product age.
WARNING: The Garmin G1000, as installed in the Cessna Corvalis/Corvalis TT aircraft, has a very high
degree of functional integrity. However, the pilot must recognize that providing monitoring and/or selftest capability for all conceivable system failures is not practical. Although unlikely, it may be possible for
erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility
of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated
information available in the cockpit.
WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
E
WARNINGS, CAUTIONS, AND NOTES
WARNING: The United States government operates the Global Positioning System and is solely responsible
for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy
and performance of all GPS equipment. Portions of the Garmin G1000 use GPS as a precision electronic
NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be
misused or misinterpreted and, therefore, become unsafe.
WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000
Pilot’s Guide documentation and the aircraft manufacturer’s Airplane Flight Manual (AFM). Thoroughly
practice basic operation prior to actual use. During flight operations, carefully compare indications from the
G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings,
charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.
WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of
according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/
aboutGarmin/environment/disposal.jsp.
WARNING: Because of variation in the earth’s magnetic field, operating the system within the following
areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all
longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude
75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W.
(Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia).
South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New
Zealand).
WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a
system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that
may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned
in error as displayed.
CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very
sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE
ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an
eyeglass lens cleaner that is specified as safe for anti-reflective coatings.
CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by
an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty
and the pilot’s authority to operate this device under FAA/FCC regulations.
NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and
displays, are subject to change and may not reflect the most current G1000 system and aviation databases.
Depictions of equipment may differ slightly from the actual equipment.
F
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
WARNINGS, CAUTIONS, AND NOTES
NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two
conditions: (1) this device may not cause harmful interference, and (2) this device must accept any
interference received, including interference that may cause undesired operation.
NOTE: This product, its packaging, and its components contain chemicals known to the State of California
to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with
California’s Proposition 65. If you have any questions or would like additional information, please refer to
our web site at www.garmin.com/prop65.
NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of
attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 feet
away from the source of the interference should alleviate the condition.
NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank.
NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin
accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of
the data.
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.
Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
G
REVISION INFORMATION
Record of Revisions
Part Number
190-00552-00
190-00552-01
H
190-00552-02
190-00552-03
190-00552-04
Revision
A
A
B
C
A
A
A
Date
03/29/06
07/11/07
07/26/07
08/03/07
10/01/08
03/06/09
08/27/10
Page Range
i – I-4
i – I-6
i – I-6
i – I-6
i – I-6
i – I-6
i – I-6
190-00552-05
A
8/25/2012
1-I-6
Description
Initial release
Added GDU 8.10 parameters, WAAS, VNAV, Airways and Charts
Clerical
Clerical
Added GDU 9.03 parameters
Added GDU 9.05 parameters and Synthetic Vision System
Added GDU 10.01
Added Auxiliary Video
Added AOPA Airport Directory
Added Flight Data Logging
Added METAR, STRMSCP, WX LGND Softkey function
Added Profile View
Added AC-U-KWIK Airport Directory
Added MV DV update procedures
Added Stormscope
Updated database procedures
Updated Message Advisories
Updated TAWS-B VCO alert description
NEXRAD display mutually exclusive with icing and turbulence
information.
Added Selected Altitude Intercept Arc
Added flight plan insertion point indicator
Updated terrain page images to reference GSL altitude
Added other GDU 12.03 parameters
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
TABLE OF CONTENTS
1.1
1.2
1.3
1.4
1.5
1.6
1.7
1.8
SECTION 1 SYSTEM OVERVIEW
System Description.................................................. 1
Line Replaceable Units............................................ 2
G1000 Controls......................................................... 7
PFD/MFD Controls......................................................... 7
MFD/PFD Control Unit.................................................. 10
Secure Digital (SD) Cards...................................... 12
System Power-up.................................................... 13
System Operation................................................... 14
Normal Display Operation............................................ 14
Reversionary Display Operation.................................... 15
AHRS Operation.......................................................... 16
G1000 System Annunciations....................................... 17
Softkey Function.......................................................... 18
GPS Receiver Operation............................................... 24
Accessing G1000 Functionality............................ 29
Menus........................................................................ 29
Data Entry.................................................................. 29
MFD Page Groups........................................................ 31
MFD System Pages...................................................... 35
Display Backlighting.............................................. 47
Automatic Adjustment................................................. 47
Manual Adjustment..................................................... 47
SECTION 2 FLIGHT INSTRUMENTS
2.1 Flight Instruments.................................................... 52
Airspeed Indicator....................................................... 52
Attitude Indicator........................................................ 54
Altimeter.................................................................... 55
Vertical Speed Indicator (VSI)........................................ 57
Vertical Deviation........................................................ 58
Horizontal Situation Indicator (HSI)............................... 59
Course Deviation Indicator (CDI)................................... 64
2.2 Supplemental Flight Data..................................... 71
Temperature Displays................................................... 71
Wind Data.................................................................. 73
Vertical Navigation (VNV) Indications............................ 74
2.3 PFD Annunciations and Alerting Functions......... 75
System Alerting........................................................... 75
Marker Beacon Annunciations...................................... 76
Traffic Annunciation..................................................... 76
190-00552-05 Rev. A
Terrain Annunciations.................................................. 77
Altitude Alerting.......................................................... 78
Low Altitude Annunciation........................................... 78
Minimum Descent Altitude/Decision Height Alerting....... 79
2.4 Abnormal Operations............................................ 80
Abnormal GPS Conditions............................................ 80
Unusual Attitudes........................................................ 81
SECTION 3 ENGINE INDICATION SYSTEM
3.1 EIS Display............................................................... 84
3.2 Engine Page............................................................ 86
Carbon Monoxide Detection......................................... 88
Fuel Calculations Group............................................... 88
Engine Temperature Group........................................... 89
3.3 Engine Leaning Assist Mode................................. 90
Corvalis...................................................................... 90
Corvalis TT.................................................................. 92
4.1
4.2
4.3
4.4
SECTION 4 AUDIO PANEL AND CNS
Overview................................................................. 93
MFD/PFD Controls and Frequency Display...................... 94
Audio Panel Controls................................................... 96
MFD/PFD Control Unit.................................................. 98
COM Operation..................................................... 100
COM Transceiver Selection and Activation.................... 100
COM Transceiver Manual Tuning................................. 101
Quick-Tuning and Activating 121.500 MHz................... 103
Auto-Tuning the COM Frequency................................. 104
Frequency Spacing..................................................... 108
Automatic Squelch..................................................... 109
Volume..................................................................... 109
NAV Operation...................................................... 110
NAV Radio Selection and Activation............................ 110
NAV Receiver Manual Tuning...................................... 111
Auto-Tuning a NAV Frequency from the MFD............... 113
Marker Beacon Receiver............................................. 118
ADF/DME Tuning....................................................... 119
GTX 33 Mode S Transponder............................... 123
Transponder Controls................................................. 123
Transponder Mode Selection....................................... 124
Entering a Transponder Code...................................... 126
IDENT Function......................................................... 127
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
I
TABLE OF CONTENTS
4.5 Additional Audio Panel Functions...................... 128
Power-Up.................................................................. 128
Mono/Stereo Headsets............................................... 128
Speaker.................................................................... 128
Intercom................................................................... 129
Passenger Address (PA) System................................... 131
Clearance Recorder and Player.................................... 131
Split COM................................................................. 132
Entertainment Inputs................................................. 133
4.6 Audio Panel Preflight Procedure........................ 134
4.7 Abnormal Operation............................................ 135
Stuck Microphone...................................................... 135
COM Tuning Failure.................................................... 135
Audio Panel Fail-Safe Operation.................................. 135
Reversionary Mode.................................................... 135
5.1
5.2
5.3
5.4
5.5
5.6
J
SECTION 5 FLIGHT MANAGEMENT
Introduction.......................................................... 137
Navigation Status Box................................................ 138
Using Map Displays.............................................. 140
Map Orientation........................................................ 140
Map Range............................................................... 142
Map Panning............................................................. 145
Measuring Bearing and Distance................................. 149
Topography............................................................... 150
Map Symbols............................................................ 153
Airways.................................................................... 159
Track Vector.............................................................. 161
Wind Vector.............................................................. 162
Nav Range Ring........................................................ 163
Fuel Range Ring........................................................ 164
Field of View (SVS)..................................................... 165
Selected Altitude Intercept Arc.................................... 166
Waypoints.............................................................. 167
Airports.................................................................... 168
Intersections............................................................. 175
NDBs........................................................................ 177
VORs........................................................................ 179
User Waypoints......................................................... 181
Airspaces............................................................... 187
Direct-to-Navigation ........................................... 191
Flight Planning...................................................... 196
Flight Plan Creation................................................... 197
Adding Waypoints to an Existing Flight Plan................. 202
Adding Airways to a Flight Plan.................................. 204
Adding Procedures to a Stored Flight Plan................... 206
Flight Plan Storage.................................................... 213
Flight Plan Editing..................................................... 215
Along Track Offsets.................................................... 219
Parallel Track............................................................. 220
Activating a Flight Plan Leg........................................ 223
Inverting a Flight Plan................................................ 224
Flight Plan Views....................................................... 225
Closest Point of FPL................................................... 227
5.7 Vertical Navigation.............................................. 228
Altitude Constraints................................................... 230
5.8 Procedures............................................................ 234
Departures................................................................ 234
Arrivals .................................................................... 237
Approaches .............................................................. 239
5.9 Trip Planning......................................................... 245
Trip Planning............................................................. 245
5.10 RAIM Prediction................................................... 249
5.11 Navigating a Flight Plan...................................... 252
5.12 Abnormal Operation............................................ 280
6.1
6.2
6.3
6.4
6.5
6.6
SECTION 6 HAZARD AVOIDANCE
SiriusXM Weather................................................. 284
Activating Services..................................................... 284
Using SiriusXM Weather Products............................... 285
Weather Softkeys on the Weather Data Link (XM) Page.289
Stormscope Lightning.......................................... 319
Setting Up Stormscope on the Navigation Map............ 319
Terrain Proximity.................................................. 324
Displaying Terrain Proximity Information...................... 324
Profile View Terrain.............................................. 329
Profile View Display................................................... 329
Terrain-SVS............................................................ 332
Displaying Terrain-SVS Information.............................. 333
Terrain-SVS Alerts...................................................... 337
System Status............................................................ 340
TAWS-B.................................................................. 342
Displaying TAWS-B Data............................................. 343
TAWS-B Page............................................................ 346
TAWS-B Alerts........................................................... 348
System Status............................................................ 354
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
TABLE OF CONTENTS
6.7 Traffic Information Service (TIS)......................... 356
Displaying TRAFFIC Data............................................ 357
Traffic Map Page........................................................ 359
TIS Alerts.................................................................. 360
System Status............................................................ 361
6.8 TCAD 9900BX/TAS 620 Traffic............................. 364
TAS Symbology.......................................................... 364
Displaying Traffic Data............................................... 365
Altitude Display......................................................... 367
Traffic Map Page Display Range.................................. 367
TAS Alerts................................................................. 369
TAS Voice Alerts......................................................... 369
System Status............................................................ 370
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS Controls....................................................... 372
7.2 Flight Director Operation.................................... 374
Activating the Flight Director...................................... 374
AFCS Status Box........................................................ 375
Command Bars.......................................................... 376
Flight Director Modes................................................. 376
7.3 Vertical Modes...................................................... 377
Pitch Hold Mode (PIT)................................................ 378
Selected Altitude Capture Mode (ALTS)........................ 379
Altitude Hold Mode (ALT)........................................... 380
Vertical Speed Mode (VS)........................................... 381
Flight Level Change Mode (FLC).................................. 382
Vertical Navigation Modes (VPTH, ALTV)...................... 384
Glidepath Mode (GP) (SBAS Only)............................... 389
Glideslope Mode (GS)................................................ 391
Go Around Mode (GA)............................................... 392
7.4 Lateral Modes....................................................... 393
Roll Hold Mode (ROL)................................................ 394
Heading Select Mode (HDG)....................................... 395
Navigation Modes (GPS, VOR, LOC,)............................ 396
Approach Modes (GPS, VAPP, LOC).............................. 398
Backcourse Mode (BC)............................................... 400
7.5 Autopilot Operation............................................. 401
Engaging the Autopilot.............................................. 401
Control Wheel Steering.............................................. 402
Disengaging the Autopilot.......................................... 402
7.6 Example Procedures............................................. 403
Departure................................................................. 404
190-00552-05 Rev. A
Intercepting a VOR Radial........................................... 406
Flying a Flight Plan/GPS Course.................................. 407
Descent.................................................................... 408
Approach.................................................................. 412
Go Around/Missed Approach...................................... 416
7.7 AFCS Annunciations and Alerts.......................... 418
AFCS Status Alerts..................................................... 418
Overspeed Protection................................................. 419
SECTION 8 ADDITIONAL FEATURES
8.1 Synthetic Vision System (SVS) (Optional).......... 422
SVS Operation........................................................... 423
SVS Features............................................................. 425
Field of View............................................................. 433
8.2 SafeTaxi................................................................. 435
SafeTaxi Cycle Number and Revision........................... 438
8.3 ChartView (Optional)........................................... 441
ChartView Softkeys.................................................... 442
Terminal Procedures Charts........................................ 443
Chart Options............................................................ 451
Day/Night View......................................................... 457
ChartView Cycle Number and Expiration Date.............. 459
8.4 FliteCharts............................................................. 462
FliteCharts Softkeys................................................... 462
Terminal Procedures Charts........................................ 463
Chart Options............................................................ 470
Day/Night View......................................................... 474
FliteCharts Cycle Number and Expiration Date.............. 476
8.5 Airport Directory.................................................. 479
Airport Directory Database Cycle Number and Revision.480
8.6 SiriusXM Satellite Radio Entertainment
(Optional)........................................................................ 482
Activating SiriusXM Satellite Radio Services................. 482
Using SiriusXM Satellite Radio.................................... 484
8.7 Scheduler............................................................... 487
8.8 Electronic Checklists (Optional)......................... 489
8.9 Flight Data Logging............................................. 492
8.10 Auxiliary Video (Optional)................................... 494
Video Setup.............................................................. 495
Display Selection....................................................... 495
Input Selection.......................................................... 496
Zoom/Range............................................................. 497
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
K
TABLE OF CONTENTS
8.11 Abnormal Operation............................................ 498
SVS Troubleshooting.................................................. 498
Reversionary Mode.................................................... 498
Unusual Attitudes...................................................... 499
APPENDICES
Annunciations and Alerts.............................................. 503
CO Guardian Messages.............................................. 507
G1000 System Annunciations..................................... 507
Other Voice Alerts...................................................... 509
Flight Plan Import/Export Messages............................ 521
Terrain-SVS Alerts...................................................... 523
TAWS-B ALERTS......................................................... 524
TAWS-B System Status Annunciations.......................... 525
Database Management................................................. 527
Jeppesen Databases................................................... 527
Garmin Databases..................................................... 531
Glossary........................................................................... 539
Frequently Asked Questions......................................... 545
General TIS Information................................................ 549
Introduction.............................................................. 549
TIS VS. TAS/TCAS........................................................ 549
TIS Limitations.......................................................... 549
Map Symbols.................................................................. 551
INDEX
Index .................................................................................I-1
L
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
SECTION 1 SYSTEM OVERVIEW
FLIGHT
INSTRUMENTS
1.1 SYSTEM DESCRIPTION
NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the GFC 700 AFCS.
• GDU 1042/1044/1044B Multi Function Display
(MFD)
• GRS 77 Attitude and Heading Reference System
(AHRS)
• GMA 1347 Audio Panel with Integrated Marker
Beacon Receiver
• GMU 44 Magnetometer
• GDL 69A Data Link Receiver
• GCU 476 MFD/PFD Control Unit
• GSA 81 AFCS Servos
• GIA 63/63W Integrated Avionics Units (IAU)
• GTA 82 Pitch Trim Adapter
• GDC 74A Air Data Computer (ADC)
• GSM 85 Servo Gearboxes
FLIGHT
MANAGEMENT
• GTX 33 Mode S Transponder
AUDIO PANEL
& CNS
• GDU 1040/1044B Primary Flight Display (PFD)
EIS
This section provides an overview of the G1000 Integrated Flight Deck as installed in the Cessna 350 Corvalis
and 400 Corvalis TT aircraft. The G1000 is an integrated flight deck system that presents flight instrumentation,
position, navigation, communication, and identification information to the pilot using flat-panel color displays.
The system is consists of the following Line Replaceable Units (LRUs):
HAZARD
AVOIDANCE
• GEA 71 Engine/Airframe Unit
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2.
NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.
AFCS
The Cessna Corvalis/Corvalis TT is also equipped with a GFC 700 Automated Flight Control System (AFCS),
providing the flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000
System.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
1
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
1.2 LINE REPLACEABLE UNITS
FLIGHT
INSTRUMENTS
• GDU 1040/1042/1044/1044B (2) – The GDU 1040 or 1044B is configured as a Primary Flight Display (PFD)
and the GDU 1042 or 1044 or 1044B as a Multi Function Display (MFD). Both displays feature 10.4-inch LCD
screens with 1024 x 768 resolution. The displays communicate with each other through a High-Speed Data
Bus (HSDB) Ethernet connection. Each display is also paired with an Ethernet connection to an IAU.
GDU 1042
GDU 1044
AUDIO PANEL
& CNS
EIS
GDU 1040
FLIGHT
MANAGEMENT
GDU 1044B
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
• GMA 1347 – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio, intercom,
and marker beacon controls, and is installed between the displays. This unit also provides manual control of
display reversionary mode (red DISPLAY BACKUP button; see Section 1.5, System Operation) and communicates
with both IAUs using an RS-232 digital interface.
INDEX
APPENDICES
• GCU 476 – The Control Unit provides MFD/PFD and radio tuning control through an RS-232 digital interface
2
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
• GIA 63/63W (2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking
all LRUs with the PFD. Each IAU contains a GPS receiver, a very high frequency (VHF) communication/
navigation/glideslope (COM/NAV/GS) receiver, and system integration microprocessors, and is paired with the
on-side display via an HSDB connection. The GIA 63W contains a GPS Satellite-Based Augmentation System
(SBAS) receiver. The IAUs are not paired together and do not communicate with each other directly.
EIS
AUDIO PANEL
& CNS
• GDC 74A – The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature
(OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the
G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital
interface.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
• GEA 71 – The Engine Airframe Unit receives and processes signals from the engine and airframe sensors. This
unit communicates with both IAUs using an RS-485 digital interface.
AFCS
ADDITIONAL
FEATURES
• GTX 33 – The solid-state Transponder provides Modes A, C, and S capability and communicates with both IAUs
through an RS-232 digital interface.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
3
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
EIS
FLIGHT
INSTRUMENTS
• GRS 77 (2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading
information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors
(including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field
information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation
is discussed in Section 1.5, System Operation.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
• GMU 44 – The Magnetometer measures local magnetic field and sends data to the AHRS for processing to
determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with
it via an RS-485 digital interface.
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
• GDL 69A – The Data Link Satellite Radio Receiver provides weather data to the G1000 MFD and PFD Inset
Map, as well as digital audio entertainment. The Data Link Receiver communicates with the MFD via a HSDB
connection. A subscription to SiriusXM’s weather data and/or satellite radio service is required to enable the
GDL 69A capability.
• GSA 81, GTA 82, and GSM 85 – The GSA 81 servos are used for automatic control of pitch and roll. The GTA
82 Pitch Trim Adapter works with the existing motor to provide automatic pitch trim. These units interface
with each IAU.
INDEX
APPENDICES
The GSM 85 servo gearboxes are responsible for transferring the output torque of the GSA 81 servo actuators
to the mechanical flight-control surface linkages.
4
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
High-Speed Data Bus (Ethernet)
GDU 1042/1044/
1044B (MFD)
GMA 1347
Audio Panel
GDU 1040/1044B (PFD)
FLIGHT
INSTRUMENTS
Reversionary
Control
Reversionary
Control
EIS
GCU 476
Control Unit
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
GDC 74
Air Data
Computer
OAT
Airspeed
Altitude
Vertical Speed
No. 1 GIA 63/63W
Integrated Avionics Unit
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
GRS 77
AHRS
Attitude
Rate of Turn
Slip/Skid
GPS Output
HAZARD
AVOIDANCE
System Inegration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/WAAS
Glideslope
No. 2 GIA 63/63W
Integrated Avionics Unit
GPS Output
AFCS
GMU 44
Magnetometer
Heading
ADDITIONAL
FEATURES
GTX 33
Transponder
GEA 71
Engine/Airframe
Unit
Autopilot Calculations
GTA 82
Pitch Trim
Adapter
Autopilot Calculations
APPENDICES
GSA 81
Pitch Servo
GSA 81
Roll Servo
Autopilot Calculations
INDEX
Figure 1-1 Basic G1000 System Block Diagram
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
5
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
High-Speed Data Bus (Ethernet)
HAZARD
AVOIDANCE
No. 2 GIA 63/63W
Integrated Avionics Unit
GDL 69A
System Integration Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS/SBAS
Glideslope
Data Link
AFCS
Data Link Weather and
Digital Audio Entertainment
(subscription-based services)
ADDITIONAL
FEATURES
Ryan 9900BX
Provides TAS Information
(optional)
CO Guardian
Carbon Monoxide
Detection
APPENDICES
Figure 1-2 G1000 With Optional/Additional Interfaces
NOTE: For information on additional equipment shown in Figure 1-2, consult the applicable optional interface
INDEX
user’s guide. This document assumes that the reader is already familiar with the operation of this additional
equipment.
6
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
1.3 G1000 CONTROLS
FLIGHT
INSTRUMENTS
The G1000 controls simplify the operation of the system and minimize workload and the time required to
access sophisticated functionality. Controls are located on the PFD and MFD bezels, MFD/PFD Control Unit, and
Audio Panel. PFD and MFD controls and softkeys are discussed in this section. Audio Panel and AFCS (on the
bezel of the MFD) controls are described in the Audio Panel and CNS and AFCS sections, respectively. See the
Audio Panel and CNS Section for more information about NAV/COM controls.
PFD/MFD CONTROLS
2
3
4
5
6
7
8
EIS
1
9
AUDIO PANEL
& CNS
11
14
12
15
HAZARD
AVOIDANCE
13
FLIGHT
MANAGEMENT
10
16
17
AFCS
18
Figure 1-3 PFD/MFD Controls
ADDITIONAL
FEATURES
The NAV, CRS/BARO, COM, FMS, and ALT knobs are concentric dual knobs, each having small (inner)
and large (outer) control portion. When a portion of the knob is not specified in the text, either may be used.
APPENDICES
Large (Outer)
Knob
Small (Inner)
Knob
Figure 1-4 Dual Concentric Knob
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
7
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
FLIGHT
INSTRUMENTS
1
NAV VOL/ID Knob Turn to control NAV audio volume (shown in the NAV Frequency Box as a
percentage)
Press to toggle Morse code identifier audio ON/OFF
Transfers the standby and active NAV frequencies
2
NAV Frequency
Transfer Key
3 NAV Knob
Heading Knob
Press to toggle light blue tuning box between NAV1 and NAV2
Turn to manually select a heading
Joystick
Press to display a digital heading momentarily to the left of the HSI and synchronize
the Selected Heading to the and current heading
Turn to change map range
CRS/BARO Knob
Press to activate Map Pointer for map panning
Turn large knob for altimeter barometric pressure setting
EIS
4
Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz)
AUDIO PANEL
& CNS
5
6
FLIGHT
MANAGEMENT
Turn small knob to adjust course (only when HSI is in VOR or OBS Mode)
7
COM Knob
Press to re-center the CDI and return course pointer directly TO bearing of active
waypoint/station
Turn to tune COM transceiver standby frequencies (large knob for MHz; small for
kHz)
HAZARD
AVOIDANCE
Press to toggle light blue tuning box between COM1 and COM2
8
COM Frequency
Transfer Key
(EMERG)
The selected COM (green) is controlled with the COM MIC Key (Audio Panel).
Transfers the standby and active COM frequencies
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Press and hold two seconds to tune the emergency frequency (121.5 MHz)
automatically into the active frequency field
9 COM VOL/SQ Knob Turn to control COM audio volume level (shown as a percentage in the COM
Frequency Box)
8
10
Direct-to Key (
11
FPL Key
12
CLR Key
(DFLT MAP)
13
MENU Key
14
PROC Key
Press to turn the COM automatic squelch ON/OFF
) Activates the direct-to function and allows the user to enter a destination waypoint
and establish a direct course to the selected destination (specified by identifier,
chosen from the active route)
Displays flight plan information
Erases information, cancels entries, or removes menus
Press and hold to display the MFD Navigation Map Page (MFD only).
Displays a context-sensitive list of options for accessing additional features or making
setting changes
Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and
approach procedures (IAPs) for a flight plan or selected airport
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
ENT Key
Validates/confirms menu selection or data entry
16
FMS Knob
Press to turn the selection cursor ON/OFF.
SYSTEM
OVERVIEW
15
FLIGHT
INSTRUMENTS
(Flight Management Data Entry: With cursor ON, turn to enter data in the highlighted field (large
knob moves cursor location; small knob selects character for highlighted cursor
System Knob)
location). When the cursor is turned ON while viewing the Active Flight Plan
Page, the cursor is placed on the line below the Data Insertion Pointer. The pointer
indicates data entered at the cursor will be inserted above the line selected.
Softkey Selection
Keys
18 ALT Knob
Page Selection: Turn knob on MFD to select the page to view (large knob selects a
page group; small knob selects a specific page from the group)
Press to select softkey shown above the bezel key on the PFD/MFD display
AUDIO PANEL
& CNS
17
EIS
Scrolling: When a list of information is too long for the window/box, a scroll bar
appears, indicating more items to view. With cursor ON, turn large knob to scroll
through the list.
FLIGHT
MANAGEMENT
Sets the Selected Altitude, shown above the Altimeter (the large knob selects the
thousands, the small knob selects the hundreds)
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
9
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
MFD/PFD CONTROL UNIT
FLIGHT
INSTRUMENTS
The MFD/PFD Control Unit is a pedestal-mounted user interface allowing for ease of data entry, PFD/MFD
operation, and NAV/COM tuning. Many procedures in this Pilot’s Guide can be performed using the MFD/PFD
Control Unit rather than the display bezel controls. Indicators above the PFD, MFD, NAV, and COM keys are
illuminated when their respective control mode(s) are selected. The unit is in MFD control mode by default on
system power-up.
AUDIO PANEL
& CNS
EIS
NAV/COM radio tuning can be accomplished in either PFD or MFD control mode. The appropriate frequency
box on the selected display is outlined by a light blue selection box, which flashes for a few seconds to indicate
Control Unit activity (refer to the Audio Panel and CNS Section for more information about NAV/COM tuning).
Selection of a different display control or radio tuning mode results in cancelation of the previous radio tuning
mode.
FLIGHT
MANAGEMENT
1
2
3
4
5
19
18
17
16
HAZARD
AVOIDANCE
15
6
ADDITIONAL
FEATURES
AFCS
14
13
7
12
8
11
10
9
INDEX
APPENDICES
Figure 1-5 GCU 476 MFD/PFD Control Unit
10
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
Direct-to Key (
3
MENU Key
4
PROC Key
5
Joystick
) Activates the direct-to function and allows the user to enter a destination waypoint
and establish a direct course to the selected destination (specified by identifier,
chosen from the active route)
Displays a context-sensitive list of options for accessing additional features or making
setting changes
Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and
approach procedures (IAPs) for a flight plan or selected airport
Turn to change map range
EIS
2
Displays flight plan information
FLIGHT
INSTRUMENTS
FPL Key
SYSTEM
OVERVIEW
1
BKSP Key
Moves cursor back one character space and removes last character entered
8
SPC Key
Adds a space character
9
ENT Key
Validates or confirms a menu selection or data entry
10
CLR Key
Erases information, cancels entries, or removes menus
SEL Key
Press and hold to display the MFD Navigation Map Page (MFD only).
Arrows move light blue Softkey Selection Box (Figure 1-13) on selected display
11
FLIGHT
MANAGEMENT
7
AUDIO PANEL
& CNS
Press to activate Map Pointer for map panning
6 Alphanumeric Keys Allow data entry (rather than using the FMS Knob to select characters/numbers)
HAZARD
AVOIDANCE
Press the center to activate the selected softkey
12
Decimal Key
13
Plus-Minus (±) Key Toggles entry between the + and - characters
14
NAV Key
Selects/deselects NAV radio tuning mode on the MFD/PFD Control Unit
15
COM Key
Selects/deselects COM radio tuning mode on the MFD/PFD Control Unit
16
Frequency Transfer Transfers between active and standby selected COM or NAV tuning frequencies
Key
Press and hold two seconds to tune the emergency frequency (121.5 MHz)
(EMERG)
automatically into the active frequency field
17
PFD Key
When selected, the MFD/PFD Control Unit can be used to access PFD functions
18
MFD Key
19
FMS/NAV-COM
Knob
When selected, the MFD/PFD Control Unit can be used to access MFD functions
(default display control mode)
NAV/COM Tuning Modes: Acts as the NAV or COM Knob
Enters a decimal point character
AFCS
ADDITIONAL
FEATURES
APPENDICES
PFD/MFD Control Modes: Acts as the FMS Knob
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
11
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
1.4 SECURE DIGITAL (SD) CARDS
FLIGHT
INSTRUMENTS
NOTE: Ensure the G1000 System is powered off before inserting an SD card.
NOTE: Refer to Appendix B for instructions on loading database updates.
EIS
The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the
display bezels. SD cards are used for storing the various databases and system software updates. Each display
bezel is equipped with two SD card slots. The top slot is used for importing and exporting flight plans, Flight
Data Logging, and loading navigation database updates. The bottom slot of each display contains a Garmin
Supplemental Data Card which is used for storing the various databases.
AUDIO PANEL
& CNS
Installing an SD card:
1) Insert the SD card in the SD card slot, pushing the card until the spring latch engages. The front of the card
should be flush with the face of the display bezel.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
2) To eject the card, gently press on the SD card to release the spring latch.
ADDITIONAL
FEATURES
AFCS
SD Card Slots
INDEX
APPENDICES
Figure 1-6 Display Bezel SD Card Slots
12
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
1.5 SYSTEM POWER-UP
FLIGHT
INSTRUMENTS
NOTE: See the Airplane Flight Manual (AFM) for specific procedures concerning avionics power application
and emergency power supply operation.
NOTE: Refer to Appendix A for system-specific annunciations and alerts.
EIS
The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical
busses. The G1000 PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test
features that exercise the processor, system memory, external inputs, and outputs to provide safe operation.
AUDIO PANEL
& CNS
During system initialization, test annunciations are displayed, as shown in Figure 1-7. All system annunciations
should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also
become momentarily illuminated on the Audio Panel, the MFD/PFD Control Unit, and the display bezels.
On the PFD, the AHRS begins to initialize and displays “AHRS ALIGN: Keep Wings Level”. The AHRS should
display valid attitude and heading fields typically within the first minute of power-up. The AHRS can align itself
both while taxiing and during level flight.
FLIGHT
MANAGEMENT
When the MFD powers up, the splash screen (Figure 1-8) displays the following information:
• Obstacle database name and version
• Navigation database name, version, and effective dates
• Airport Directory name, version and effective dates
• FliteCharts/ChartView database information
HAZARD
AVOIDANCE
• System version
• Copyright
• Land database name and version
• Safe Taxi database information
• Terrain database name and version
Current database information includes database type, cycle number, or valid operating dates. Review the listed
information for currency (to ensure that no databases have expired).
AFCS
Pressing the ENT Key (or right-most softkey) acknowledges this information, and the Navigation Map Page is
displayed upon pressing the key a second time. When the system has acquired a sufficient number of satellites to
determine a position, the aircraft’s current position is shown on the Navigation Map Page.
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 1-7 PFD Initialization
190-00552-05 Rev. A
Figure 1-8 MFD Power-Up
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
13
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
1.6 SYSTEM OPERATION
FLIGHT
INSTRUMENTS
The displays are connected together via a single Ethernet bus for high-speed communication. As shown in
Figure 1-1, each IAU is connected to a single display. This allows the units to share information, enabling true
system integration.
NORMAL DISPLAY OPERATION
NOTE: In normal operating mode, backlighting can only be adjusted from the PFD, or from any display
EIS
operating in reversionary mode.
AUDIO PANEL
& CNS
In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed,
altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section
for more information).
The MFD normally displays a full-color moving map with navigation information (see the Flight Management
Section), while the left portion of the MFD is dedicated to the Engine Indication System (EIS; see the EIS
Section).
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Both displays offer control for COM and NAV frequency selection.
INDEX
Figure 1-9 G1000 Normal Operation
14
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
REVERSIONARY DISPLAY OPERATION
NOTE: The system alerts the pilot when backup paths are utilized by the LRUs. Refer to the Appendices for
FLIGHT
INSTRUMENTS
further information regarding system-specific alerts.
In the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In
Reversionary Mode, all important flight information from the PFD is presented on the operating display in the
same format as in normal operating mode, with the addition of the EIS. EIS operation while in Reversionary
Mode is discussed in the EIS Section. As when the PFD is operating normally, windows for flight planning,
nearest airports, and procedures are available. The Inset Map is moved to the right side of the display.
EIS
AUDIO PANEL
& CNS
If a display fails, the appropriate IAU-display Ethernet interface is cut off. Thus, the IAU can no longer
communicate with the operating display (refer to Figure 1-1), and the NAV and COM functions provided to
the failed display by the IAU are flagged as invalid on the operating display. The system reverts to backup
paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is
completely automated for all LRUs and no pilot action is required.
FLIGHT
MANAGEMENT
If the system fails to detect a display problem, Reversionary Mode may be manually activated by pressing
the Audio Panel’s red DISPLAY BACKUP Button (refer to the Audio Panel & CNS Section for further details).
Pressing this button again deactivates Reversionary Mode.
NAV1 and COM1 (provided by
the failed PFD) Flagged Invalid
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
The DISPLAY BACKUP Button Activates/Deactivates
Reversionary Mode on Both Displays
APPENDICES
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
Figure 1-10 G1000 Reversionary Mode (Failed PFD)
15
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
AHRS OPERATION
FLIGHT
INSTRUMENTS
NOTE: Refer to Appendix A for specific AHRS alert information.
NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy.
EIS
The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration
calculations for the G1000 System, using GPS, magnetometer, and air data in addition to information from its
internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate
combinations of information from the external sensor inputs.
unavailable
available
le
ab
Attitude/Heading Invalid
ADDITIONAL
FEATURES
AFCS
AHRS
no-GPS
Mode
ail
av
AHRS no- AHRS no-Mag/
Mag Mode
no-Air Mode
Heading Invalid
Air Data
un
HAZARD
AVOIDANCE
Air Data
AHRS Normal
Operation
Magnetometer Data
available
available
unavailable
Magnetometer Data
available
FLIGHT
MANAGEMENT
available
unavailable
GPS Data
unavailable
AUDIO PANEL
& CNS
The system uses message advisory alerts to communicates loss of GPS, magnetometer, or air data inputs (refer
to Appendix A for specific AHRS alert information). Any failure of the internal AHRS inertial sensors results in
loss of attitude and heading information (indicated by red ‘X’ flags over the corresponding flight instruments).
Figure 1-11 AHRS Operation
APPENDICES
NOTE: In-flight initialization of AHRS, when operating without any valid source of GPS data and at true
air speed values greater than approximately 200 knots, is not guaranteed. Under these rare conditions, it
is possible for in-flight AHRS initialization to take an indefinite amount of time which would result in an
extended period of time where valid AHRS outputs are unavailable.
INDEX
Two GPS inputs are provided to the AHRS. If GPS information from one of the inputs fails, the AHRS uses
the operating GPS input and an alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS
16
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
can continue to provide attitude and heading information to the PFD as long as magnetometer and airspeed
data are available and valid.
FLIGHT
INSTRUMENTS
If the magnetometer input fails, the AHRS continues to output valid attitude information; however, the
heading output on the PFD is flagged as invalid with a red ‘X’.
Failure of the air data input has no affect on the AHRS output while AHRS is receiving valid GPS information.
Invalid/unavailable airspeed data in addition to GPS failure results in loss of all attitude and heading information.
EIS
The AHRS (GRS 77) corrects for shifts and variations in the Earth’s magnetic field by applying the Magnetic
Field Variation Database. The Magnetic Field Variation Database is derived from the International Geomagnetic
Reference Field (IGRF). The IGRF is a mathematical model that describes the Earth’s main magnetic field and
its annual rate of change. The database is updated approximately every five years. See the Appendices for
information on updating the Magnetic Field Variation Database. The system will prompt the pilot on startup
when an update is available. Failure to update this database could lead to erroneous heading information being
displayed to the pilot.
AUDIO PANEL
& CNS
G1000 SYSTEM ANNUNCIATIONS
FLIGHT
MANAGEMENT
When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with
the failed data (Figure 1-12 displays all possible flags and responsible LRUs). Upon G1000 power-up, certain
instruments remain invalid as equipment begins to initialize. All windows should be operational within one
minute of power-up. If any window remains flagged, the G1000 should be serviced by a Garmin-authorized
repair facility.
HAZARD
AVOIDANCE
NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Airplane
Flight Manual (AFM) for additional information regarding pilot responses to these annunciations.
GIA 63/63W Integrated Avionics Unit
ADDITIONAL
FEATURES
GEA 71 Engine
Airframe Unit
OR
GIA 63/63W
Integrated
Avionics Unit
AFCS
GIA 63/63W
Integrated
Avionics Unit
GDC 74 Air
Data Computer
Database
Mismatch in
PFD and MFD
APPENDICES
GRS 77 AHRS
OR GMU 44
Magnetometer
GIA 63/63W
Integrated
Avionics Unit
INDEX
GDC 74 Air
Data Computer
GTX 33 Transponder OR GIA 63/63W
Integrated Avionics Unit
Figure 1-12 G1000 System Failure Annunciations
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
17
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
SOFTKEY FUNCTION
FLIGHT
INSTRUMENTS
The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or
page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When a
softkey is selected, its color changes to black text on gray background and remains this way until it is disabled,
at which time it reverts to white text on black background. When a softkey function is disabled, the softkey
label is subdued (dimmed). Softkeys revert to the previous level after 45 seconds of inactivity.
Bezel-Mounted
Softkeys (Press)
Softkey Selection
Box (Light Blue)
Softkey Names
(Displayed)
EIS
Softkey
On
AUDIO PANEL
& CNS
Figure 1-13 Softkeys (Second-Level PFD Configuration)
The MFD/PFD Control Unit can also be used to select softkeys.
Selecting a softkey using the MFD/PFD Control Unit:
FLIGHT
MANAGEMENT
1) Choose the desired display control mode by pressing the PFD or MFD Key on the MFD/PFD Control Unit.
2) Move the softkey selection box to the desired softkey using the arrows of the SEL Key.
3) Press the center of the SEL Key to select the desired softkey.
HAZARD
AVOIDANCE
In the following descriptions, top level softkeys are denoted by bullets.
PFD SOFTKEYS
The CDI, IDENT, TMR/REF, NRST, and ALERTS softkeys undergo a momentary change to black text on
gray background and automatically change to white text on black background when selected.
AFCS
The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic,
and lightning (optional). Each softkey sublevel has a BACK Softkey which can be selected to return to the
previous level. The ALERTS Softkey is visible at all softkey levels (label changes if messages are issued).
ADDITIONAL
FEATURES
(optional)
INSET
PFD
OBS
CDI
ADF/DME
XPDR
IDENT
TMR/REF
NRST
ALERTS
APPENDICES
Press the CDI Softkey to cycle
through navigation sources:
- GPS
- NAV1 (VOR/LOC)
- NAV2 (VOR/LOC)
INDEX
Figure 1-14 Top Level PFD Softkeys
INSET
18
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
(optional) (optional)
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
Displays Inset Map in PFD lower left corner
• INSET
Removes Inset Map
OFF
DCLTR (3) Selects desired amount of map detail; cycles through declutter levels:
DCLTR (No Declutter): All map features visible
DCLTR-1: Removes land data
DCLTR-2: Removes land and SUA data
(optional)active flight plan
DCLTR-3: Removes everything except
INSET
PFD
OBS
CDI
XPDR
IDENT TMR/REF
ALERTS
ADF/DME
product
icon
and weatherNRST
product
age box for
WX LGND Displays/removes the SiriusXM Weather
displayed weather products (optional)
Press the CDIon
Softkey
cycle
InsettoMap
TRAFFIC Displays/removes traffic information
through navigation sources:
- GPS
Displays/removes topographical
data (e.g., coastlines, terrain, rivers, lakes) on Inset Map
TOPO
- NAV1 (VOR/LOC)
on Inset Map
TERRAIN Displays/removes terrain information
- NAV2 (VOR/LOC)
STRMSCP Displays/removes Stormscope lightning information on Inset Map (optional)
Displays/removes NEXRAD weather and radar coverage information on Inset Map (optional)
NEXRAD
XM LTNG Displays/removes SiriusXM lightning information on Inset Map (optional)
Displays/removes SiriusXM METAR information on Inset Map (optional)
METAR
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
INSET
DCLTR
HAZARD
AVOIDANCE
(optional) (optional) (optional) (optional)
(optional)
OFF
WX LGND TRAFFIC
TRFC-1
DCLTR-2
TRFC-2
TERRAIN STRMSCP NEXRAD XM LTNG
METAR
BACK
ALERTS
Press the OFF or BACK Softkey
to return to the top-level softkeys.
AFCS
DCLTR-1
TOPO
DCLTR-3
ADDITIONAL
FEATURES
Figure 1-15 INSET Softkeys
STBY
ON
ALT
GND
VFR
CODE
APPENDICES
XPDR
IDENT
BACK
ALERTS
INDEX
Press the BACK Softkey to
return to the top-level softkeys.
190-00552-05 Rev. A
0
1
2
3
4
5
6
7
IDENT
BKSP
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
BACK
ALERTS
19
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
Displays second-level softkeys for additional PFD configuration
Displays the softkeys for enabling or disabling Synthetic Vision features (optional)
Displays rectangular boxes representing the horizontal and vertical flight path of the
active flight plan
SYN TERR Enables synthetic terrain depiction
HRZN HDG Displays compass heading along the Zero-Pitch line
APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft
position. Airport identifiers are displayed when the airport is within approximately
9nm.
Resets PFD to default settings, including changing units to standard
DFLTS
Displays softkeys to select and configure wind data
WIND
Displays wind direction arrows with headwind and crosswind components
OPTN1
Displays wind direction arrow and speed
OPTN2
Displays wind direction arrow with direction and speed
OPTN3
Removes wind information from display
OFF
Displays/removes DME Information Window (optional)
DME
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
• PFD
SYN VIS
PATHWAY
HAZARD
AVOIDANCE
BRG1
ADDITIONAL
FEATURES
AFCS
HSI FMT
360 HSI
ARC HSI
BRG2
ALT UNIT
INDEX
APPENDICES
METERS
IN
HPA
STD BARO
• OBS
• CDI
• ADF/DME
20
Cycles the Bearing 1 Information Window through:
NAV1: Waypoint frequency/identifier and DME information
GPS: Waypoint identifier and GPS distance information
ADF: Waypoint frequency
Off: Removes window
Displays softkeys to select the HSI format
Displays HSI as a 360° compass rose
Displays HSI as a 140° viewable arc (Bearing Information windows unavailable)
Cycles the Bearing 2 Information Window through:
NAV2: Waypoint frequency/identifier and DME information
GPS: Waypoint identifier and GPS distance information
ADF: Waypoint frequency
Off: Removes window
Displays softkeys for changing the Altimeter barometric setting and altitude displays to
metric units
Displays the current and Selected altitudes in meters in addition to feet, when selected
Displays the Altimeter barometric setting in inches of mercury (in Hg)
Displays the Altimeter barometric setting in hectopascals (hPa)
Sets barometric pressure to 29.92 in Hg (1013 hPa if metric display is selected)
Selects OBS Mode on the CDI when navigating by GPS (only available with active leg)
Cycles CDI through GPS, NAV1 (VOR/LOC), and NAV2 (VOR/LOC) navigation sources
Displays/removes ADF/DME Radio Tuning Window (optional; may appear as ADF, DME,
or ADF/DME depending on installation)
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
PFD
SYN VIS
FLIGHT
INSTRUMENTS
(optional)
(optional)
DFLTS
WIND
BRG1
DME
HSI FMT
ALT UNIT STD BARO
BRG2
BACK
ALERTS
OPTN2
OPTN3
OFF
METERS
ARC HSI
IN
HPA
BACK
ALERTS
BACK
ALERTS
BACK
ALERTS
HAZARD
AVOIDANCE
PATHWAY SYN TERR HRZN HDG APTSIGNS
ALERTS
FLIGHT
MANAGEMENT
360 HSI
BACK
AUDIO PANEL
& CNS
OPTN1
EIS
Press the BRG1/BRG2
Press the STD BARO or BACK
softkeys to display/remove Softkey to return to the top-level
the Bearing Information
softkeys.
windows and cycle through
bearing sources:
- NAV1/NAV2
- GPS
- ADF
Figure 1-16 PFD Configuration Softkeys
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
21
- GPS
- NAV1 (VOR/LOC)
- NAV2 (VOR/LOC)
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
Displays transponder mode selection softkeys:
Selects standby mode (Transponder does not reply to any interrogations)
INSET
Selects Mode A (Transponder replies to interrogations)
Selects Mode C – altitude reporting mode (Transponder replies to identification and altitude
interrogations)
Manually selects Ground Mode (Transponder does not allow Mode A and Mode C
GND
replies, but does permit acquisition squitter and
replies
to discretely addressed Mode S
(optional)
(optional)
XM
LTNG
NEXRAD
TRAFFIC
ALERTS
OFF
DCLTR
TOPO
TERRAIN
BACK
interrogations)
Automatically enters the VFR code (1200 in U.S.A. only)
VFR
Displays transponder
code selection softkeys 0-7
CODE
Press the OFF or BACK Softkey
DCLTR-1
TRFC-1
to return to the top-level softkeys.
Use numbers to enter code
0—7
TRFC-2
Removes numbers
entered, one at a time
BKSP DCLTR-2
Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the
• IDENT
DCLTR-3
transponder return on the ATC screen
• TMR/REF Displays/removes Timer/References Window
Displays/removes Nearest Airports Window
• NRST
Displays/removes Alerts Window
• ALERTS
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
• XPDR
STBY
ON
ALT
HAZARD
AVOIDANCE
XPDR
STBY
ON
ALT
GND
VFR
CODE
IDENT
BACK
ALERTS
AFCS
Press the BACK Softkey to
return to the top-level softkeys.
1
2
3
4
5
6
ADDITIONAL
FEATURES
0
7
IDENT
BKSP
BACK
ALERTS
APPENDICES
Press the IDENT or BACK
Softkey to return to the toplevel softkeys.
INDEX
Figure 1-17 XPDR Softkeys
22
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
MFD SOFTKEYS
MFD softkeys vary depending on the page selected. EIS and Navigation Map Page (default MFD page)
softkeys are described here.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
• CHKLIST
AUDIO PANEL
& CNS
TERRAIN
NEXRAD
XM LTNG
METAR
LEGEND
BACK
• DCLTR (3)
Displays EIS Page and second-level engine softkeys; press again to exit EIS Page (see the EIS
Section for more information)
Turns oxygen system ON/OFF (optional)
Turns off CHT and EGT cylinder readouts
Accesses engine leaning assist mode
Resets the CO Guardian and acknowledges CO warning alert
Decreases displayed fuel remaining in 1-gal increments
Increases displayed fuel remaining in 1-gal increments
Resets displayed fuel remaining to 98 gallons and fuel used to zero
Enables second-level Navigation Map Page softkeys
Displays/removes traffic information on Navigation Map Page
Displays/removes profile view display on the Navigation Map Page
Displays/removes topographical data (e.g., coastlines, terrain, rivers, lakes) on Navigation
Map Page
Displays/removes terrain information on Navigation Map Page
Displays/removes NEXRAD weather/coverage on Navigation Map Page (optional)
Displays/removes SiriusXM lightning information on Navigation Map Page (optional)
Displays/removes METAR information on the Navigation Map Page (optional)
Displays/removes XM Weather Legends window for enabled weather products (optional)
Returns to top-level softkeys
Selects desired amount of map detail; cycles through declutter levels:
DCLTR (No Declutter): All map features visible
DCLTR-1: Removes land data
DCLTR-2: Removes land and SUA data
DCLTR-3: Removes everything except the active flight plan
Displays the optional Checklist Page; press the EXIT Softkey to return to the top-level
softkeys
EIS
OXYGEN
DCLTR
ASSIST
CO RST
DEC FUEL
INC FUEL
RST FUEL
• MAP
TRAFFIC
PROFILE
TOPO
FLIGHT
INSTRUMENTS
• SYSTEM
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
23
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
(optional) (optional)
MAP
SYSTEM
DCLTR
SHW CHRT CHKLIST
FLIGHT
INSTRUMENTS
DCLTR-1
DCLTR-2
DCLTR-3
EIS
(optional) (optional) (optional) (optional) (optional)
AUDIO PANEL
& CNS
TRAFFIC PROFILE
TOPO
TERRAIN AIRWAYS STRMSCP NEXRAD
XM LTNG
METAR
LEGEND
BACK
Press the BACK Softkey to
return to the top-level softkeys.
Press the SYSTEM Softkey to
return to the top-level softkeys.
(optional)
FLIGHT
MANAGEMENT
SYSTEM
OXYGEN
DCLTR
ASSIST
CO RST
DEC FUEL INC FUEL RST FUEL
Figure 1-18 EIS and MFD Softkeys
GPS RECEIVER OPERATION
HAZARD
AVOIDANCE
Each GIA 63/63W Integrated Avionics Unit (IAU) contains a GPS receiver. Information collected by the
specified receiver (GPS1 for the #1 IAU or GPS2 for the #2 IAU) may be viewed on the AUX - GPS Status
Page.
AFCS
These GPS sensor annunciations are most often seen after system power-up when one GPS receiver has
acquired satellites before the other, or in SBAS (Satellite-Based Augmentation System) capable systems, one of
the GPS receivers has not yet acquired an SBAS signal. While the aircraft is on the ground, the SBAS signal may
be blocked by obstructions causing one GPS receiver to have difficulty acquiring a good signal. Also, while
airborne, turning the aircraft may result in one of the GPS receivers temporarily losing the SBAS signal.
ADDITIONAL
FEATURES
If the sensor annunciation persists, check for a system failure message in the Messages Window on the PFD.
If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2.
Discrepancies may indicate a problem.
Viewing GPS receiver status information
APPENDICES
1) Use the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.7 for information on
navigating MFD page groups).
2) Use the small FMS Knob to select GPS Status Page.
Selecting the GPS receiver for which data may be reviewed
INDEX
1) Turn the FMS Knob to select the AUX - GPS Status Page.
2) To change the selected GPS receiver:
a) Select the desired GPS Softkey.
24
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
Or:
a) Press the MENU Key.
b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key.
Satellite Signal
Information Status
FLIGHT
INSTRUMENTS
Satellite Constellation
Diagram
GPS Receiver
Status
RAIM
Availability
Prediction
EIS
AUDIO PANEL
& CNS
SBAS
Selected
FLIGHT
MANAGEMENT
Satellite Signal
Strength Bars
Figure 1-19 GPS Status Page (RAIM or SBAS Selected)
HAZARD
AVOIDANCE
RAIM Softkey
Selected
SBAS Softkey
Selected
The GPS Status Page provides the following information:
AFCS
• Satellite constellation diagram
ADDITIONAL
FEATURES
Satellites currently in view are shown at their respective positions on a sky view diagram. The sky view is
always in a north-up orientation, with the outer circle representing the horizon, the inner circle representing
45° above the horizon, and the center point showing the position directly overhead.
Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite
identification number). Satellites whose signals are currently being used are represented by solid ovals.
• Satellite signal information status
APPENDICES
The accuracy of the aircraft’s GPS fix is calculated using Estimated Position Uncertainty (EPU), Dilution
of Precision (DOP), and horizontal and vertical figures of merit (HFOM and VFOM). EPU is the radius of a
circle centered on an estimated horizontal position in which actual position has 95% probability of laying.
EPU is a statistical error indication and not an actual error measurement.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
DOP measures satellite geometry quality (i.e., number of satellites received and where they are relative to
each other) on a range from 0.0 to 9.9, with lower numbers denoting better accuracy. HFOM and VFOM,
25
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
measures of horizontal and vertical position uncertainty, are the current 95% confidence horizontal and
vertical accuracy values reported by the GPS receiver.
FLIGHT
INSTRUMENTS
The current calculated GPS position, time, altitude, ground speed, and track for the aircraft are displayed
below the satellite signal accuracy measurements.
• GPS receiver status
EIS
The GPS solution type (ACQUIRING, 2D NAV, 2D DIFF NAV, 3D NAV, 3D DIFF NAV) for the active
GPS receiver (GPS1 or GPS2) is shown in the upper right of the GPS Status Page. When the receiver is
in the process of acquiring enough satellite signals for navigation, the receiver uses satellite orbital data
(collected continuously from the satellites) and last known position to determine the satellites that should be
in view. ACQUIRING is indicated as the solution until a sufficient number of satellites have been acquired
for computing a solution.
AUDIO PANEL
& CNS
When the receiver is in the process of acquiring a 3D navigational GPS solution, 3D NAV is indicated as the
solution until the 3D differential fix has finished acquisition. SBAS (Satellite-Based Augmentation System)
indicates INACTIVE. When acquisition is complete, the solution status indicates 3D DIFF NAV and SBAS
indicates ACTIVE.
FLIGHT
MANAGEMENT
• RAIM (Receiver Autonomous Integrity Monitoring) Prediction (RAIM Softkey is selected)
In most cases performing a RAIM prediction is not necessary. However, in some cases, the selected approach
may be outside the SBAS coverage area and it may be necessary to perform a RAIM prediction for the intended
approach.
HAZARD
AVOIDANCE
Receiver Autonomous Integrity Monitoring (RAIM) is a GPS receiver function that performs a consistency
check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to
calculate a position within a specified RAIM protection limit (2.0 nautical miles for oceanic and enroute, 1.0
nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of
flight, RAIM is available nearly 100% of the time.
AFCS
The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM
computations predict satellite coverage within ±15 min of the specified arrival date and time.
ADDITIONAL
FEATURES
Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The
G1000 automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not
predicted to be available for the final approach course, the approach does not become active, as indicated by
the messages “Approach is not active” and “RAIM not available from FAF to MAP”. If RAIM is not available
when crossing the FAF, the missed approach procedure must be flown.
Predicting RAIM availability
APPENDICES
1) Select the GPS Status Page.
2) If necessary, select the RAIM Softkey.
3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted.
4) Turn the small FMS Knob to display the Waypoint Information Window.
INDEX
5) Enter the desired waypoint:
a) Use the FMS Knob to enter the desired waypoint by identifier, facility, or city name and press the ENT Key. Refer
to Section 1.7 for instructions on entering alphanumeric data into the G1000.
26
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
Or:
a) Use the large FMS Knob to scroll to the Most Recent Waypoints List.
FLIGHT
INSTRUMENTS
b) Use the small FMS Knob to highlight the desired waypoint in the list and press the ENT Key. The G1000
automatically fills in the identifier, facility, and city fields with the information for the selected waypoint.
c) Press the ENT Key to accept the waypoint entry.
Or:
a) To use the present position, press the MENU Key.
b) With ‘Set WPT to Present Position’ highlighted, press the ENT Key.
EIS
c) Press the ENT Key to accept the waypoint entry.
6) Use the FMS Knob to enter an arrival time and press the ENT Key.
AUDIO PANEL
& CNS
7) Use the FMS Knob to enter an arrival date and press the ENT Key.
8) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one
of the following is displayed:
• ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination
• ‘COMPUTING AVAILABILITY’—RAIM calculation in progress
• ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date
• ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
• SBAS Selection (SBAS Softkey is pressed) (WAAS, EGNOS, or MSAS-capable systems only)
In certain situations, such as when the aircraft is outside or on the fringe of the WAAS, EGNOS, or MSAS
coverage area, it may be desirable to disable the reception of the applicable SBAS signal (although it is not
recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. There may be a
small delay for the GPS Status box to be updated upon WAAS, EGNOS, and MSAS enabling/disabling.
AFCS
Disabling WAAS, EGNOS or MSAS
1) Select the GPS Status Page.
2) If necessary, select the SBAS Softkey.
ADDITIONAL
FEATURES
3) Press the FMS Knob, and turn the large FMS Knob to highlight the desired SBAS system.
4) Press the ENT Key to uncheck the box.
5) Press the FMS Knob to remove the cursor.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
27
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
FLIGHT
INSTRUMENTS
• GPS Satellite Signal Strengths
The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite
coverage or installation problems. As the GPS receiver locks onto satellites, a signal strength bar is displayed
for each satellite in view, with the appropriate satellite PRN number (01-32 or 120-138 for SBAS) below each
bar. The progress of satellite acquisition is shown in three stages, as indicated by signal bar appearance:
EIS
- No bar—Receiver is looking for the indicated satellite
- Hollow bar—Receiver has found the satellite and is collecting data
- Light blue bar—Receiver has collected the necessary data and the satellite signal can be used
- Green bar—Satellite is being used for the GPS solution
- Checkered bar—Receiver has excluded the satellite (Fault Detection and Exclusion)
- “D” indication—Denotes the satellite is being used as part of the differential computations
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Each satellite has a 30-second data transmission that must be collected (signal strength bar is hollow) before
the satellite may be used for navigation (signal strength bar becomes solid).
28
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
1.7 ACCESSING G1000 FUNCTIONALITY
MENUS
FLIGHT
INSTRUMENTS
EIS
The G1000 has a dedicated MENU Key that when pressed displays a context-sensitive list of options. This
options list allows the user to access additional features or make settings changes which specifically relate to
the currently displayed window/page. There is no all-encompassing menu. Some menus provide access to
additional submenus that are used to view, edit, select, and review options. Menus display ‘NO OPTIONS’
when there are no options for the window/page selected. The main controls used in association with all
window/page group operations are described in Section 1.3, G1000 Controls. Softkey presses do not display
menus or submenus.
Navigating a menu:
AUDIO PANEL
& CNS
1) Press the MENU Key to display the menu.
2) Turn the FMS Knob to scroll through a list of available options (a scroll bar always appears to the right of the
window/box when the option list is longer than the window/box).
3) Press the ENT Key to select the desired option.
FLIGHT
MANAGEMENT
4) Press the CLR Key or FMS Knob to remove the menu and cancel the operation.
No Options for
NRST Window
Options for FPL Window
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 1-20 Page Menu Examples
DATA ENTRY
APPENDICES
Two methods exist for directly entering alphanumeric data (e.g., waypoint identifiers, barometric minimum
descent altitude) into the G1000: using the alphanumeric keypad (on the MFD/PFD Control Unit) or the FMS
Knob corresponding to the display (PFD, MFD, or MFD/PFD Control Unit). In some instances, such as when
entering an identifier, the G1000 will try to predict the desired identifier based on the characters being entered.
In this case, if the desired identifier appears, use the ENT Key to confirm the entry without entering the rest of
the identifier manually. This can save the pilot from entering all the characters of the identifier.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
Besides character-by-character data entry, the system also provides a shortcut for entering waypoint identifiers.
When the cursor is on a field awaiting entry of a waypoint identifier, turning the small FMS Knob counterclockwise accesses three different lists of waypoint identifiers for quick selection: flight plan (FPL), nearest
29
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
(NRST), and recently-entered (RECENT). The G1000 automatically fill in the identifier, facility, and city fields
with the information for the selected waypoint.
FLIGHT
INSTRUMENTS
Using the MFD/PFD Control Unit keypad to enter data:
1) Choose the desired display control mode by pressing the PFD or MFD Key on the MFD/PFD Control Unit.
2) If needed, press the FMS Knob to activate the cursor.
3) Use the large FMS Knob to highlight the desired field.
4) Use the alphanumeric keys to enter the desired information.
EIS
5) Press the ENT Key to confirm the entry
6) Press the CLR Key to cancel data entry (the field revers back to its previous information).
AUDIO PANEL
& CNS
Using the FMS Knob to enter data:
1) If needed, press the FMS Knob to activate the cursor.
2) Use the large FMS Knob to highlight the desired field.
FLIGHT
MANAGEMENT
3) Begin entering data by turning the small FMS Knob to select a character for the first placeholder.
Turning the knob to the right scrolls through the alphabet (where appropriate) toward the letter Z, starting in
the middle at K, and the digits zero through nine. Turning the knob to the left scrolls in the opposite direction.
4) Use the large FMS Knob to move the cursor to the next placeholder in the field.
HAZARD
AVOIDANCE
5) Repeat, using the small FMS Knob to select a character and the large FMS Knob to move the cursor, until the
field is complete.
6) Press the ENT Key to confirm entry.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
7) Press the FMS Knob or CLR Key to cancel data entry (the field reverts back to its previous information).
30
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
MFD PAGE GROUPS
NOTE: Refer to the Flight Management, Hazard Avoidance, and Additional Features sections for details on
FLIGHT
INSTRUMENTS
specific pages.
Page Group
EIS
Information on the MFD is presented on pages which are grouped according to function. The page group
and active page title are displayed in the upper center of the screen, below the Navigation Status Box. The page
group tabs are displayed along the bottom right corner of the screen. Available pages in the group are displayed
in a list above the page groups. The current page group and current page within the group are shown in light
blue. For some of these pages (Airport/Procedure/Weather Information, XM, Procedure Loading), the active
title of the page changes while the page name in the list remains the same.
Active Page Title
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Pages in
Current
Group
HAZARD
AVOIDANCE
Page Groups
MFD
Figure 1-21 Page Title and Page Groups
AFCS
Selecting a page using the FMS Knob:
ADDITIONAL
FEATURES
1) Turn either FMS Knob one click to display the pop-up page selection window.
2) Turn the large FMS Knob until the desired page group is selected. For example, the MAP page group is selected
in Figure 1-21.
3) Turn the small FMS Knob until the desired page is selected.
APPENDICES
There are also several pages (Airport/Procedures/Weather Information and XM pages) which are selected first
from within a main page group with the FMS Knob, then with the appropriate softkey at the bottom of the page
(or from the page menu). In this case, the page remains set to the selected page until a different page softkey is
selected, even if a different page group is selected.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
31
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
• Map Page Group (MAP)
Navigation Map
FLIGHT
INSTRUMENTS
Traffic Map
Weather Data Link (XM) (service optional)
AUDIO PANEL
& CNS
EIS
Terrain Proximity/Terrain-SVS/TAWS-B
FLIGHT
MANAGEMENT
Figure 1-22 Map Pages
HAZARD
AVOIDANCE
Waypoint Pages (WPT)
Airport Information pages
- Airport Information
(INFO-1 Softkey)
AFCS
- Airport Directory
(INFO-2 Softkey)
- Departure Information
(DP Softkey)
ADDITIONAL
FEATURES
- Arrival Information
(STAR Softkey)
- Approach Information
(APR Softkey)
APPENDICES
- Weather Information
(WX Softkey)
Intersection Information
Airport
Information
Pages
NDB Information
INDEX
VOR Information
User Waypoint Information
32
Figure 1-23 Waypoint Pages
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
Auxiliary Pages (AUX)
FLIGHT
INSTRUMENTS
Trip Planning
Utility
GPS Status
System Setup
EIS
XM Satellite pages
- XM Information
(INFO Softkey)
- XM Radio
(RADIO Softkey)
AUDIO PANEL
& CNS
XM
Satellite
Pages
System Status
Video (Optional)
FLIGHT
MANAGEMENT
Figure 1-24 Auxiliary Pages
• Nearest Page Group (NRST)
HAZARD
AVOIDANCE
Nearest Airports
Nearest Intersections
Nearest NDB
Nearest VOR
AFCS
Nearest User Waypoints
Nearest Frequencies
Nearest Airspaces
ADDITIONAL
FEATURES
APPENDICES
Figure 1-25 Nearest Pages
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
33
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
In addition to the main page groups accessed exclusively using the FMS Knob, there are pages for flight
planning (FPL) and loading procedures (PROC) which are accessed by key. In some instances, softkeys may be
used to access the Procedure Loading pages.
FLIGHT
INSTRUMENTS
The Flight Plan pages are accessed using the FPL Key on the MFD. Main pages within this group are selected
by turning the small FMS Knob.
• Flight Plan Page Group (FPL)
Active Flight Plan
Flight Plan Catalog
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
- Stored Flight Plan
(NEW Softkey)
Figure 1-26 Flight Plan Pages
HAZARD
AVOIDANCE
The Procedure Loading pages may be accessed at any time on the MFD by pressing the PROC Key. A menu
is initialized, and when a departure, approach, or arrival is selected, the appropriate Procedure Loading page is
opened. Turning the FMS Knob does not scroll through the Procedure Loading pages.
• Procedure Loading Page Group (PROC)
Departure Loading
AFCS
Arrival Loading
APPENDICES
ADDITIONAL
FEATURES
Approach Loading
Figure 1-27 Procedure Loading Pages
INDEX
Information on optional electronic checklist pages is offered later in this section. Checklist pages may be
accessed from most pages on the MFD using the CHKLIST Softkey.
34
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
MFD SYSTEM PAGES
FLIGHT
INSTRUMENTS
In the Auxiliary (AUX) Page Group, there are two system pages: System Setup and System Status. The System
Setup Page allows management of various system parameters, while the System Status Page displays the status
of all G1000 system LRUs.
SYSTEM SETUP PAGE
The System Setup Page allows management of the following system parameters:
• Time display format (local or UTC )
• Flight director format (only the single que option
is available)
• Baro transition alert (see Flight Instruments
Section)
• Page Navigation
• Airspace alerts
• GPS Course Deviation Indicator (CDI) range
• Arrival alert
• COM transceiver channel spacing
• Audio alert voice
• Displayed nearest airports
EIS
• Displayed measurement units
• MFD Data Bar (Navigation Status Box) fields
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Selecting the System Setup Page:
1) Turn the large FMS Knob to select the AUX Page group.
2) Turn the small FMS Knob to display the System Setup Page.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
Figure 1-28 System Setup Page
35
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
Restoring system setup defaults:
1) Use the FMS Knob to select the AUX - System Setup Page.
FLIGHT
INSTRUMENTS
2) Select the DFLTS Softkey.
Or:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the MENU Key.
3) Highlight ‘Restore Defaults’ and press the ENT Key.
EIS
Date/Time
AUDIO PANEL
& CNS
The Date/Time Box on the System Setup Page displays the current date and time and allows the pilot to set
the time format (local 12-hr, local 24-hr, or UTC) and offset. The time offset is used to define current local
time. UTC (also called GMT or Zulu) date and time are calculated directly from the GPS satellites signals
and cannot be changed. When using a local time format, designate the offset by adding or subtracting the
desired number of hours.
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
PFD
Figure 1-29 System Time (Local 24-hr Format)
ADDITIONAL
FEATURES
Set the system time format:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the time format field in the Date/Time Box.
APPENDICES
3) Turn the small FMS Knob to select the desired system time format (local 12hr, local 24hr, UTC) and press the
ENT Key.
Set the current time offset:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
INDEX
2) Turn the large FMS Knob to highlight the time offset field in the Date/Time Box.
3) Turn the FMS Knobs to enter the time offset and press the ENT Key.
36
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Figure 1-30 Date/Time Settings
(AUX - System Setup Page)
Display Units
FLIGHT
MANAGEMENT
The Display Units Box on the System Setup Page allows configuration of the measurement units used for
the following displayed data:
• Nav angle (magnetic, true)
When set to ‘MAGNETIC’, magnetic variation is figured into the displayed value. When ‘TRUE’ is
selected, no magnetic variation is calculated and a ‘T’ is displayed next to the value.
HAZARD
AVOIDANCE
Affects the BRG field in the PFD Navigation Status Box.
Affects Current Heading, Selected Heading, and Selected Course boxes on the PFD.
Affects the BRG, DTK, TKE, TRK, and XTK fields in the MFD Navigation Status Box.
• Distance and speed (metric, nautical)
AFCS
Affects the DIS field in the PFD Navigation Status Box and the range setting of the Inset Map.
Affects all distance and speed displays on the MFD with the exception of the displayed wind speed
displayed on the Navigation Map Page. Wind speed is affected on the Trip Planning Page.
ADDITIONAL
FEATURES
• Altitude and vertical speed (feet, meters)
Affects all altitude and elevation displays on the MFD, with the exception of VNAV altitudes on the
Active Flight Plan Page.
APPENDICES
• Temperature (Celsius, Fahrenheit)
Affects all temperature displays on the PFD.
Affects the temperature display on the Trip Planning Page. Does not affect the Engine Indicating
System display.
• Fuel and fuel flow (gallons, gallons/hour)
INDEX
Indicates fuel quantities are measured in gallons and fuel flow is measured in gallons per hour.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
37
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
• Weight (pounds, kilograms)
Affects aircraft weights on the Weight Planning Page.
FLIGHT
INSTRUMENTS
• Position (HDDD°MM.MM’, HDDD°MM’SS.S”)
Affects all position displays.
Change a Display Units setting:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
EIS
2) Turn the large FMS Knob to highlight the desired field in the Display Units Box.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
3) Turn the small FMS Knob to select from a list of measurement units and press the ENT Key when the desired
unit is highlighted. Press the CLR Key to cancel the action without changing the units.
Figure 1-31 Display Unit Settings (AUX - System Setup Page)
Airspace Alerts
AFCS
The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on
or off. This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries
depicted on the MFD Navigation Map Page. It simply turns on/off the warning provided when the aircraft
is approaching or near an airspace.
APPENDICES
ADDITIONAL
FEATURES
Alerts for the following airspaces can be turned on/off in the Airspace Alerts Box:
• Class B/TMA
• Restricted
• Class C/TCA
• MOA (Military)
• Class D
• Other airspaces
INDEX
An altitude buffer is also provided which “expands” the vertical range above or below an airspace. For
example, if the buffer is set at 500 feet, and the aircraft is more than 500 feet above/below an airspace, an
alert message is not generated, but if the aircraft is less than 500 feet above/below an airspace and projected
to enter it, the pilot is notified with an alert message. The default setting for the altitude buffer is 200
feet.
38
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
Change the altitude buffer distance setting:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the altitude buffer field in the Airspace Alerts Box.
FLIGHT
INSTRUMENTS
3) Turn the FMS Knobs to enter an altitude buffer value and press the ENT Key.
To turn an airspace alert on or off:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the desired field in the Airspace Alerts Box.
EIS
3) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF.
Audio Alerts
AUDIO PANEL
& CNS
The Audio Alert Box on the System Setup Page allows the audio alert voice to be set to male or female.
To change the audio alert voice:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
FLIGHT
MANAGEMENT
2) Turn the large FMS Knob to highlight the voice in the Audio Alert Box.
3) Turn the small FMS Knob to display and highlight the desired voice and press the ENT Key.
Flight Director
HAZARD
AVOIDANCE
Not pilot selectable.
Page Navigation
AFCS
The large FMS Knob displays the Page Group Tabs and navigates through the tabs. The small FMS Knob
navigates through the pages listed within a specific group. The number of clicks it takes to display the
Page Group Tabs and change to the next tab can be controlled from the Page Navigation box on the AUX
- System Setup Page.
OFF – Displays the Page Group Tabs with one click of either FMS Knob.
ON – Displays the Page Group Tabs and navigates to the next tab with one click of either FMS Knob.
ADDITIONAL
FEATURES
The pilot can select, from the AUX - System Setup Page, the amount of time the Page Group Tabs are
displayed (in the lower right corner of the MFD). The timeout can range from two to ten seconds.
Selecting page navigation settings:
APPENDICES
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the ‘Change On 1st Click’ field in the Page Navigation Box.
4) Turn the small FMS Knob to select ‘OFF’ or ‘ON’.
INDEX
5) Turn the large FMS Knob to highlight the ‘Timeout Seconds’ field in the Page navigation Box.
6) Turn the small FMS Knob to select the desired number of seconds
7) Press the FMS Knob momentarily to remove the flashing cursor.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
39
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
MFD Data Bar Fields
FLIGHT
INSTRUMENTS
The MFD Data Bar Fields Box on the System Setup Page displays the current configuration of the MFD
Navigation Status Box. By default, the Navigation Status Bar is set to display ground speed (GS), distance
to next waypoint (DIS), estimated time enroute (ETE), and enroute safe altitude (ESA).
Change the information shown in an MFD Navigation Status Bar field:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the desired field number in the MFD Data Bar Fields Box.
EIS
3) Turn the small FMS Knob to display and scroll through the data options list and press the ENT Key when the
desired data selection is highlighted.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
The following data may be selected for display in each of the four fields of the Navigation Status Box.
• Bearing (BRG)
• Fuel Over Destination (FOD)
• Crosstrack Error (XTK)
• Fuel On Board (FOB)
• Distance (DIS)
• Ground Speed (GS)
• Desired Track (DTK)
• Minimum Safe Altitude (MSA)
• Endurance (END)
• True Air Speed (TAS)
• En Route Safe Altitude (ESA)
• Track Angle Error (TKE)
• Estimated Time of Arrival (ETA)
• Track (TRK)
• Estimated Time En Route (ETE)
• Vertical Speed Required (VSR)
GPS CDI
ADDITIONAL
FEATURES
AFCS
The GPS CDI Box on the System Setup Page allows the pilot to define the range for the on-screen course
deviation indicator (CDI). The range values represent full range deflection for the CDI to either side. The
default setting is ‘AUTO’. At this setting, leaving the departure airport the CDI range is set to 1.0 nm and
gradually ramps up to 2 nm beyond 30 nm from the departure airport. The CDI range is set to 2.0 nautical
miles during the en route phase of flight. Within 30 nm of the destination airport, the CDI range gradually
ramps down to 1.0 nm (terminal area). During approach operations, the CDI range ramps down even
further to 0.3 nm. This transition normally occurs within 2.0 nm of the final approach fix (FAF).
APPENDICES
If a lower CDI range setting is selected (i.e., 1.0 or 0.3 nm), the higher range settings are not selected
during any phase of flight. For example, if 1.0 nm is selected, the system uses this for en route and terminal
phases and ramps down to 0.3 nm during an approach. Note that the Receiver Autonomous Integrity
Monitoring (RAIM) protection limits follow the selected CDI range and corresponding flight phases.
The GPS CDI Box on the System Setup Page displays the following:
• Selected CDI range (auto, 2 nm, 1 nm, 0.3 nm)
INDEX
• Current system CDI range (2 nm, 1 nm, 0.3 nm)
40
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
Changing the CDI range:
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the selected field in the GPS CDI Box.
FLIGHT
INSTRUMENTS
3) Turn the small FMS Knob to display and scroll through the range list and press the ENT Key when the desired
selection is highlighted.
4) Press the FMS Knob to deactivate the cursor.
COM Configuration
EIS
NOTE: 8.33 kHz VHF communication frequency channel spacing is not approved for use in the United States.
Select the 25.0 kHz channel spacing option for use in the United States.
AUDIO PANEL
& CNS
The COM Configuration Box on the System Setup Page allows the pilot to select 8.33 kHz or 25.0 kHz
COM frequency channel spacing.
Change COM channel spacing:
FLIGHT
MANAGEMENT
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the channel spacing field in the COM Configuration Box.
3) Turn the small FMS Knob to select the desired spacing and press the ENT Key.
Nearest Airports
HAZARD
AVOIDANCE
The Nearest Airports Box on the System Setup Page defines the minimum runway length and surface type
used when determining the nine nearest airports to display on the MFD Nearest Airports Page. A minimum
runway length and/or surface type can be entered to prevent airports with small runways or runways that
are not of appropriate surface from being displayed. Default settings are zero feet (or meters) for runway
length and “HARD/SOFT” for runway surface type.
AFCS
Select nearest airport surface matching criteria (any, hard only, hard/soft, water):
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
ADDITIONAL
FEATURES
2) Turn the large FMS Knob to highlight the runway surface field in the Nearest Airports Box.
3) Turn the small FMS Knob to display and scroll through the runway options (any, hard only, hard/soft, water) and
press the ENT Key when the desired selection is highlighted.
Select nearest airport minimum runway length matching criteria:
APPENDICES
1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.
2) Turn the large FMS Knob to highlight the minimum length field in the Nearest Airport Box.
3) Turn the FMS Knobs to enter the minimum runway length (zero to 99,999 feet) and press the ENT Key.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
41
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
SYSTEM STATUS PAGE
FLIGHT
INSTRUMENTS
The System Status Page displays the status and software version numbers for all detected system LRUs.
Pertinent information on all system databases is also displayed. Active LRUs are indicated by green check
marks and failed LRUs are indicated by red “X”s. Failed LRUs should be noted and a Cessna service center
or Garmin dealer informed.
Viewing LRU information:
1) Use the FMS Knob to select the AUX - System Status Page.
EIS
2) To place the cursor in the ‘LRU Info’ Box,
a) Select the LRU Softkey.
Or:
AUDIO PANEL
& CNS
a) Press the MENU Key.
b) With ‘Select LRU Window’ highlighted, press the ENT Key.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
3) Use the FMS Knob to scroll through the box to view LRU status information.
INDEX
Figure 1-32 Example AUX - System Status Page
42
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
Pertinent information on all system databases is also displayed on this page. Refer to the Appendices and
Additional Features sections for more information about databases.
Viewing database information:
FLIGHT
INSTRUMENTS
1) Select the AUX - System Status Page.
2) To place the cursor in the ‘MFD1 Database’ Box, select the MFD1 DB Softkey.
Or:
a) Press the MENU Key.
EIS
b) Highlight ‘Select Dbase Window’ and press the ENT Key.
3) Use the FMS Knob to scroll through the box to view database status information.
AUDIO PANEL
& CNS
The G1000 uses aural tones to convey the priority of airframe-specific alerts. The alerting system’s annunciation
tone may be tested from the System Status Page. Refer to the Appendices for airframe-specific alerts.
Testing the system annunciation tone:
1) Select the AUX - System Status Page.
FLIGHT
MANAGEMENT
2) Select the ANN TEST Softkey.
Or:
a) Press the MENU Key.
b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key.
HAZARD
AVOIDANCE
SYSTEM UTILITIES
AFCS
For flight planning purposes, timers, trip statistics, and a scheduler feature are provided on the AUX - Utility
Page. The timers available include a stopwatch-like generic timer, a total time in flight timer, and a record of the
time of departure. Trip statistics—odometer, trip odometer, and average trip and maximum groundspeeds—are
displayed from the time of the last reset. A scheduler feature is also provided so the pilot can enter reminder
messages to be displayed at specified intervals in the Alerts Window on the PFD (see the Additional Features
Section).
ADDITIONAL
FEATURES
Timers
APPENDICES
The generic timer can be set to count up or down from a specified time (HH:MM:SS). When the
countdown on the timer reaches zero the digits begin to count up from zero. If the timer is reset before
reaching zero on a countdown, the digits are reset to the initial value. If the timer is counting up when
reset, the timer digits return to zero.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
43
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
Setting the generic timer (PFD):
1) Select the TMR/REF Softkey.
FLIGHT
INSTRUMENTS
2) Turn the large FMS Knob to select the timer field (hh/mm/ss).
3) Use the FMS Knob to enter the desired time and press the ENT Key.
4) With the UP/DN field highlighted, turn the small FMS Knob to select the timer counting direction.
5) Press the ENT Key.
6) With ‘START?’ highlighted, press the ENT Key to start the timer. The field changes to ‘STOP?’.
EIS
7) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’.
8) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the
digits are reset.
AUDIO PANEL
& CNS
9) To remove the window, press the CLR Key or select the TMR/REF Softkey.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
PFD
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 1-33 Generic Timer
(Timer/References Window)
44
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
Setting the generic timer (MFD AUX - Utility Page):
1) Select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
FLIGHT
INSTRUMENTS
3) Turn the small FMS Knob to select the timer counting direction (UP/DN) and press the ENT Key.
4) Use the FMS Knob to enter the desired time and press the ENT Key.
5) With ‘START?’ highlighted, press the ENT Key to start the timer. The field changes to ‘STOP?’.
6) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’.
EIS
7) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the
digits are reset.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 1-34 Timers (AUX - Utility Page)
The flight timer can be set to count up from zero starting at system power-up or from the time the aircraft
lifts off; the timer can also be reset to zero at any time.
AFCS
Setting the flight timer starting criterion:
1) Select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
ADDITIONAL
FEATURES
3) Turn the large FMS Knob to highlight the field next to the flight timer.
4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and press the ENT Key.
Resetting the flight timer:
APPENDICES
1) Select the AUX - Utility Page.
2) Press the MENU Key.
3) With ‘Reset Flight Timer’ highlighted, press the ENT Key.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
45
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
FLIGHT
INSTRUMENTS
The G1000 records the time at which departure occurs, depending on whether the pilot prefers the time
to be recorded from system power-up or from aircraft lift off. The displayed departure time can also be reset
to display the current time at the point of reset. The format in which the time is displayed is controlled
from the System Setup Page.
Setting the departure timer starting criterion:
1) Use the FMS Knob to select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the field next to the departure time.
EIS
4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and press the ENT Key.
Resetting the departure time:
AUDIO PANEL
& CNS
1) Use the FMS Knob to select the AUX - Utility Page.
2) Press the MENU Key.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
3) Use the FMS Knob to highlight ‘Reset Departure Time’ and press the ENT Key.
46
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
1.8 DISPLAY BACKLIGHTING
FLIGHT
INSTRUMENTS
The backlighting of the PFD and MFD displays and bezel and Audio Panel keys can be adjusted automatically
or manually.
AUTOMATIC ADJUSTMENT
EIS
The existing instrument panel dimmer bus normally controls the PFD and MFD backlighting as well as the
PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and audio panel key annunciator lighting. When
the dimmer bus is not used by the G1000 system, photocell technology automatically controls backlighting
adjustments. Photocell calibration curves are pre-configured to optimize display appearance through a broad
range of cockpit lighting conditions.
MANUAL ADJUSTMENT
AUDIO PANEL
& CNS
NOTE: In normal mode, backlighting can only be adjusted from the PFD. In reversionary mode, it can also
be adjusted from the MFD.
FLIGHT
MANAGEMENT
NOTE: No other window can be displayed on the PFD while the PFD Setup Menu Window is displayed.
Adjusting display backlighting:
1) Press the PFD MENU Key to display the PFD Setup Menu. ‘AUTO’ is now highlighted next to ‘PFD DSPL’.
HAZARD
AVOIDANCE
2) Turn the small FMS Knob to select ‘MANUAL’.
3) Press the ENT Key.
4) With the intensity value now highlighted, enter the desired backlighting then press the ENT Key.
5) Turn the large FMS Knob to highlight ‘AUTO’ next to ‘MFD DSPL’ and repeat steps 2-4.
AFCS
6) To remove the menu, press the CLR or MENU Key.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
47
SYSTEM
OVERVIEW
SYSTEM OVERVIEW
Adjusting key backlighting:
1) Press the PFD MENU Key to display the PFD Setup Menu. ‘AUTO’ is now highlighted next to ‘PFD DSPL’.
FLIGHT
INSTRUMENTS
2) Turn the large FMS Knob to highlight ‘PFD DSPL’.
3) Turn the small FMS Knob in the direction of the green arrowhead to display ‘PFD KEY’.
4) Turn the large FMS Knob to highlight ‘AUTO’.
5) Turn the small FMS Knob to select ‘MANUAL’.
6) Press the ENT Key.
EIS
7) With the intensity value now highlighted, enter the desired backlighting and press the ENT Key.
8) Turn the large FMS Knob to highlight ‘MFD DSPL’.
AUDIO PANEL
& CNS
9) Turn the small FMS Knob in the direction of the green arrowhead to display ‘MFD KEY’ and repeat steps 4-7.
10) To remove the menu, press the CLR or MENU Key.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
PFD
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 1-35 PFD Setup Menu
48
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
SECTION 2 FLIGHT INSTRUMENTS
FLIGHT
INSTRUMENTS
WARNING: In the event that the airspeed, attitude, altitude, or heading indications become unusable, refer
to the backup instruments.
NOTE: The Automatic Flight Control System (AFCS) provides additional readouts and bugs on selected flight
instruments. Refer to the AFCS Section for details on these bugs and readouts, as they appear on the display
during certain AFCS modes.
EIS
AUDIO PANEL
& CNS
Increased situational awareness is provided by replacing the traditional instrument on the panel with an easyto-scan Primary Flight Display (PFD) that features a large horizon, airspeed, attitude, altitude, vertical speed, and
course deviation information. In addition to the flight instruments, navigation, communication, terrain, traffic,
and weather information are also presented on the PFD and explained in other sections of this Pilot’s Guide.
The following flight instruments and supplemental flight data are displayed on the PFD:
• Airspeed Indicator, showing
– True airspeed
• Vertical Speed Indicator (VSI)
– Generic timer
– Airspeed awareness ranges
• Vertical Navigation (VNV)
Indications
– Vspeed values
– Trend vector
• Attitude Indicator with slip/skid
indication
• Altimeter, showing
• Horizontal Situation Indicator,
showing
– Turn Rate Indicator
– Course Deviation Indicator
(CDI)
– Barometric Minimum Descent
Altitude (MDA)
• Transponder Mode, Code, and
Ident/Reply
• Outside Air Temperature (OAT)
– Reference altitude
– Navigation source
• Wind data
AFCS
– Trend vector
– Bearing pointers and
information windows
• Deviation from International
Standard Atmosphere (ISA)
Temperature
– Barometric setting
HAZARD
AVOIDANCE
– Vspeed reference flags
• Timer/References Window,
showing
FLIGHT
MANAGEMENT
– Indicated airspeed
• Vertical Deviation, Glideslope,
and Glidepath Indicators
ADDITIONAL
FEATURES
The PFD also displays various alerts and annunciations.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
49
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
FLIGHT
INSTRUMENTS
22
21
20
19
1
18
17
16
2
EIS
15
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
14
3
13
4
12
5
11
6
10
7
9
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
8
1
NAV Frequency Box
12
Turn Rate Indicator
2
Airspeed Indicator
13
Altimeter Barometric Setting
3
True Airspeed
14
Vertical Speed Indicator (VSI)
4
Current Heading
15
Selected Altitude Bug
5
Horizontal Situation Indicator ( HSI)
16
Altimeter
6
Outside Air Temperature (OAT)
17
Selected Altitude
7
ISA Temperature Deviation
18
COM Frequency Box
8
Softkeys
19
AFCS Status Box
9
System Time
20
Navigation Status Box
10
Transponder Data Box
21
Slip/Skid Indicator
11
Selected Heading Bug
22
Attitude Indicator
INDEX
Figure 2-1 Primary Flight Display (Default)
50
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
15
14
FLIGHT
INSTRUMENTS
1
13
12
EIS
2
3
11
5
AUDIO PANEL
& CNS
10
4
9
FLIGHT
MANAGEMENT
6
7
8
Flight Plan Window
2
Vspeed References
10
Annunciation Window
3
Selected Heading
11
Selected Course
4
Wind Data
12
Glideslope Indicator
5
Inset Map
13
Marker Beacon Annunciation
6
DME Information Window
14
Terrain Annunciation
7
Bearing Information Windows
15
AFCS Status Annunciation
8
Barometric Minimum Descent Altitude
ADDITIONAL
FEATURES
9
AFCS
Traffic Annunciation
HAZARD
AVOIDANCE
1
Figure 2-2 Additional PFD Information
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
51
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
2.1 FLIGHT INSTRUMENTS
FLIGHT
INSTRUMENTS
AIRSPEED INDICATOR
NOTE: Refer to the Airplane Flight Manual (AFM) for speed criteria.
AUDIO PANEL
& CNS
EIS
The Airspeed Indicator displays airspeed on a moving tape rolling number gauge. The true airspeed is
displayed in knots below the Airspeed Indicator. The numeric labels and major tick marks on the moving tape
are marked at intervals of 10 knots. The minor tick marks on the moving tape are indicated at intervals of
five knots. Speed indication starts at 20 knots, with 60 knots of airspeed viewable at any time. The indicated
airspeed is displayed inside the black pointer. The pointer remains black until reaching never-exceed speed
(VNE), at which point it turns red.
FLIGHT
MANAGEMENT
Airspeed
Trend
Vector
Vspeed
References
Actual
Airspeed
HAZARD
AVOIDANCE
Speed
Ranges
Figure 2-4 Red Pointer at VNE
True
Airspeed
Figure 2-3 Airspeed Indicator
AFCS
A color-coded (white, green, yellow, and red) speed range strip is located on the moving tape. The colors
denote flaps operating range, normal operating range, caution range, and never-exceed speed (VNE). A red range
is also present for low speed awareness.
INDEX
APPENDICES
ADDITIONAL
FEATURES
The Airspeed Trend Vector is a vertical, magenta line that appears to the right of the color-coded speed
range strip when airspeed is either accelerating or decelerating. One end of the magenta line is anchored to
the tip of the airspeed pointer while the other end moves continuously up or down corresponding to the rate
of acceleration or deceleration. For any constant rate of acceleration or deceleration, the moving end of the
line shows approximately what the indicated airspeed value will be in six seconds. If the trend vector crosses
VNE, the text of the actual airspeed readout changes to yellow. The trend vector is absent if the speed remains
constant or if any data needed to calculate airspeed is not available due to a system failure.
52
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
Vspeeds (Glide, VX, and VY) can be changed and their flags turned on/off from the Timer/References Window. When active (on), the Vspeeds are displayed at their respective locations to the right of the airspeed scale. All
Vspeed values are reset and all flags turned off when power is cycled.
FLIGHT
INSTRUMENTS
Changing Vspeeds and turning Vspeed flags on/off:
1) Select the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to enter the desired value. When a speed has been changed from a default value, an
asterisk appears next to the speed.
EIS
4) Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field.
5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
FLIGHT
MANAGEMENT
Figure 2-5 Timer/References Window (Corvalis)
AUDIO PANEL
& CNS
6) To remove the window, press the CLR Key or the TMR/REF Softkey.
Figure 2-6 Timer/References Menu
HAZARD
AVOIDANCE
Turning all Vspeed flags on/off:
1) Select the TMR/REF Softkey.
2) Press the MENU Key.
AFCS
3) To activate all Vspeed flags, highlight ‘All References On’ and press the ENT Key.
4) To remove all Vspeed flags, turn the FMS Knob to highlight ‘All References Off’ and press the ENT Key.
Restoring all Vspeed defaults:
ADDITIONAL
FEATURES
1) Select the TMR/REF Softkey.
2) Press the MENU Key.
3) Turn the FMS Knob to highlight ‘Restore Defaults’ and press the ENT Key.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
53
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
ATTITUDE INDICATOR
FLIGHT
INSTRUMENTS
Attitude information is displayed over a virtual blue sky and brown ground with a white horizon line. The
Attitude Indicator displays the pitch, roll, and slip/skid information.
9
8
1
7
EIS
2
6
AUDIO PANEL
& CNS
3
4
5
1
Roll Pointer
2
Roll Scale
3
Horizon Line
4
Aircraft Symbol
5
Land Representation
6
Pitch Scale
7
Slip/Skid Indicator
8
Sky Representation
9
Roll Scale Zero
FLIGHT
MANAGEMENT
Figure 2-7 Attitude Indicator
HAZARD
AVOIDANCE
The horizon line is part of the pitch scale. Above and below the horizon line, major pitch marks and numeric
labels are shown for every 10˚, up to 80˚. Minor pitch marks are shown for intervening 5˚ increments, up to
25˚ below and 45˚ above the horizon line. Between 20˚ below to 20˚ above the horizon line, minor pitch marks
occur every 2.5˚. When the Synthetic Vision System (optional) is activated, the pitch scale is reduced to 10˚ up
and 7.5˚ down; refer to the Additional Features section.
The inverted white triangle indicates zero on the roll scale. Major tick marks at 30˚ and 60˚ and minor tick
marks at 10˚, 20˚, and 45˚ are shown to the left and right of the zero. Angle of bank is indicated by the position
of the pointer on the roll scale.
APPENDICES
ADDITIONAL
FEATURES
AFCS
The Slip/Skid Indicator is the bar beneath the roll pointer. The indicator bar moves with the roll pointer and
moves laterally away from the pointer to indicate uncoordinated flight. Slip (inside the turn) or skid (outside
the turn) is indicated by the location of the bar relative to the pointer. One bar displacement is equal to one ball
displacement on a traditional Slip/Skid Indicator.
INDEX
Figure 2-8 Slip/Skid Indication
54
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
ALTIMETER
FLIGHT
INSTRUMENTS
The Altimeter displays 600 feet of barometric altitude values at a time on a moving tape rolling number gauge. Numeric labels and major tick marks are shown at intervals of 100 feet. Minor tick marks are at intervals of 20
feet. The current altitude is displayed in the black pointer.
The Selected Altitude is displayed above the Altimeter in the box indicated by a selection bug symbol. A bug
corresponding to this altitude is shown on the tape. If the Selected Altitude exceeds the range shown on the
tape, the bug appears at the corresponding edge of the tape. When the metric value is selected it is displayed
in a separate box above the Selected Altitude.
EIS
A magenta Altitude Trend Vector extends up or down the left of the altitude tape, the end resting at the
approximate altitude to be reached in 6 seconds at the current vertical speed. The trend vector is not shown if
altitude remains constant or if data needed for calculation is not available due to a system failure.
Turn the ALT Knob to set the Selected Altitude. The large knob adjusts the Selected Altitude in 1000-ft increments,
the small knob in 100-ft increments. If the altimeter is set to display meters, the large knob adjusts the Selected
Altitude in 500-meter increments, the small knob in 50-meter increments.
If set, the Minimum Descent Altitude/Decision Height (MDA/DH) value is also available for the Selected
altitude.
Selected
Altitude
Selected
Altitude
(Meters)
HAZARD
AVOIDANCE
Selected
Altitude
Bug
Altitude
Trend
Vector
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Setting the Selected Altitude:
Current
Altitude
(Meters)
Current
Altitude
AFCS
Barometric
Setting
Figure 2-9 Altimeter
ADDITIONAL
FEATURES
MDA/DH
Bug
Barometric
Setting Box
(Hectopascals)
Figure 2-10 Altimeter (Metric)
APPENDICES
Altitudes can also be displayed in meters (Figure 2-10). Note that the altitude tape does not change scale.
Displaying altitude in meters:
1) Select the PFD Softkey to display the second-level softkeys.
INDEX
2) Select the ALT UNIT Softkey.
3) Select the METERS Softkey to turn on metric altitude readouts.
4) Select the BACK Softkey to return to the top-level softkeys.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
55
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
FLIGHT
INSTRUMENTS
The barometric pressure setting is displayed below the Altimeter in inches of mercury (in Hg) or hectopascals
(hPa) when metric units are selected. Adjusting the altimeter barometric setting creates discontinuities in VNV
vertical deviation, moving the descent path. For large adjustments, it may take several minutes for the aircraft
to re-establish on the descent path. If the change is made while nearing a waypoint with a VNV Target Altitude,
the aircraft may not re-establish on the descent path in time to meet the vertical constraint.
Selecting the altimeter barometric pressure setting:
Turn the BARO Knob to select the desired setting.
Selecting standard barometric pressure:
EIS
1) Select the PFD Softkey to display the second-level softkeys.
AUDIO PANEL
& CNS
2) Select the STD BARO Softkey; STD BARO is displayed in barometric setting box.
FLIGHT
MANAGEMENT
Figure 2-11 Standard Barometric Altimeter Setting
Changing altimeter barometric pressure setting units:
1) Select the PFD Softkey to display the second-level softkeys.
2) Select the ALT UNIT Softkey.
HAZARD
AVOIDANCE
3) Select the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg).
Or, select the HPA Softkey to display the barometric pressure setting in hectopascals (hPa; see Figure 2-10).
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
4) Select the BACK Softkey to return to the top-level softkeys.
56
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
A Baro Transition Alert is provided to alert the pilot to change the barometric pressure setting when crossing
the transition altitude in either direction. This is displayed by the flashing light blue barometric pressure setting
when crossing the transition altitude.
FLIGHT
INSTRUMENTS
Setting the Baro Transition Alert:
1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight Altitude in the Baro Transition Alert box.
4) Turn the small FMS Knob to turn the alert OFF or ON and press the ENT Key.
EIS
5) Turn the small FMS Knob to change the altitude and press the ENT Key.
6) To cancel the selection, press the FMS Knob.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
Figure 2-12 Baro Transition Alert
(AUX - System Setup Page)
ADDITIONAL
FEATURES
VERTICAL SPEED INDICATOR (VSI)
APPENDICES
The Vertical Speed Indicator (VSI) displays the aircraft vertical speed on a fixed scale with labels at 1000 and
2000 fpm and minor tick marks every 500 fpm (Figure 2-13). Digits appear in the pointer when the climb or
descent rate is greater than 100 fpm. If the rate of ascent/descent exceeds 2000 fpm, the pointer appears at the
corresponding edge of the tape and the rate appears inside the pointer.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
A magenta chevron is displayed as the Required Vertical Speed Indication (RVSI) for reaching a VNV Target
Altitude once the “TOD [Top of Descent] within 1 minute” alert has been generated. See the Flight Management
Section for details on VNV features, and refer to Section 2.2, Supplemental Flight Data, for more information
about VNV indications on the PFD.
57
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
VERTICAL DEVIATION
NOTE: The Glidepath Indicator is only shown for aircraft with GIA 63W Integrated Avionics Units when SBAS
FLIGHT
INSTRUMENTS
is available.
EIS
The Vertical Deviation Indicator (VDI) is a magenta chevron indicating the baro-VNV vertical deviation when
Vertical Navigation (VNV) is being used (Figure 2-13). The VDI appears in conjunction with the “TOD within
1 minute” alert. The VDI is removed from the display if vertical deviation becomes invalid. See the Flight
Management Section for details on VNV features, and refer to Section 2.2, Supplemental Flight Data, for more
information about VNV indications on the PFD.
AUDIO PANEL
& CNS
The Glideslope Indicator (Figure 2-14) appears to the left of the Altimeter whenever an ILS frequency is
tuned in the active NAV field. A green diamond acts as the Glideslope Indicator, like a glideslope needle on
a conventional indicator. If a localizer frequency is tuned and there is no glideslope, “NO GS” is displayed in
place of the diamond.
FLIGHT
MANAGEMENT
The glidepath is analogous to the glideslope for GPS approaches supporting SBAS vertical guidance (LNAV+V,
L/VNV, LPV). When an approach of this type is loaded into the flight plan and GPS is the selected navigation
source, the Glidepath Indicator (Figure 2-15) appears as a magenta diamond. If the approach type downgrades
past the final approach fix (FAF), “NO GP” is displayed in place of the diamond.
Full-scale deflection (two dots) is 1000 feet.
HAZARD
AVOIDANCE
VNV Target
Altitude
Vertical
Speed
Indicator
AFCS
Vertical
Deviation
Indicator
ADDITIONAL
FEATURES
Required
Vertical
Speed
Indicator
Glideslope
Indicator
Vertical
Speed
Pointer
Figure 2-13 Vertical Speed and
Deviation Indicators (VSI and VDI)
Figure 2-14 Glideslope Indicator
Figure 2-15 Glidepath Indicator
INDEX
APPENDICES
Glidepath
Indicator
58
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
HORIZONTAL SITUATION INDICATOR (HSI)
FLIGHT
INSTRUMENTS
The Horizontal Situation Indicator (HSI) displays a rotating compass card in a heading-up orientation. Letters
indicate the cardinal points and numeric labels occur every 30˚. Major tick marks are at 10˚ intervals and minor
tick marks at 5˚ intervals. A digital reading of the current heading appears on top of the HSI, and the current
track is represented on the HSI by a magenta diamond. The HSI also presents turn rate, course deviation,
bearing, and navigation source information. The HSI is available in two formats, a 360˚ compass rose and a
140˚ arc.
Changing the HSI display format:
EIS
1) Select the PFD Softkey.
2) Select the HSI FRMT Softkey.
3) Select the 360 HSI or ARC HSI Softkey.
AUDIO PANEL
& CNS
The 360˚ HSI contains a Course Deviation Indicator (CDI), with a Course Pointer, To/From Indicator, and a
sliding deviation bar and scale. The course pointer is a single line arrow (GPS, VOR1, and LOC1) or a double
line arrow (VOR2 and LOC2) which points in the direction of the set course. The To/From arrow rotates with
the course pointer and is displayed when the active NAVAID is received.
16
FLIGHT
MANAGEMENT
17
15
1
14
2
4
13
5
12
6
11
HAZARD
AVOIDANCE
3
10
AFCS
7
9
8
To/From Indicator
2
Selected Heading
11
Heading Bug
3
Current Track Indicator
12
Course Pointer
4
Lateral Deviation Scale
13
Flight Phase
5
Navigation Source
14
Selected Course
6
Aircraft Symbol
15
Turn Rate and Heading Trend Vector
7
Course Deviation Indicator (CDI)
16
Current Heading
8
Rotating Compass Card
17
Lubber Line
9
OBS Mode Active
INDEX
10
APPENDICES
Turn Rate Indicator
ADDITIONAL
FEATURES
1
Figure 2-16 Horizontal Situation Indicator (360˚ HSI)
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
59
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
FLIGHT
INSTRUMENTS
The Arc HSI is a 140˚ expanded section of the compass rose. The Arc HSI contains a Course Pointer,
combined To/From Indicator and a sliding deviation indicator, and a deviation scale. Upon station passage, the
To/From Indicator flips and points to the tail of the aircraft, just like a conventional To/From flag. Depending
on the navigation source, the CDI on the Arc HSI can appear in two different ways, an arrowhead (GPS, VOR,
OBS) or a diamond (LOC).
Course Pointer
Flight Phase
Annunciation
Lateral
Deviation
Scale
Course
Deviation
and To/From
Indicator
AUDIO PANEL
& CNS
EIS
Navigation
Source
Figure 2-17 Arc HSI
FLIGHT
MANAGEMENT
The Selected Heading is shown to the upper left of the HSI and is displayed in light blue. The light blue
heading bug on the compass rose corresponds to the selected heading.
Adjusting the selected heading:
Turn the HDG Knob to set the selected heading.
Press the HDG Knob to synchronize the bug to the current heading.
HAZARD
AVOIDANCE
The Selected Course is shown to the upper right of the HSI. The color of the Selected Course corresponds to
the selected navigation source: magenta for GPS or green for NAV (VOR, LOC).
Adjusting the Selected Course:
Turn the CRS Knob to set the Selected Course.
AFCS
Press the CRS Knob to re-center the CDI and return the course pointer to the bearing of the active waypoint or
navigation station (see OBS Mode for adjusting a GPS course).
ADDITIONAL
FEATURES
Current Heading
Heading Bug
APPENDICES
Selected
Heading
Selected
Course
INDEX
Figure 2-18 Heading and Course Indications (Magnetic)
60
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
Navigation angles (track, heading, course, bearing) are corrected to the computed magnetic variation (‘Mag
Var’) or referenced to true north (denoted ‘T’), set on the AUX - System Setup Page. When an approach
referenced to true north has been loaded into the flight plan, the system generates a message to change the
navigation angle setting to ‘True’ at the appropriate time.
FLIGHT
INSTRUMENTS
EIS
Figure 2-19 Heading and Course Indications (True)
Changing the navigation angle setting:
AUDIO PANEL
& CNS
1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight ‘Nav Angle’ in the ‘Display Units’ box.
FLIGHT
MANAGEMENT
4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key.
• TRUE - References angles to true north (denoted with ‘T’)
• MAGNETIC - Angles corrected to the computed magnetic variation (‘Mag Var’)
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
Figure 2-20 Navigation Angle Settings
(AUX - System Setup Page)
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
61
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
TURN RATE INDICATOR
FLIGHT
INSTRUMENTS
The Turn Rate Indicator is located directly above the rotating compass card. Tick marks to the left and right
of the lubber line denote half-standard and standard turn rates. A magenta Turn Rate Trend Vector shows the
current turn rate. The end of the trend vector gives the heading predicted in 6 seconds, based on the present
turn rate. A standard-rate turn is shown on the indicator by the trend vector stopping at the standard turn
rate tick mark, corresponding to a predicted heading of 18˚ from the current heading. At rates greater than 4
deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.
EIS
Half-standard
Turn Rate
Arrow Shown
for Turn Rate
> 4 deg/sec
AUDIO PANEL
& CNS
Standard
Turn Rate
Figure 2-21 Turn Rate Indicator and Trend Vector
BEARING POINTERS AND INFORMATION WINDOWS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Two bearing pointers and associated information can be displayed on the HSI for NAV, GPS, and ADF
sources by pressing the PFD Softkey then a BRG or DME Softkey. The bearing pointers are light blue and are
single-line (BRG1) or double-line (BRG2). A pointer symbol is shown in the information windows to indicate
the navigation source. The bearing pointers never override the CDI and are visually separated from the CDI
by a white ring. Bearing pointers may be selected but not necessarily visible due to data unavailability. When
the Arc HSI is displayed, the Bearing Information windows and pointers are disabled.
NOTE: ADF radio installation is optional.
AFCS
Tuning Mode
Frequency
Bearing 1
Pointer
Bearing 2
Pointer
ADDITIONAL
FEATURES
Distance
APPENDICES
Distance to
Bearing Source
Station
Identifier
ADF
Frequency
Bearing Source Pointer 1
Pointer 2
Bearing 1 Information Window
Bearing Source
Bearing 2 Information Window
INDEX
Figure 2-22 HSI with Bearing and Distance Information
62
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
When a bearing pointer is displayed, its associated information window is also displayed. The Bearing
Information windows (Figure 2-22) are displayed to the lower sides of the HSI and display the following
information:
• Station/waypoint identifier (NAV, GPS)
• Pointer icon (BRG1 = single line, BRG2 = double line)
• GPS-derived great circle distance to bearing
source
• Frequency (NAV, ADF)
FLIGHT
INSTRUMENTS
• Bearing source (NAV, GPS, ADF)
EIS
When the NAV radio is tuned to an ILS frequency the bearing source and the bearing pointer is removed
from the HSI. When NAV1 or NAV2 is the selected bearing source, the frequency is replaced by the station
identifier when the station is within range. If GPS is the bearing source, the active waypoint identifier is
displayed in lieu of a frequency.
AUDIO PANEL
& CNS
The bearing pointer is removed from the HSI and “NO DATA” is displayed in the information window if
the NAV radio is not receiving the tuned VOR station or if GPS is the bearing source and an active waypoint
is not selected.
Selecting bearing display and changing sources:
1) Select the PFD Softkey.
FLIGHT
MANAGEMENT
2) Select a BRG Softkey to display the desired bearing pointer and information window with a NAV source.
3) Select the BRG Softkey again to change the bearing source to GPS.
4) To remove the bearing pointer and information window, select the BRG Softkey again.
HAZARD
AVOIDANCE
DME INFORMATION WINDOW
The DME Information Window is displayed above the BRG1 Information Window on the 360˚ HSI and in
a box above and along side the Arc HSI. It shows the DME label, tuning mode (NAV1, NAV2, or HOLD),
frequency, and distance. When a signal is invalid, the distance is replaced by –.– – NM Refer to the Audio
Panel and CNS Section for information on tuning the DME.
AFCS
NOTE: DME installation is optional.
Displaying the DME Information Window:
ADDITIONAL
FEATURES
1) Select the PFD Softkey.
2) Select the DME Softkey to display the DME Information Window.
3) To remove the DME Information Window, select the DME Softkey again.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
63
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
COURSE DEVIATION INDICATOR (CDI)
NOTE: During a heading change of greater than 105˚ with respect to the course, the CDI on the Arc HSI
FLIGHT
INSTRUMENTS
switches to the opposite side of the deviation scale and displays reverse sensing.
The Course Deviation Indicator (CDI) moves left or right from the course pointer along a lateral deviation
scale to display aircraft position relative to the course. If the course deviation data is not valid, the CDI is not
displayed.
EIS
360º HSI
AUDIO PANEL
& CNS
Navigation
Source
Flight
Phase
Arc HSI
Navigation
Source
Flight
Phase
CDI
CDI
Scale
Scale
FLIGHT
MANAGEMENT
Crosstrack
Error
CDI
HAZARD
AVOIDANCE
Figure 2-23 Course Deviation Indicator
APPENDICES
ADDITIONAL
FEATURES
AFCS
The CDI can display two sources of navigation, GPS or VOR/LOC. Color indicates the current navigation
source, magenta for GPS and green for VOR and LOC. The full scale limits for the CDI are defined by a GPSderived distance when coupled to GPS. When navigating using a VOR or localizer (LOC), the CDI uses the
same angular limits as a mechanical CDI. If the CDI exceeds the maximum deviation on the scale (two dots)
while navigating with GPS, the crosstrack error (XTK) is displayed below the white aircraft symbol.
INDEX
Figure 2-24 Navigation Sources
64
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
Changing navigation sources:
1) Select the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the
NAV1 standby frequency in the upper left corner of the PFD.
FLIGHT
INSTRUMENTS
2) Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning
box over the NAV2 standby frequency.
3) Select the CDI Softkey a third time to return to GPS.
NAV2 Selected for Tuning
NAV1 Selected for Tuning
EIS
LOC1
Selected
VOR2
Selected
AUDIO PANEL
& CNS
GPS
Selected
FLIGHT
MANAGEMENT
Selecting the CDI Softkey
Cycles through
Navigation Sources
Figure 2-25 Selecting a Navigation Source
HAZARD
AVOIDANCE
The system automatically switches from GPS to LOC navigation source and changes the CDI scaling accordingly
when all of the following occur:
• A localizer or ILS approach has been loaded into the active flight plan
• The final approach fix (FAF) is the active waypoint, the FAF is less than 15 nm away, and the aircraft is moving
toward the FAF
AFCS
• A valid localizer frequency has been tuned
• The GPS CDI deviation is less than 1.2 times full-scale deflection
ADDITIONAL
FEATURES
GPS steering guidance is still provided after the CDI automatically switches to LOC until LOC capture, up
to the Final Approach Fix (FAF) for an ILS approach, or until GPS information becomes invalid. Activating a
Vector-to-Final (VTF) also causes the CDI to switch to LOC navigation source. GPS steering guidance is not
provided after this switch.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
65
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
GPS CDI SCALING
FLIGHT
INSTRUMENTS
When GPS is the selected navigation source, the flight plan legs are sequenced automatically and
annunciations appear on the HSI for the flight phase. Flight phase annunciations are normally shown in
magenta, but when cautionary conditions exist the color changes to yellow. If the current leg in the flight plan
is a heading leg, ‘HDG LEG’ is annunciated in magenta beneath the aircraft symbol.
EIS
The current GPS CDI scale setting is displayed as ‘System CDI’ on the AUX - System Setup Page and the fullscale deflection setting may also be changed (2.0 nm, 1.0 nm, 0.3 nm, or Auto) from this page. If the selected
scaling is smaller than the automatic setting for enroute and terminal phases, the CDI is scaled accordingly
and the selected setting is be displayed rather than the flight phase annunciation.
Changing the selected GPS CDI setting:
1) Use the FMS Knob to select the AUX - System Setup Page on the MFD.
AUDIO PANEL
& CNS
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight ‘Selected’ in the ‘GPS CDI’ box.
4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key.
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
5) To cancel the selection, press the FMS Knob or the CLR Key.
APPENDICES
Figure 2-26 GPS CDI Settings
(AUX - System Setup Page)
INDEX
When set to ‘Auto’ (default), the GPS CDI scale automatically adjusts to the desired limits based upon the
current phase of flight (Figure 2-27, Table 2-1).
66
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
Enroute
(Oceanic if >200 nm
from nearest airport)
Terminal
Approach
0.3 nm
1.0 nm
1.0 nm
2.0 nm
0.3 nm
1.0 nm
Terminal
FLIGHT
INSTRUMENTS
CDI Full-scale Deflection
SYSTEM
OVERVIEW
Departure
Refer to accompanying
approach CDI scaling figures
Missed
Approach
EIS
Figure 2-27 Automatic CDI Scaling
AUDIO PANEL
& CNS
• Once a departure procedure is activated, the CDI is scaled for departure (0.3 nm).
• The system switches from departure to terminal CDI scaling (1.0 nm) under the following conditions:
- The next leg in the procedure is not aligned with the departure runway
FLIGHT
MANAGEMENT
- The next leg in the departure procedure is not CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF (see
Glossary for leg type definitions)
- After any leg in the departure procedure that is not CA or FA
HAZARD
AVOIDANCE
• At 30 nm from the departure airport the enroute phase of flight is automatically entered and CDI scaling
changes to 2.0 nm over a distance of 1.0 nm, except under the following conditions:
- When navigating with an active departure procedure, the flight phase and CDI scale does not change
until the aircraft arrives at the last departure waypoint (if more than 30 nm from the departure airport) or
the leg after the last departure waypoint has been activated or a direct-to waypoint is activated.
AFCS
• If after completing the departure procedure the nearest airport is more than 200 nm away from the aircraft
and the approach procedure has not yet commenced, the CDI is scaled for oceanic flight (2.0 nm).
• Within 31 nm of the destination airport (terminal area), the CDI scale gradually ramps down from 2.0 nm
to 1.0 nm over a distance of 1.0 nm, except under the following conditions:
ADDITIONAL
FEATURES
- Upon reaching the first waypoint of an arrival route that is more than 31 nm from the destination airport,
the flight phase changes to terminal and the CDI scale begins to transition down from 2.0 nm to 1.0 nm
over a distance of 1.0 nm.
APPENDICES
• During approach, the CDI scale ramps down even further (see Figures 2-28 and 2-29). This transition
normally occurs within 2.0 nm of the final approach fix (FAF). The CDI switches to approach scaling
automatically once the approach procedure is activated or if Vector-to-Final (VTF) is selected.
- If the active waypoint is the FAF, the ground track and the bearing to the FAF must be within 45° of the
final approach segment course.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
- If the active waypoint is part of the missed approach procedure, the active leg and preceding missed
approach legs must be aligned with the final approach segment course and the aircraft must not have
passed the turn initiation point.
67
2 nm
FAF
CDI scale varies if VTF is activated
0.3 nm
1.0 nm
2 nm
FAF
EIS
angle based
on database
information
course width
angle set
by system
CDI Full-scale Deflection
0.3 nm
1.0 nm
CDI scale is set to the smaller of 0.3 nm
or an angle set by the system
350 ft
FLIGHT
INSTRUMENTS
CDI Full-scale Deflection
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
Landing
Threshold
CDI scale varies if VTF is activated
Figure 2-28 Typical LNAV and LNAV+V Approach CDI Scaling
Figure 2-29 Typical LNAV/VNAV and LPV Approach CDI Scaling
AUDIO PANEL
& CNS
• When a missed approach is activated, the CDI scale changes to 0.3 nm.
• The system automatically switches back to terminal scaling under the following conditions:
- The next leg in the missed approach procedure is not aligned with the final approach path
FLIGHT
MANAGEMENT
- The next leg in the missed approach procedure is not CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF
AFCS
HAZARD
AVOIDANCE
- After any leg in the missed approach procedure that is not CA or FA
Flight Phase
Departure
Terminal
Enroute
Oceanic
Annunciation
DPRT
TERM
ENR
OCN
Approach
(Non-precision)
LNAV
APPENDICES
ADDITIONAL
FEATURES
Approach
(Non-precision with
Vertical Guidance)
Approach
(LNAV/VNAV)
Approach
(LPV)
Missed Approach
Automatic CDI Full-scale Deflection
0.3 nm
1.0 nm
2.0 nm
2.0 nm
1.0 nm decreasing to 350 feet depending on
variables (see Figure 2-28)
LNAV + V
L/VNAV
LPV
MAPR
1.0 nm decreasing to a specified course width, then
0.3 nm, depending on variables (see Figure 2-29)
0.3 nm
INDEX
Table 2-1 Automatic GPS CDI Scaling
68
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
OBS MODE
NOTE: VNV is inhibited while automatic waypoint sequencing has been suspended.
FLIGHT
INSTRUMENTS
Enabling Omni-bearing Selector (OBS) Mode suspends the automatic sequencing of waypoints in a GPS
flight plan (GPS must be the selected navigation source), but retains the current “active-to” waypoint as the
navigation reference even after passing the waypoint. ‘OBS’ is annunciated to the lower right of the aircraft
symbol when OBS Mode is selected.
EIS
While OBS Mode is enabled, a course line is drawn through the “active-to” waypoint on the moving map. If desired, the course to/from the waypoint can now be adjusted. When OBS Mode is disabled, the GPS flight
plan returns to normal operation with automatic sequencing of waypoints, following the course set in OBS
Mode. The flight path on the moving map retains the modified course line.
AUDIO PANEL
& CNS
GPS
Selected
FLIGHT
MANAGEMENT
OBS Mode
Enabled
Extended
Course
Line
Pressing the OBS
Softkey Again
Disables OBS Mode
HAZARD
AVOIDANCE
Pressing the OBS
Softkey Enables
OBS Mode
Figure 2-30 Omni-bearing Selector (OBS) Mode
Enabling/disabling OBS Mode while navigating a GPS flight plan:
AFCS
1) Select the OBS Softkey to select OBS Mode.
2) Turn the CRS Knob to select the desired course to/from the waypoint. Press the CRS Knob to synchronize the
Selected Course with the bearing to the next waypoint.
ADDITIONAL
FEATURES
3) Select the OBS Softkey again to return to automatic waypoint sequencing.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
69
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
As the aircraft crosses the missed approach point (MAP), automatic approach waypoint sequencing is
suspended. ‘SUSP’ appears on the HSI at the lower right of the aircraft symbol. The OBS Softkey label
changes to indicate the suspension is active as shown in Figure 2-31. Selecting the SUSP Softkey, deactivates
the suspension and resumes automatic sequencing of approach waypoints.
FLIGHT
MANAGEMENT
SUSP
Softkey
SUSP
Annunciation
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Figure 2-31 Suspending Automatic Waypoint Sequencing
70
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
2.2 SUPPLEMENTAL FLIGHT DATA
NOTE: Selecting the DFLTS Softkey turns off metric Altimeter display, the Inset Map, and wind data display.
FLIGHT
INSTRUMENTS
In addition to the flight instruments, the PFD also displays various supplemental information, including
temperatures, wind data, and Vertical Navigation (VNV) indications.
TEMPERATURE DISPLAYS
EIS
The Outside Air Temperature (OAT) and deviation from International Standard Atmosphere (ISA) temperature
are displayed in the lower left of the PFD under normal display conditions, or to the right of the Elevator Trim
in reversionary display mode. Both are displayed in degrees Celsius (°C).
Normal Display
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
Reversionary Mode
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 2-32 Outside Air Temperature and ISA Temperature
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
71
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
Changing temperature display units:
1) Select the AUX - System Setup Page on the MFD using the FMS Knob.
FLIGHT
INSTRUMENTS
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the TEMP field in the Display Units box.
4) Turn the small FMS Knob to highlight either CELSIUS or FAHRENHEIT and press the ENT Key to confirm the
selection.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
5) To cancel the selection, press the FMS Knob or the CLR Key.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 2-33 Temperature Selection
(AUX - System Setup Page)
72
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
WIND DATA
Option 2
Option 3
No Data
EIS
Option 1
FLIGHT
INSTRUMENTS
Wind direction and speed (relative to the aircraft) in knots can be displayed in a window to the upper left of
the HSI. When the window is selected for display, but wind information is invalid or unavailable, the window
shows “NO WIND DATA”. Wind data can be displayed in three different ways:
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 2-34 Wind Data
Displaying wind data:
1) Select the PFD Softkey.
HAZARD
AVOIDANCE
2) Select the WIND Softkey to display wind data display options.
3) Select one of the OPTN softkeys to change how wind data is displayed:
• OPTN 1: Wind direction arrows with headwind and crosswind components
• OPTN 2: Wind direction arrow and speed
AFCS
• OPTN 3: Wind direction arrow with direction and speed
4) To remove the window, select the OFF Softkey.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
73
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
VERTICAL NAVIGATION (VNV) INDICATIONS
FLIGHT
INSTRUMENTS
When a VNV flight plan has been activated, VNV indications (VNV Target Altitude, RSVI, VDI) appear on the
PFD in conjunction with the “TOD within 1 minute” message and “Vertical track” voice alert. See the Flight
Management section for details on VNV features. VNV indications are removed from the PFD according to the
criteria listed in Table 2-2.
Top of Descent Message
EIS
VNV Target
Altitude
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Vertical
Deviation
Indicator
Required
Vertical
Speed Bug
GPS is
Selected
Navigation
Source
HAZARD
AVOIDANCE
Terminal
Phase of
Flight
Figure 2-35 Vertical Navigation Indications (PFD)
AFCS
Criteria
APPENDICES
ADDITIONAL
FEATURES
Aircraft > 1 min before the next TOD due to flight plan change
VNV cancelled (CNCL VNV Softkey selected on MFD)
Distance to active waypoint cannot be computed due to
unsupported flight plan leg type (see Flight Management
Section)
Aircraft > 250 feet below active VNV Target Altitude
Current crosstrack or track angle error has exceeded limit
Active altitude-constrained waypoint can not be reached within
maximum allowed flight path angle and vertical speed
VNV Indication Removed
Required Vertical
Vertical
VNV Target
Speed (RSVI)
Deviation (VDI)
Altitude
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
INDEX
Table 2-2 VNV Indication Removal Criteria
74
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
2.3 PFD ANNUNCIATIONS AND ALERTING FUNCTIONS
FLIGHT
INSTRUMENTS
The following annunciations and alerting functions are displayed on the PFD. Refer to Appendix A for more
information on alerts and annunciations.
SYSTEM ALERTING
EIS
Messages appear in the Alerts Window in the lower right corner of the PFD when a warning, caution,
advisory alert, or system message advisory occurs. System alert messages are provided for awareness of system
problems or status and may not require pilot action. The Alerts Window allows system alerts to be displayed
simultaneously. The FMS Knob is used to scroll through the alert messages. The Alerts Window is enabled/
disabled by selecting the ALERTS Softkey. If the window is already open when a new message is generated,
selecting the ALERTS Softkey to acknowledge the message causes it to turn gray.
AUDIO PANEL
& CNS
The ALERTS Softkey label changes to display the appropriate annunciation when an alert is issued. The
annunciation flashes and the appropriate aural alert sounds until acknowledged by selecting the softkey. The
softkey then reverts to the ALERTS Softkey label, and when selected again opens the Alerts Window to display
a descriptive message of the alert.
FLIGHT
MANAGEMENT
The Annunciation Window appears to the right of the Vertical Speed Indicator and displays abbreviated
annunciation text for aircraft alerts. Warnings appear in red, cautions in yellow, advisory alerts in white. New
alerts are displayed at the top of the Annunciation Window, regardless of priority. Once acknowledged, they
are sequenced based on priority.
HAZARD
AVOIDANCE
Annunciation
Window
Alerts
Window
AFCS
ADDITIONAL
FEATURES
APPENDICES
Softkey
Annunciations
Figure 2-36 System Alerting
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
75
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
MARKER BEACON ANNUNCIATIONS
FLIGHT
INSTRUMENTS
Marker Beacon Annunciations are displayed on the PFD to the left of the Selected Altitude. Outer marker
reception is indicated in blue, middle in yellow, and inner in white. Refer to the Audio Panel and CNS Section
for more information on Marker Beacon Annunciations.
Middle Marker
Inner Marker
EIS
Outer Marker
AUDIO PANEL
& CNS
Altimeter
Figure 2-37 Marker Beacon Annunciations
FLIGHT
MANAGEMENT
TRAFFIC ANNUNCIATION
Traffic is displayed symbolically on the PFD Inset Map, the MFD Navigation Map Page, and various other
MFD page maps. Refer to the Hazard Avoidance Section and the Appendix for more details about the Traffic
Information Service (TIS) and optional Traffic Advisory Systems (TAS). When a traffic advisory (TA) is detected,
the following automatically occur:
HAZARD
AVOIDANCE
• The PFD Inset Map is enabled and displays traffic
• A flashing black-on-yellow ‘TRAFFIC’ annunciation (Figure 2-38) appears to the top left of the Attitude
Indicator for five seconds and remains displayed until no TAs are detected in the area
AFCS
• A single “Traffic” aural alert is generated, unless an optional Traffic Advisory System (TAS) is installed (refer
to the applicable TAS documentation for alerts generated by TAS equipment)
ADDITIONAL
FEATURES
If additional TAs appear, new aural and visual alerts are generated.
APPENDICES
Figure 2-38 Traffic Annunciation
Traffic
Symbols
INDEX
Figure 2-39 Inset Map with Traffic Displayed
76
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
TERRAIN ANNUNCIATIONS
FLIGHT
INSTRUMENTS
Terrain Awareness and Warning System - Class B (TAWS-B) or Terrain-SVS annunciations appear on the PFD
to the upper left of the Altimeter. Refer to the Hazard Avoidance Section and the Appendix for information on
optional TAWS-B or Terrain-SVS alerts and annunciations.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Inset Map
Enabled,
Displaying
Traffic When
TA Detected
Figure 2-40 Traffic and Example TAWS-B Annunciations
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
77
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
ALTITUDE ALERTING
FLIGHT
INSTRUMENTS
Altitude Alerting provides the pilot with visual and aural alerts when approaching the Selected Altitude. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of
the GFC 700 AFCS, but alerting tones and visual alerts are only provided when the GFC 700 is installed. The
following occur when approaching the Selected Altitude:
• Upon passing through 1000 feet of the Selected Altitude, the Selected Altitude changes to black text on a light
blue background and flashes for 5 seconds.
EIS
• When the aircraft passes within 200 ft of the Selected Altitude, an aural tone is heard, and the Selected
Altitude changes to light blue text on a black background and flashes for 5 seconds.
AUDIO PANEL
& CNS
• After reaching the Selected Altitude, if the pilot flies outside the deviation band (±200 feet of the Selected
Altitude) an aural tone is heard. The Selected Altitude changes to yellow text on a black background and
flashes for 5 seconds.
Within 1000 ft
Within 200 ft
Deviation of ±200 ft
FLIGHT
MANAGEMENT
Figure 2-41 Altitude Alerting Visual Annunciations
LOW ALTITUDE ANNUNCIATION
HAZARD
AVOIDANCE
NOTE: The Low Altitude Annunciation is available only when SBAS is available. This annunciation is not
shown for systems with TAWS or Terrain-SVS, unless terrain alerting is inhibited.
AFCS
When the Final Approach Fix (FAF) is the active waypoint in a GPS SBAS approach using vertical guidance,
a Low Altitude Annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed
altitude at the FAF. A black-on-yellow ‘LOW ALT’ annunciation appears to the top left of the Altimeter, flashing
for several seconds then remaining displayed until the condition is resolved.
ADDITIONAL
FEATURES
Altimeter
INDEX
APPENDICES
Figure 2-42 Low Altitude on GPS SBAS Approach
78
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
MINIMUM DESCENT ALTITUDE/DECISION HEIGHT ALERTING
FLIGHT
INSTRUMENTS
For altitude awareness, a barometric Minimum Descent Altitude (MDA) or Decision Height (DH) can be set
in the Timer/References Window and is reset when the power is cycled. When active, the altitude setting is
displayed to the bottom left of the Altimeter. Once the altitude is within the range of the tape, a bug appears
at the reference altitude on the Altimeter. The following visual annunciations occur when approaching the
MDA/DH:
• When the aircraft altitude descends to within 2500 feet of the MDA/DH setting, the ‘BARO MIN’ box appears
with the altitude in light blue text. The bug appears on the altitude tape in light blue once in range.
EIS
• When the aircraft passes through 100 feet of the MDA/DH, the bug and text turn white.
• Once the aircraft reaches the MDA/DH, the bug and text turn yellow and the aural alert, “Minimums
Minimums”, is heard.
White Within 100 ft
Yellow When Altitude Reached
AUDIO PANEL
& CNS
Light Blue Within 2500 ft
MDA/DH
Bug
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Barometric
Minimum
Box
Figure 2-43 Barometric MDA/DH Alerting Visual Annunciations
Setting the barometric Minimum Descent Altitude/Decision Height and bug:
AFCS
1) Select the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the ‘Minimums’ field (Figure 2-44).
ADDITIONAL
FEATURES
3) Turn the small FMS Knob to select BARO. OFF is selected by default. Press the ENT Key or turn the large FMS
Knob to highlight the next field.
4) Use the small FMS Knob to enter the desired altitude from zero to 16,000 feet.
5) To remove the window, press the CLR Key or select the TMR/REF Softkey.
APPENDICES
Figure 2-44 Minimum Descent Altitude/Decision Height
Setting (Timer/References Window)
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
Alerting is inhibited while the aircraft is on the ground and until the aircraft reaches 150 feet above the MDA/
DH. If the aircraft proceeds to climb after having reached the MDA/DH, once it reaches 50 feet above the MDA/
DH, alerting is disabled.
79
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
2.4 ABNORMAL OPERATIONS
FLIGHT
INSTRUMENTS
ABNORMAL GPS CONDITIONS
The annunciations listed in Table 2-3 can appear on the HSI when abnormal GPS conditions occur. Refer to
the Flight Management Section for more information on Dead Reckoning Mode.
Annunciation
EIS
LOI
INTEG OK
AUDIO PANEL
& CNS
DR
Location
Lower left of
aircraft symbol
Lower left of
aircraft symbol
Upper right of
aircraft symbol
Description
Loss of Integrity Monitoring–GPS integrity is insufficient for the current
phase of flight
Integrity OK–GPS integrity has been restored to within normal limits
(annunciation displayed for 5 seconds)
Dead Reckoning–System is using projected position rather than GPS position
to compute navigation data and sequence active flight plan waypoints
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Table 2-3 Abnormal GPS Conditions Annunciated on HSI
Figure 2-45 Example HSI Annunciations
In Dead Reckoning Mode the following items on the PFD are then shown in yellow:
• CDI (when GPS is the selected navigation source; the CDI is removed after 20 minutes)
AFCS
• Current Track Bug
• Wind Data
• Distances in the Bearing Information windows
ADDITIONAL
FEATURES
• GPS bearing pointers
INDEX
APPENDICES
These items should be verified when operating in Dead Reckoning Mode and they become increasingly
inaccurate over time.
80
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT INSTRUMENTS
SYSTEM
OVERVIEW
UNUSUAL ATTITUDES
Nose High
FLIGHT
INSTRUMENTS
When the aircraft enters an unusual pitch attitude, red chevrons pointing toward the horizon warn of extreme
pitch. The chevrons are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon
line.
Nose Low
EIS
AUDIO PANEL
& CNS
Figure 2-46 Pitch Attitude Warnings
FLIGHT
MANAGEMENT
• Traffic Annunciations
• AFCS Annunciations
• Windows displayed in the lower
right corner of the PFD:
• Vertical Deviation, Glideslope,
and Glidepath Indicators
• Altimeter Barometric Setting
• Inset Map
– Nearest Airports
• Selected Altitude
• Outside Air Temperature (OAT)
– Flight Plan
• VNV Target Altitude
• Wind Data
– Alerts
• Selected Heading
• Transponder Status Box
– Procedures
• Selected Course
• Minimum Descent Altitude/
Decision Height readout
ADDITIONAL
FEATURES
– Timer/References
AFCS
• Flight Director Command Bars
• System Time
HAZARD
AVOIDANCE
If pitch exceeds +30˚/-20˚ or bank exceeds 65˚, some information displayed on the PFD is removed. The
Altimeter, Airspeed, Attitude, Vertical Speed, and Horizontal Situation indicators remain on the display and
the Bearing Information, Alerts, and Annunciation windows can be displayed during such situations. The
following information is removed from the PFD (and corresponding softkeys are disabled) when the aircraft
experiences unusual attitudes:
• PFD Setup Menu
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
81
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
FLIGHT INSTRUMENTS
Blank Page
82
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
SECTION 3 ENGINE INDICATION SYSTEM
FLIGHT
INSTRUMENTS
The Engine Indication System (EIS) for the Cessna Corvalis/Corvalis TT displays critical engine, electrical, fuel,
and other system parameters on the left side of the MFD during normal operations. EIS information can be fully
expanded to an entire page (Engine Page) using the SYSTEM Softkey. In reversionary display mode, the display is
configured to present PFD symbology together with the EIS Display (refer to the System Overview for information
about reversionary display mode).
EIS
Instrument types include dial gauges, horizontal and vertical bar indicators, digital readouts, slide bars, and bar
graphs. Green bands indicate normal ranges of operation; yellow and red bands indicate caution and warning,
respectively. White bands indicate areas outside of normal operation not yet in the caution or warning ranges.
When unsafe operating conditions occur, the corresponding readouts flash to indicate cautions and warnings.
If sensory data to an instrument becomes invalid or unavailable, a red “X” is displayed across the instrument.
AUDIO PANEL
& CNS
EIS Display
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 3-1 MFD (Corvalis TT)
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
83
SYSTEM
OVERVIEW
ENGINE INDICATION SYSTEM
3.1 EIS DISPLAY
FLIGHT
INSTRUMENTS
NOTE: For engine speeds less than 500 rpm, no warning occurs for manifold pressure and oil pressure
outside the acceptable operating range.
Engine Manifold Pressure
Gauge (MAN IN HG)
Displays engine power in inches of Mercury (in Hg)
2
Tachometer (RPM)
Shows propeller speed in revolutions per minute (rpm)
3
Fuel Quantity Indicator
(FUEL QTY GAL)
Displays the amount of fuel in gallons (gal). A light blue marker is
displayed next to the selected fuel tank.
4
Fuel Flow Indicator
(FFLOW GPH)
Displays fuel flow in gallons per hour (gph)
5
Oil Pressure Indicator
(OIL PSI)
Oil pressure is displayed in pounds per square inch (psi)
6
Oil Temperature Indicator
(OIL °F)
Oil temperature is shown in degrees Fahrenheit (°F)
7
Exhaust Gas Temperature
Indicator (EGT °F)
Corvalis only
Turbo Inlet Temperature
Indicator (TIT °F) Corvalis
TT only
Cylinder Head Temperature
Indicator (CHT °F)
Shows the Exhaust Gas Temperature of the hottest cylinder (number is
shown in pointer) in degrees Fahrenheit (°F)
Trim Group (AILERON
TRIM, ELEV TRIM)
Aileron and elevator trim are displayed on slide bars; the green portions
of the bars represent correct takeoff trim positions
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
1
AFCS
8
ADDITIONAL
FEATURES
9
Shows the head temperature of the hottest cylinder (number is shown
in pointer) in degrees Fahrenheit (°F)
INDEX
APPENDICES
10
Displays the inlet temperature for both turbo inlets in degrees Fahrenheit
(°F); the inlet number is shown in pointer
84
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
1
EIS
2
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
3
4
HAZARD
AVOIDANCE
5
6
7
8
9
9
10
10
AFCS
6
ADDITIONAL
FEATURES
Corvalis
APPENDICES
Corvalis TT
Figure 3-2 EIS Display
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
85
SYSTEM
OVERVIEW
ENGINE INDICATION SYSTEM
3.2 ENGINE PAGE
FLIGHT
INSTRUMENTS
Selecting the SYSTEM Softkey on the MFD accesses the Engine Page, which displays all Engine Indication
System instruments; selecting the softkey again exits the Engine Page.
The Engine Page displays engine, fuel, fuel calculation, electrical, oxygen, and trim information using round dial
gauges, bar indicators, bar graphs, digital readouts, and slide bars. As in the EIS Display, the manifold pressure
gauge, tachometer, and trim slide bars are shown. Fuel flow and oil parameters are displayed using gauges rather
than horizontal bar indicators.
AUDIO PANEL
& CNS
EIS
Oxygen quantity and outlet pressure (if installed) are also shown on the Engine Page. The OXYGEN Softkey
can be used to turn the oxygen system on/off. If no oxygen system is installed, blank gauges are displayed.
SYSTEM
MAP
SYSTEM
(Corvalis TT
Option)
OXYGEN
DCLTR
DCLTR
ASSIST
CO RST
SHW CHRT CHKLIST
DEC FUEL INC FUEL RST FUEL
FLIGHT
MANAGEMENT
Press the SYSTEM Softkey to
return to the top-level softkeys.
Figure 3-3 EIS Engine Page Softkeys
HAZARD
AVOIDANCE
1
2
AFCS
3
ADDITIONAL
FEATURES
4
5
APPENDICES
6
7
INDEX
8
86
Oil Temperature/Pressure
Gauge
(OIL °F PSI)
Engine Manifold Pressure
Gauge
(MAN IN HG)
Tachometer
(RPM)
Fuel Calculations Group
(GAL REM, GAL USED,
ENDUR, RANGE NM)
Oxygen Quantity Gauge
(OXY QTY PSI) Corvalis
TT only
Oxygen Outlet Pressure
Gauge (OXY OUTLET
PSI) Corvalis TT only
Electrical Group
(ALT AMPS, BATT AMPS,
BUS VOLTS)
Trim Group
(AILERON TRIM,
ELEV TRIM)
Oil temperature is shown on the left half in degrees Fahrenheit (°F) and
pressure is displayed on the right in pounds per square inch (psi)
Displays engine power in inches of Mercury (in Hg)
Shows propeller speed in revolutions per minute (rpm)
The fuel totalizer fuel remaining and used and the totalizer-based
endurance and range calculations are displayed
Oxygen amount in psi; note that gauge increment is 100 psi
Oxygen outlet pressure in psi. Gauge ranges are dependent on type of
oxygen outlet pressure system installed (high or low).
Currents for the right and left alternators and batteries along with bus
voltages are displayed using vertical bar indicators and readouts
Aileron and elevator trim are displayed on slide bars.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ENGINE INDICATION SYSTEM
10
Fuel Quantity Gauges
(L/R FUEL QTY GAL)
Fuel Flow Gauge
(FFLOW GPH)
11
For each cylinder, the exhaust gas and head temperatures are shown in
degrees Fahrenheit (°F). The temperature for both turbo inlets in °F
is also shown (Corvalis TT only).
Gauges display the amount of fuel in gallons (gal). A light blue marker
is displayed next to the selected fuel tank.
Displays fuel flow in gallons per hour (gph)
1
2
3
FLIGHT
INSTRUMENTS
Engine Temperature Group
(EGT °F, CHT °F, TIT °F)
SYSTEM
OVERVIEW
9
4
EIS
AUDIO PANEL
& CNS
11
7
9
8
FLIGHT
MANAGEMENT
10
HAZARD
AVOIDANCE
Carbon
Monoxide
Warning
Figure 3-4 Engine Page (Corvalis)
1
2
3
4
5
AFCS
6
10
7
9
8
APPENDICES
11
ADDITIONAL
FEATURES
Optional High Pressure
Oxygen Outlet Gauge
INDEX
Figure 3-5 Engine Page (Corvalis TT)
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
87
SYSTEM
OVERVIEW
ENGINE INDICATION SYSTEM
CARBON MONOXIDE DETECTION
FLIGHT
INSTRUMENTS
If carbon monoxide (CO) in the cabin becomes too high (exceeds 50 ppm), a flashing red annunciation and
the current level of CO in parts per million (ppm) are displayed in the lower right corner of the Engine Page.
Figure 3-6 Carbon Monoxide Warning
EIS
When a warning is generated, the CO RST Softkey becomes available to reset the CO Guardian and
acknowledge the alert. A warning annunciation is also displayed on the PFD in the Annunciations Window
along with an aural warning (refer to the aircraft-specific alerts in Appendix A).
AUDIO PANEL
& CNS
FUEL CALCULATIONS GROUP
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time
FLIGHT
MANAGEMENT
the fuel was reset.
Fuel used (GAL USED), endurance (ENDUR), and range (RANGE NM) are all calculated based on the
displayed fuel remaining (GAL REM) and the fuel flow totalizer. The fuel remaining can be adjusted using the
following softkeys:
• DEC FUEL – Decreases totalizer-based fuel remaining in one-gallon increments
HAZARD
AVOIDANCE
• INC FUEL – Increases totalizer-based fuel remaining in one-gallon increments
ADDITIONAL
FEATURES
AFCS
• RST FUEL – Resets totalizer-based fuel remaining to the aircraft’s fuel capacity (98 or 102 gal usable) and sets
the GAL USED display to zero
Fuel
Remaining
Endurance
Calculation
Fuel Used
Calculation
Range
Calculation
INDEX
APPENDICES
Figure 3-7 Fuel Calculations Group
88
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
ENGINE TEMPERATURE GROUP
FLIGHT
INSTRUMENTS
The temperature group displays the Cylinder Head Temperature (CHT) and Exhaust Gas Temperature (EGT)
in degrees Fahrenheit for each cylinder using bar graphs and digital readouts. For the Corvalis TT, Turbo Inlet
Temperature (TIT) is shown on a sliding bar scale.
The following softkeys can be used to modify the display of engine temperature information:
• DCLTR – Removes/displays the EGT and CHT readouts from the display
• ASSIST – Accesses the Engine Leaning Assist Mode (see Section 3.3)
EIS
Cylinder Head
Temperature
AUDIO PANEL
& CNS
Exhaust Gas
Temperature
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 3-8 Engine Temperature Group (Corvalis)
Turbo Inlet
Temperature
Cylinder Head
Temperature
AFCS
Exhaust Gas
Temperature
ADDITIONAL
FEATURES
APPENDICES
Figure 3-9 Engine Temperature Group (Corvalis TT)
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
89
SYSTEM
OVERVIEW
ENGINE INDICATION SYSTEM
3.3 ENGINE LEANING ASSIST MODE
FLIGHT
INSTRUMENTS
NOTE: Consult the Cessna Corvalis/Corvalis TT Airplane Flight Manual (AFM) for leaning procedures.
From the Engine Page, the Engine Leaning Assist Mode may be accessed by selecting the ASSIST Softkey.
Selecting the ASSIST Softkey again returns the MFD to the Engine Page. Use the SYSTEM Softkey to exit the
Engine Page.
EIS
While in Assist Mode, the EIS Display is shown along with the Fuel Flow Gauge and an expanded Engine
Temperature Group.
CORVALIS
AUDIO PANEL
& CNS
When the ASSIST Softkey is selected, the system initially highlights the number and EGT readout of the
cylinder with the hottest EGT.
FLIGHT
MANAGEMENT
Fuel Flow Gauge
EIS Display
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
EGT Deviation
from Peak
INDEX
APPENDICES
Figure 3-10 Engine Leaning Assist Mode (Corvalis)
90
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
When the first peak is detected, the cylinder numbers disappear, “1st” is annunciated in light blue below that
cylinder’s EGT bar, the temperature is marked in light blue on the graph, and the EGT readout is outlined.
FLIGHT
INSTRUMENTS
Temperature Deviation from Peak
(First Cylinder)
EIS
Light Blue Bar
Represents Peak
AUDIO PANEL
& CNS
Indicates First
Cylinder to Peak
Figure 3-11 Assist Mode - First Peaked Cylinder (Corvalis)
FLIGHT
MANAGEMENT
The system continues to detect peak EGTs for each cylinder as the fuel flow is decreased and the peak of
each cylinder’s EGT is indicated by a light blue marker. The last cylinder to peak is denoted by the “Last”
annunciation below its bar on the graph and the EGT readout is outlined in light blue.
Temperature Deviation from Peak
(Last Cylinder)
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Indicates Last
Cylinder to Peak
Figure 3-12 Assist Mode - Last Peaked Cylinder (Corvalis)
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
91
SYSTEM
OVERVIEW
ENGINE INDICATION SYSTEM
CORVALIS TT
FLIGHT
INSTRUMENTS
Once the ASSIST Softkey is selected, the peak of each TIT is indicated by a light blue bar which moves and
remains at the peak Turbo Inlet Temperature.
AUDIO PANEL
& CNS
EIS
Peak TIT
FLIGHT
MANAGEMENT
Lean or Rich
From Peak
TIT Deviation
from Peak
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Figure 3-13 Engine Leaning Assist Mode (Corvalis TT)
92
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
SECTION 4 AUDIO PANEL AND CNS
FLIGHT
INSTRUMENTS
4.1 OVERVIEW
The Communication/Navigation/Surveillance (CNS) system includes the audio panel, communication radios,
navigation radios, and Mode S transponder. The System Overview Section provides a block diagram description
of the Audio Panel and CNS system interconnection.
• Audio Panel
• Multi Function Display (MFD)
• Mode S Transponder
• Integrated Avionics Unit (2)
• MFD/PFD Control Unit
AUDIO PANEL
& CNS
• Primary Flight Display (PFD)
EIS
CNS operation in Cessna Corvalis/Corvalis TT aircraft is performed by the following Line Replaceable Units
(LRUs):
The MFD/PFD controls are used to tune the communication transceivers and navigation radios.
FLIGHT
MANAGEMENT
The Audio Panel provides the traditional audio selector functions of microphone and receiver audio selection.
The Audio Panel includes an intercom system (ICS) between the pilot, copilot, and passengers, a marker beacon
receiver, and a COM clearance recorder. Ambient noise from the aircraft radios is reduced by a feature called
Master Avionics Squelch (MASQ). When no audio is detected, MASQ processing further reduces the amount of
background noise from the radios.
HAZARD
AVOIDANCE
The Mode S transponder is controlled with softkeys and the FMS Knob located on the Primary Flight Display
(PFD). The Transponder Data Box is located to the left of the System Time Box. The data box displays the active
four-digit code, mode, and reply status (Figure 4-1).
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
93
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
MFD/PFD CONTROLS AND FREQUENCY DISPLAY
2
3
4
5
6
7
8
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
1
9
10
HAZARD
AVOIDANCE
11
12
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 4-1 MFD/PFD Controls, NAV/COM Frequency Tuning Boxes, and ADF/DME Tuning Window
94
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
5
COM Frequency Box – Displays COM standby and active frequency fields and volume. The selected COM
transceiver frequency is displayed in green.
6
COM Knob – Tunes the standby frequencies for the COM transceiver (large knob for MHz; small knob for
kHz). Press to move the tuning box (light blue box) and Frequency Transfer Arrow between COM1 and
COM2.
7
COM Frequency Transfer Key – Transfers the standby and active COM frequencies. Press and hold this key
for two seconds to tune the emergency frequency (121.500 MHz) automatically into the active frequency
field.
8
COM VOL/SQ Knob – Controls COM audio volume level. Press to turn the COM automatic squelch on
and off. Volume level is shown in the COM frequency field as a percentage.
9
ADF/DME Tuning Window – Displays ADF frequencies, volume setting, and modes, and DME tuning
selection. Display by pressing the ADF/DME Softkey.
10
ENT Key – Validates or confirms an Auto-tune selection.
11
FMS Knob – Flight Management System Knob, used to enter transponder codes and select Auto-tune
entries when NRST Window is present. Press the FMS Knob to turn the selection cursor on and off.
The large knob moves the cursor in the window. The small knob selects individual characters for the
highlighted cursor location.
12
Transponder Data Box – Indicates the selected transponder code, operating mode, reply, and ident status
for the transponder.
ADDITIONAL
FEATURES
NAV Frequency Box – Displays NAV standby and active frequency fields, volume, and station ID. The
frequency of the NAV radio selected for navigation is displayed in green.
AFCS
4
HAZARD
AVOIDANCE
NAV Knob – Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for kHz).
Press to move the tuning box (light blue box) and Frequency Transfer Arrow between NAV1 and NAV2.
FLIGHT
MANAGEMENT
3
AUDIO PANEL
& CNS
NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies.
EIS
2
FLIGHT
INSTRUMENTS
NAV VOL/ID Knob – Controls NAV audio volume level. Press to turn the Morse code identifier audio on
and off. Volume level is shown in the NAV frequency field as a percentage.
SYSTEM
OVERVIEW
1
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
95
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
3
4
5
6
7
8
9
10
11
12
14
15
16
AUDIO PANEL
& CNS
2
13
FLIGHT
MANAGEMENT
1
18
19
20
21
HAZARD
AVOIDANCE
EIS
FLIGHT
INSTRUMENTS
AUDIO PANEL CONTROLS
22
23
17
24
AFCS
Figure 4-2 Audio Panel Controls
INDEX
APPENDICES
ADDITIONAL
FEATURES
NOTE: When a key is selected, a triangular annunciator above the key is illuminated.
96
1
COM1 MIC – Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when
this key is pressed allowing received audio from the #1 COM receiver to be heard. COM2 receive can be
added by pressing the COM2 Key.
2
COM1 – When selected, audio from the #1 COM receiver can be heard.
3
COM2 MIC – Selects the #2 transmitter for transmitting. COM2 receive is simultaneously selected when
this key is pressed allowing received audio from the #2 COM receiver to be heard. COM1 receive can be
added by pressing the COM1 Key.
4
COM2 – When selected, audio from the #2 COM receiver can be heard.
5
COM3 MIC – Not used in Cessna Corvalis/Corvalis TT aircraft.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the
speaker.
11
MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver
audio. Unmutes automatically when new marker beacon audio is received. Also, stops play of recorded
COM audio.
12
HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity.
13
DME – Turns optional DME audio on or off.
14
NAV1 – When selected, audio from the #1 NAV receiver can be heard.
15
ADF – Turns optional ADF receiver audio on or off
16
NAV2 – When selected, audio from the #2 NAV receiver can be heard.
17
AUX – Not used in Cessna Corvalis/Corvalis TT aircraft.
18
MAN SQ – Enables manual squelch for the intercom. When the intercom is active, press the PILOT Knob
to illuminate SQ. Turn the PILOT/PASS Knobs to adjust squelch.
19
PLAY – Press once to play the last recorded COM audio. Press again while audio is playing and the
previous block of recorded audio will be played. Each subsequent press plays each previously recorded
block. Pressing the MKR/MUTE Key during play of a memory block stops play.
20
PILOT – Selects and deselects the pilot intercom isolation.
21
COPLT – Selects and deselects the copilot intercom isolation.
22
PILOT Knob – Press to switch between volume and squelch control as indicated by illumination of VOL
or SQ. Turn to adjust intercom volume or squelch. The MAN SQ Key must be selected to allow squelch
adjustment.
23
PASS Knob – Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be
selected to allow squelch adjustment.
24
DISPLAY BACKUP Button – Manually selects Reversionary Mode.
APPENDICES
10
ADDITIONAL
FEATURES
PA – Selects the passenger address system. The selected COM transmitter is deselected when the PA Key
is pressed.
AFCS
9
HAZARD
AVOIDANCE
TEL – Not used in Cessna Corvalis/Corvalis TT aircraft.
FLIGHT
MANAGEMENT
8
AUDIO PANEL
& CNS
COM 1/2 – Split COM Key. Allows simultaneous transmission on COM1 and COM2 by the pilot and copilot.
EIS
7
FLIGHT
INSTRUMENTS
COM3 – Not used in Cessna Corvalis/Corvalis TT aircraft.
SYSTEM
OVERVIEW
6
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
97
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
MFD/PFD CONTROL UNIT
FLIGHT
INSTRUMENTS
The MFD/PFD Control Unit is a pedestal-mounted interface allowing MFD/PFD operation, data entry, COM
and NAV tuning, and transponder control. The MFD/PFD Control Unit duplicates many MFD/PFD display
bezel controls. Annunciators above the PFD, MFD, NAV, and COM keys are illuminated when their respective
control modes are selected. The unit is in MFD control mode by default on system power-up.
AUDIO PANEL
& CNS
13
FLIGHT
MANAGEMENT
EIS
Tune the COM and NAV radios in either MFD or PFD control mode. The appropriate frequency box on the
selected display is outlined by a light blue selection box, which flashes for a few seconds to indicate control
unit activity. Selection of a different display control or radio tuning mode results in cancellation of the previous
radio tuning mode.
10
1
12
11
9
2
HAZARD
AVOIDANCE
8
3
AFCS
7
6
5
4
ADDITIONAL
FEATURES
Figure 4-3 MFD/PFD Control Unit
APPENDICES
Tuning Selection
Box
INDEX
Figure 4-4 Frequency Tuning with the MFD/PFD Control Unit
98
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
ENT Key – Validates or confirms a menu selection or data entry.
5
CLR Key – Erases information, cancels entries, or removes menus.
6
SEL Key – Arrows move light blue Softkey Selection Box on selected display. Press the center to activate
the selected softkey
7
Decimal Key – Enters a decimal point.
8
NAV Key – Selects NAV radio tuning mode on the MFD/PFD Control Unit. The NAV tuning box is
outlined with a light blue selection line when the NAV frequency is active on the control unit.
9
COM Key – Selects COM radio tuning mode on the MFD/PFD Control Unit. The COM tuning box is
outlined with a light blue selection line when the COM frequency is active on the control unit.
10
Frequency Transfer Key (EMERG) – Transfers the standby and active COM or NAV frequencies. Press
and hold for two seconds to tune the emergency frequency (121.500 MHz) automatically into the COM
active frequency field.
11
PFD Key – When selected, the MFD/PFD Control Unit is used to access PFD functions.
12
MFD Key – When selected, the MFD/PFD Control Unit is used to access MFD functions (default control
mode).
13
FMS/NAV-COM Knob – NAV/COM Tuning Modes: Acts as the NAV or COM Knob. MFD/PFD Control
Modes: Acts as the FMS Knob.
AFCS
4
HAZARD
AVOIDANCE
BKSP Key – Moves cursor back one character space and removes last character entered.
FLIGHT
MANAGEMENT
3
AUDIO PANEL
& CNS
Alphanumeric Keys – Allows data entry (rather than using the FMS Knob to select characters/
numbers).
EIS
2
FLIGHT
INSTRUMENTS
MENU Key – Displays a list of options for accessing additional features or making setting changes.
SYSTEM
OVERVIEW
1
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
99
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
4.2 COM OPERATION
FLIGHT
INSTRUMENTS
COM TRANSCEIVER SELECTION AND ACTIVATION
NOTE: During PA Mode, the COM MIC Annunciator is extinguished and the COM active frequency color
changes to white, indicating that neither COM transmitter is active.
NOTE: When turning on the G1000 for use, the system remembers the last frequencies used and the active
EIS
COM transceiver state prior to shutdown.
AUDIO PANEL
& CNS
The COM Frequency Box is composed of four fields; the two active frequencies are on the left side and
the two standby frequencies are on the right. Select the COM transceiver for transmitting by pressing the
COM MIC Keys on the Audio Panel. During reception of audio from the COM radio selected for transmission,
audio from the other COM radio is muted.
FLIGHT
MANAGEMENT
An active COM frequency displayed in green indicates that the COM transceiver is selected on the Audio
Panel (COM1 MIC or COM2 MIC Key). Both active COM frequencies appearing in white indicate that no COM
radio is selected for transmitting (PA Key is selected on the Audio Panel).
Frequencies in the standby field are displayed in either white or gray. The standby frequency in the tuning
box is white. The other standby frequency is gray.
HAZARD
AVOIDANCE
Active
Fields
Standby
Fields
Top Section of
the Audio Panel
AFCS
Tuning Box
ADDITIONAL
FEATURES
COM2 Radio is Selected
on the Audio Panel
INDEX
APPENDICES
Figure 4-5 Selecting a COM Radio for Transmit
100
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
TRANSMIT/RECEIVE INDICATIONS
FLIGHT
INSTRUMENTS
During COM transmission, a white TX appears by the active COM frequency replacing the Frequency
Transfer Arrow. On the Audio Panel, when the active COM is transmitting, the active transceiver COM MIC
Key Annunciator flashes approximately once per second.
During COM signal reception, a white RX appears by the active COM frequency replacing the Frequency
Transfer Arrow.
EIS
Transmit and
Receive Indicators
Annunciator
Flashes During
Transmission
AUDIO PANEL
& CNS
Figure 4-6 COM Radio Transmit and Receive Indications
COM TRANSCEIVER MANUAL TUNING
The COM frequency controls and frequency boxes are on the right side of the MFD and PFD.
FLIGHT
MANAGEMENT
Manually tuning a COM frequency:
1) Turn the COM Knob to tune the desired frequency in the COM Tuning Box (large knob for MHz; small knob for
kHz).
HAZARD
AVOIDANCE
2) Press the Frequency Transfer Key to transfer the frequency to the active field.
3) Adjust the volume level with the COM VOL/SQ Knob.
4) Press the COM VOL/SQ Knob to turn automatic squelch on and off.
Press the Frequency Transfer
Key to Transfer COM
Frequencies Between Active
and Standby Frequency Boxes
AFCS
Turn the VOL/SQ Knob to adjust
volume. Press the Knob to enable
or disable Automatic Squelch
ADDITIONAL
FEATURES
Turn the COM Knob to
Tune the Frequency in
the Tuning Box
APPENDICES
Figure 4-7 COM Frequency Tuning
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
101
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
Manual COM frequency tuning from the MFD/PFD Control Unit:
1) Press the COM Key to select the COM frequency box.
FLIGHT
INSTRUMENTS
2) Turn the FMS NAV/COM Knob to tune the desired frequency in the COM Tuning Box (large knob for MHz; small
knob for kHz).
Or:
Press the Numeric Keys on the keypad to enter a Frequency
3) Press the Frequency Transfer Key to transfer the frequency to the active field.
AUDIO PANEL
& CNS
EIS
If an error is made during frequency entry with the numeric keypad, pressing the BKSP Key moves the cursor
back one space. If an incorrect frequency is entered, reenter the correct one using the same procedure.
Second, turn the NAV/COM Knob to enter a
Frequency into the COM Standby Frequency Field
FLIGHT
MANAGEMENT
Third, press the Frequency
Transfer Key to move the
Frequency to the Active Field.
HAZARD
AVOIDANCE
First, press the COM
Key to place the
Tuning Selection
Box on the COM
frequencies
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 4-8 Frequency Tuning from the MFD/PFD Control Unit
102
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
SELECTING THE RADIO TO BE TUNED
Press the small COM Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the
upper and lower radio frequency fields.
FLIGHT
INSTRUMENTS
Press the COM Knob to
Switch the Tuning Box From
One COM Radio to the Other
EIS
Figure 4-9 Switching COM Tuning Boxes
AUDIO PANEL
& CNS
QUICK-TUNING AND ACTIVATING 121.500 MHZ
FLIGHT
MANAGEMENT
Pressing and holding the COM Frequency Transfer Key for two seconds automatically loads the emergency
COM frequency (121.500 MHz) in the active field of the COM radio selected for tuning (the one with the
transfer arrow). In the example shown, pressing the Audio Panel COM2 MIC Key activates the transceiver.
HAZARD
AVOIDANCE
Press for Two Seconds to
Load 121.500 MHz
Figure 4-10 Quickly Tuning 121.500 MHz
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
103
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
FLIGHT
INSTRUMENTS
AUTO-TUNING THE COM FREQUENCY
Tune COM frequencies from the following:
• Nearest Airports Window (PFD)
• NRST – Nearest Frequencies Page (ARTCC, FSS, WX)
• WPT – Airport Information Page
• NRST – Nearest Airspaces Page
• NRST – Nearest Airports Page
AUTO-TUNING FROM THE PFD
EIS
Tune COM frequencies for the nearest airports from the Nearest Airports Window on the PFD. When the
desired frequency is entered, it becomes a standby frequency. Pressing the Frequency Transfer Key places
this frequency into the COM Active Frequency Field.
AUDIO PANEL
& CNS
Auto-tuning a COM frequency for a nearby airport from the PFD:
1) Select the NRST Softkey on the PFD to open the Nearest Airports Window. A list of 25 nearest airport identifiers
and COM frequencies is displayed.
2) Turn the FMS Knob to scroll through the list and highlight the desired COM frequency.
FLIGHT
MANAGEMENT
3) Press the ENT Key to load the COM frequency into the COM Standby Tuning Box.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
4) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field.
INDEX
Figure 4-11 Nearest Airports Window (PFD)
Select the
NRST Softkey
to Open
the Nearest
Airports
Window
104
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
AUTO-TUNING FROM THE MFD
Load frequencies into the COM Frequency Box from pages in the NRST or WPT page group by highlighting
the frequency and pressing the ENT Key (Figures 4-13, 4-14, and 4-15).
FLIGHT
INSTRUMENTS
Auto-tuning a COM frequency from the WPT and NRST Pages:
1) From any page that the COM frequency can be auto-tuned, activate the cursor by pressing the FMS Knob or the
appropriate softkey.
2) Turn the FMS Knob to place the cursor on the desired COM frequency (Figure 4-14).
EIS
3) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio.
4) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field.
FLIGHT
MANAGEMENT
Turn the FMS
Knob to Scroll
Through a List
of Frequencies
AUDIO PANEL
& CNS
Press the ENT Key to
Load a Highlighted
Frequency into
the COM Standby
Frequency Box
Figure 4-12 Frequency Auto-Tuning from the MFD
HAZARD
AVOIDANCE
Or:
1) On the Nearest Airports, Frequencies, or Airspaces page, press the MENU Key to display the page menu.
2) Turn the large FMS Knob to scroll through the menu options.
3) Press the ENT Key to place the cursor on the desired selection.
AFCS
4) Scroll through the frequency selections with the FMS Knob.
5) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio.
6) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field.
ADDITIONAL
FEATURES
APPENDICES
Nearest Frequencies Menu
INDEX
Nearest Airports Menu
Nearest Airspaces Menu
Figure 4-13 Nearest Pages Menus
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
105
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
On the WPT - Airport Information Page, place the cursor on the frequency field by pressing the FMS Knob
and scrolling through the list. Transfer the frequency to the COM Standby Field with the ENT Key.
FLIGHT
INSTRUMENTS
Press Frequency
Transfer Key to Load
Frequency into COM
Active Frequency Field
EIS
Selected Airport
Identifier and
Information
AUDIO PANEL
& CNS
Runway
Information
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Press ENT Key to Load
Frequency into COM
Standby Field. Cursor
then Advances to
Next Frequency.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 4-14 WPT – Airport Information Page
Select INFO-x
Softkey for AIRPORT,
RUNWAYS, and
FREQUENCIES Windows
106
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
Tune COM frequencies from the NRST – Nearest Airspaces, NRST – Nearest Frequencies, and
NRST – Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU
Key, the FMS Knob, and the ENT Key.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 4-15 NRST – Nearest Airspaces, NRST – Nearest Airports, and NRST – Nearest Frequencies Pages
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
107
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
FREQUENCY SPACING
FLIGHT
INSTRUMENTS
The G1000 COM radios can tune either 25-kHz spacing (118.000 to 136.975 MHz) or 8.33-kHz spacing
(118.000 to 136.990 MHz) for 760-channel or 3040-channel configuration. When 8.33-kHz channel spacing
is selected, all of the 25-kHz channel spacing frequencies are also available in the complete 3040-channel list.
COM channel spacing is set on the System Setup Page of the AUX Page Group.
EIS
8.33-kHz Channel
Spacing
25-kHz Channel
Spacing
AUDIO PANEL
& CNS
Changing COM frequency channel spacing:
FLIGHT
MANAGEMENT
Figure 4-16 COM Channel Spacing
3) Turn the large FMS Knob to highlight the Channel Spacing Field in the COM Configuration Box.
1) Select the AUX – System Setup Page.
2) Press the FMS Knob to activate the flashing cursor.
4) Turn the small FMS Knob to select the desired channel spacing.
5) Press the ENT Key to complete the channel spacing selection.
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
While the COM CONFIG Window is selected, the G1000 softkeys are blank.
INDEX
APPENDICES
Select 8.33-kHz
or 25.0-kHz
COM Frequency
Channel Spacing
Figure 4-17 AUX – System Setup Page
108
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
AUTOMATIC SQUELCH
FLIGHT
INSTRUMENTS
Automatic Squelch quiets unwanted static noise when no audio signal is received, while still providing good
sensitivity to weak COM signals. To disable Automatic Squelch, press the VOL/SQ Knob. While Automatic
Squelch is disabled, COM audio reception is continuous (static noise is heard over the headsets and speaker).
Pressing the VOL/SQ Knob again enables Automatic Squelch.
When Automatic Squelch is disabled, a white SQ appears next to the COM frequency.
EIS
Squelch
Indication
Press the COM VOL/
SQ Knob to disable
Automatic Squelch.
Press again to enable
Automatic Squelch.
AUDIO PANEL
& CNS
Figure 4-18 Overriding Automatic Squelch
VOLUME
FLIGHT
MANAGEMENT
Adjust COM radio volume level from 0 to 100% using the VOL/SQ Knob. Turning the knob clockwise
increases volume, turning the knob counterclockwise decreases volume. When adjusting volume, the level is
displayed in place of the standby frequencies. Volume level indication remains for two seconds after the change.
HAZARD
AVOIDANCE
COM Volume
Level Remains for
Two Seconds
Figure 4-19 COM Volume Level
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
109
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
4.3 NAV OPERATION
FLIGHT
INSTRUMENTS
NAV RADIO SELECTION AND ACTIVATION
The NAV Frequency Box is composed of four fields; two standby fields and two active fields. The active
frequencies are on the right side and the standby frequencies are on the left.
EIS
Press the CDI Softkey on the PFD to select a NAV radio for navigation. The active NAV frequency selected for
navigation is displayed in green. Selecting the CDI Softkey once selects NAV1 as the navigation radio. Selecting
the CDI Softkey a second time selects NAV2 as the navigation radio. Selecting the CDI Softkey a third time
activates GPS mode. Selecting the CDI Softkey again cycles back to NAV1.
While cycling through the CDI Softkey selections, the NAV Tuning Box and the Frequency Transfer Arrow are
placed in the active NAV Frequency Field and the active NAV frequency color changes to green.
AUDIO PANEL
& CNS
The three navigation modes that can be cycled through are:
• VOR1 (or LOC1) – If NAV1 is selected, a green single line arrow (not shown) labeled either VOR1 or LOC1
is displayed on the HSI and the active NAV1 frequency is displayed in green.
FLIGHT
MANAGEMENT
• VOR2 (or LOC2) – If NAV2 is selected, a green double line arrow (shown) labeled either VOR2 or LOC2 is
displayed on the HSI and the active NAV2 frequency is displayed in green.
• GPS – If GPS Mode is selected, a magenta single line arrow (not shown) appears on the HSI and neither NAV
radio is selected. Both active NAV frequencies are then displayed in white.
HAZARD
AVOIDANCE
Standby
Fields
Active
Fields
Tuning Box
ADDITIONAL
FEATURES
AFCS
The NAV Radio is
Selected by Selecting
the CDI Softkey
Figure 4-20 Selecting a NAV Radio for Navigation
INDEX
APPENDICES
See the Flight Instruments Section for selecting the DME and Bearing Information windows and using VOR
or ADF as the source for the bearing pointer.
110
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
Select NAV radios for listening by pressing the corresponding keys on the Audio Panel. Pressing the NAV1,
NAV2, ADF, or DME Key selects and deselects the navigation radio source. Selected audio can be heard over the
headset and the speaker (if selected). All radios can be selected individually or simultaneously.
FLIGHT
INSTRUMENTS
EIS
Figure 4-21 Selecting a NAV Radio Receiver
AUDIO PANEL
& CNS
NAV RECEIVER MANUAL TUNING
The NAV frequency controls and frequency boxes are on the left side of the PFD and MFD.
Manually tuning a NAV frequency:
FLIGHT
MANAGEMENT
1) Turn the NAV Knob to tune the desired frequency in the NAV Tuning Box.
2) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field.
3) Adjust the volume level with the NAV VOL/ID Knob.
HAZARD
AVOIDANCE
4) Press the NAV VOL/ID Knob to turn the Morse code identifier audio on and off.
AFCS
Turn VOL/ID Knob to adjust
volume. Press Knob to Turn
Morse Code On or Off.
Press the Frequency Transfer Key to
Transfer NAV Frequencies Between
Active and Standby Frequency Fields
Turn the NAV Knob to
Tune the Frequency in
the Tuning Box
ADDITIONAL
FEATURES
Figure 4-22 NAV Frequency Tuning
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
111
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
Manual NAV frequency tuning from the MFD/PFD Control Unit:
1) Press the NAV Key to select the NAV frequency box.
FLIGHT
INSTRUMENTS
2) Turn the FMS NAV/COM Knob to tune the desired frequency in the NAV Tuning Box (large knob for MHz; small
knob for kHz).
Or:
Press the Numeric Keys on the keypad to enter a Frequency
3) Press the Frequency Transfer Key to transfer the frequency to the active field.
AUDIO PANEL
& CNS
EIS
If an error is made during frequency entry with the numeric keypad, pressing the BKSP Key moves the cursor
back one space. If an incorrect frequency is entered, reenter the correct one using the same procedure.
FLIGHT
MANAGEMENT
Second, turn the FMS NAV/COM Knob to enter a
Frequency into the COM Standby Frequency Field
HAZARD
AVOIDANCE
First, press the NAV
Key to place the
Tuning Selection
Box on the NAV
frequencies
Third, press the Frequency Transfer Key to move
the Frequency to the Active Field.
Figure 4-23 Frequency Tuning from the MFD/PFD Control Unit
SELECTING THE RADIO TO BE TUNED
ADDITIONAL
FEATURES
AFCS
Press the small NAV Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the
upper and lower radio frequency fields.
APPENDICES
Press the NAV Knob to
Switch the Tuning Box From
One NAV Radio to the Other
INDEX
Figure 4-24 Switching NAV Tuning Boxes
112
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
VOR/LOC ID
When the Morse code Identifier audio is on for a NAV radio, a white ID appears to the left of the active
NAV frequency.
FLIGHT
INSTRUMENTS
In the example shown, in order to listen to either station identifier, press the NAV1 or NAV2 Key on the
Audio Panel. Pressing the VOL/ID Knob turns off the Morse code audio only in the radio with the NAV
Tuning Box. To turn off both NAV IDs, transfer the NAV Tuning Box between NAV1 and NAV2 by pressing
the small NAV Knob and pressing the VOL/ID Knob again to turn the Morse code off in the other radio.
EIS
The Morse Code Identifier
for the GHM VOR is On
Station
Identifier
AUDIO PANEL
& CNS
Figure 4-25 NAV Radio ID Indication
VOLUME
FLIGHT
MANAGEMENT
Adjust NAV Radio volume level from 0 to 100% using the VOL/ID Knob. Turning the knob clockwise
increases volume, counterclockwise decreases volume.
When adjusting, the level is displayed in place of the standby frequencies. Volume level indication remains
for two seconds after the change.
HAZARD
AVOIDANCE
NAV Volume
Level Remains
for Two Seconds
Figure 4-26 NAV Volume Levels
AUTO-TUNING A NAV FREQUENCY FROM THE MFD
AFCS
Select and load NAV frequencies from the following MFD pages:
• WPT – Airport Information
• NRST – Nearest VOR
• NRST – Nearest Frequencies (FSS, WX)
• NRST – Nearest Airports
• NRST – Nearest Airspaces
ADDITIONAL
FEATURES
• WPT – VOR Information
APPENDICES
The MFD provides auto-tuning of NAV frequencies from waypoint and nearest pages. During enroute
navigation, the NAV frequency is entered automatically into the NAV standby frequency field. During approach
activation the NAV frequency is entered automatically into the NAV active frequency field.
Load frequencies into the NAV Frequency Box from pages in the NRST or WPT page group by highlighting
the frequency and pressing the ENT Key (Figures 4-28, 4-29, and 4-30).
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
113
SYSTEM
OVERVIEW
Auto-tuning a NAV frequency from the WPT and NRST Pages:
FLIGHT
INSTRUMENTS
AUDIO PANEL AND CNS
2) Turn the FMS Knob to place the cursor on the desired NAV identifier or NAV frequency.
1) From any page that the NAV frequency can be auto-tuned, activate the cursor by pressing the FMS Knob or the
appropriate softkey.
3) On the Nearest VOR, Nearest Airspaces, and Nearest Airports pages, select the FREQ Softkey to place the cursor
on the NAV frequency (Figure 4-29).
4) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio.
AUDIO PANEL
& CNS
EIS
5) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field.
Press the ENT
Key to Load
a Highlighted
Frequency into
the NAV Standby
Frequency Box
FLIGHT
MANAGEMENT
Turn the FMS
Knob to Scroll
Through a List
of Frequencies
Figure 4-27 NAV Frequency Auto-Tuning from the MFD
Or:
HAZARD
AVOIDANCE
1) When on the NRST pages, press the MENU Key to display the page menu.
2) Turn the large FMS Knob to scroll through the menu options.
3) Press the ENT Key to place the cursor in the desired window.
4) Scroll through the frequency selections with the FMS Knob.
AFCS
5) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio.
APPENDICES
ADDITIONAL
FEATURES
6) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field.
Nearest Airports Menu
Nearest VOR Menu
Nearest Frequencies Menu
Nearest Airspaces Menu
INDEX
Figure 4-28 Nearest Pages Menus
114
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
In the example shown, the VOR list is selected with the VOR Softkey or from the page menu. Use the FMS
Knob or ENT Key to scroll through the list. Place the cursor on the frequency with the FREQ Softkey and load
it into the NAV Tuning Box with the ENT Key.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Select the FREQ
Softkey to Place
the Cursor on the
VOR Frequency
HAZARD
AVOIDANCE
Select the VOR
Softkey to Place
the Cursor on the
VOR Identifier
FLIGHT
MANAGEMENT
Press the ENT
Key to Load
the Frequency
into the NAV
Standby Field.
Figure 4-29 Loading the NAV Frequency from the NRST – Nearest VOR Page
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
115
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
While enroute, tune NAV frequencies from the NRST – Nearest Airports, WPT – Airport Information,
WPT – VOR Information, and NRST – Nearest Frequencies Pages on the MFD in a similar manner using the
appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key.
INDEX
Figure 4-30 NRST – Nearest Frequencies, WPT – VOR Information, WPT – Airport Information, and
NRST – Nearest Airports Pages
116
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
AUTO-TUNING NAV FREQUENCIES ON APPROACH ACTIVATION
NOTE: The primary NAV frequency is auto-tuned upon loading a VOR or ILS/Localizer approach.
FLIGHT
INSTRUMENTS
NOTE: When an ILS/LOC approach has been activated in GPS Mode, the system switches to NAV Mode
as the final approach course is intercepted (within 15 nm of the FAF). See the GPS Navigation Section for
details.
NAV frequencies are automatically loaded into the NAV Frequency Box on approach activation.
EIS
When loading or activating a VOR or ILS/LOC approach, the approach frequency is automatically transferred
to a NAV frequency field as follows:
AUDIO PANEL
& CNS
• If the current CDI navigation source is GPS, the approach frequency is transferred to the NAV1 active
frequency field. The frequency that was previously in the NAV1 active frequency field is transferred to
standby.
• If the current CDI navigation source is GPS, and if the approach frequency is already loaded into the NAV1
standby frequency field, the standby frequency is transferred to active.
FLIGHT
MANAGEMENT
• If the current CDI navigation source is NAV1 or NAV2, the approach frequency is transferred to the standby
frequency fields of the selected CDI NAV radio.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
117
SYSTEM
OVERVIEW
MARKER BEACON RECEIVER
FLIGHT
INSTRUMENTS
AUDIO PANEL AND CNS
The marker beacon receiver is used as part of the ILS. The marker beacon receiver is always on and detects
any marker beacon signals within the reception range of the aircraft.
NOTE: The marker beacon indicators operate independently of marker beacon audio and cannot be disabled.
The receiver detects the three marker tones – outer, middle, and inner – and provides the marker beacon
annunciations located to the left of the Altimeter on the PFD.
Middle Marker
Indication
Inner Marker
Indication
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Outer Marker
Indication
HAZARD
AVOIDANCE
Figure 4-31 Marker Beacon Annunciations on the PFD
Figure 4-32 Marker Beacon Keys
AFCS
The Audio Panel provides three different states of marker beacon operation; On, Muted, and Deselected. Pressing the MKR/MUTE Key selects and deselects marker beacon audio. The key annunciator indicates when
marker beacon audio is selected.
ADDITIONAL
FEATURES
During marker beacon audio reception, pressing the MKR/MUTE Key mutes the audio but does not affect the
marker annunciations (Figure 4-30). The marker tone is silenced, then waits for the next marker tone. The
MKR/MUTE Key Annunciator is illuminated, indicating audio muting. The audio returns when the next marker
beacon signal is received. If the MKR/MUTE Key is pressed during signal reception (O, M, I indication) while
marker beacon audio is muted, the audio is deselected and the MKR/MUTE Key Annunciator is extinguished.
INDEX
APPENDICES
Pressing the HI SENS Key switches between high and low marker beacon receiver sensitivity. The HI SENS
function (annunciator illuminated) is used to provide an earlier indication when nearing a marker during an
approach. The LO SENS function (annunciator extinguished) results in a narrower marker dwell while over a
station.
118
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
ADF/DME TUNING
NOTE: When another auxiliary window is turned on, the ADF/DME Tuning Window is replaced on the PFD.
FLIGHT
INSTRUMENTS
See the Flight Instruments Section for displaying the DME and bearing information windows (ADF) and
using the ADF as the source for the bearing pointer.
The G1000 system tunes the ADF receiver (optional) and DME transceiver (optional). Tune the ADF by
entering the frequency in the ADF standby frequency field of the ADF/DME Tuning Window. (The softkey may
be labeled ADF/DME, ADF, or DME, depending on installed equipment.)
EIS
Tune the UHF DME frequency by pairing with a VHF NAV frequency. DME frequency pairing is automatic
and only the VHF NAV frequency is shown.
The following ADF/DME information is displayed in the ADF/DME Tuning Window:
AUDIO PANEL
& CNS
• Active and standby ADF frequencies
• ADF receiver mode
• ADF receiver volume
FLIGHT
MANAGEMENT
• DME tuning mode (DME transceiver pairing)
When the ADF/DME Tuning Window is displayed, the selection cursor is placed over the standby ADF
frequency field.
Active ADF Frequency
HAZARD
AVOIDANCE
Turning the large FMS Knob moves the selection cursor through the various fields (standby ADF frequency,
ADF receiver mode, ADF radio volume, and DME tuning mode). Pressing the FMS Knob activates/deactivates
the selection cursor in the ADF/DME Tuning Window. Enter the ADF frequency using the FMS Knob and the
ENT Key.
Standby ADF Frequency
AFCS
ADF
Volume
ADF
Mode
ADDITIONAL
FEATURES
DME
Tuning
Mode
Figure 4-33 ADF/DME Tuning Window
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
119
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
ADF TUNING
FLIGHT
INSTRUMENTS
ADF frequencies in the 190.0-kHz to 1799.5-kHz range are entered in the standby ADF frequency field of the
ADF/DME Tuning Window. The G1000 System does not tune the ADF emergency frequency, 2182.0‑kHz.
Tuning an ADF frequency:
1) Press the ADF/DME Softkey to display the ADF/DME Tuning Window.
2) Turn the large FMS Knob to place the selection cursor over the standby ADF frequency field.
3) Turn the small FMS Knob to begin data entry and change each digit.
EIS
4) Turn the large FMS Knob to move the cursor to the next digit position.
AUDIO PANEL
& CNS
5) Press the ENT Key to complete data entry for the standby frequency.
Press the
ENT Key to
Complete ADF
Frequency Entry
FLIGHT
MANAGEMENT
Turn the Small
FMS Knob to
Enter Data in
the Standby ADF
Frequency Field
Turn the Large
FMS Knob
to Move the
Cursor to the
Next Character
Figure 4-34 Entering ADF Standby Frequencies
HAZARD
AVOIDANCE
Pressing the CLR Key before completing frequency entry cancels the frequency change and reverts back to
the previously entered frequency.
Pressing the CLR Key when the cursor is flashing, clears the frequency and replaces the standby field with
0000.0.
AFCS
Transferring the active and standby ADF frequencies:
1) Turn the large FMS Knob to place the selection cursor over the standby ADF frequency field.
2) Press the ENT Key to complete the frequency transfer.
APPENDICES
ADDITIONAL
FEATURES
Press the ENT
Key to Transfer
the ADF
Frequencies
INDEX
Figure 4-35 Transferring ADF Frequencies
120
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
SELECTING ADF RECEIVER MODE
Select the following modes: (In all modes NDB audio can be heard by selecting the ADF Key on the Audio
Panel.)
FLIGHT
INSTRUMENTS
• ANT (Antenna) – The ADF bearing pointer parks on the HSI at 90 degrees. Best mode for listening to NDB
audio.
• ADF (Automatic Direction Finder) – The ADF pointer points to the relative bearing of the NDB station.
EIS
• ADF/BFO (ADF/Beat Frequency Oscillator) – The ADF pointer points to the relative bearing of the NDB
station and an audible tone confirms signal reception. This mode allows identification of the interrupted
carrier beacon stations used in various parts of the world.
AUDIO PANEL
& CNS
• ANT/BFO (Antenna/Beat Frequency Oscillator) – The ADF bearing pointer parks on the HSI at 90 degrees
while an audible tone is provided when a signal is received. This mode also allows identification of the
interrupted carrier beacon stations and confirms signal reception.
Selecting an ADF receiver mode:
1) Turn the large FMS Knob to place the selection cursor over the ADF mode field.
FLIGHT
MANAGEMENT
2) Turn the small FMS Knob to select the desired ADF receiver mode.
Turn the Small
FMS Knob
to Select the
Mode
HAZARD
AVOIDANCE
Figure 4-36 Selecting ADF Receiver Mode
AFCS
Adjust ADF receiver volume level in the tuning window from 0 to 100%. The default volume level is set to
50%. The ADF volume level is the same for both Audio Panels.
Adjusting ADF receiver volume:
ADDITIONAL
FEATURES
1) Turn the large FMS Knob to place the selection cursor over the ADF volume field.
2) Turn the small FMS Knob to adjust volume as desired.
APPENDICES
Turn the Small
FMS Knob
to Select the
Volume
INDEX
Figure 4-37 Adjusting ADF Receiver Volume
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
121
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
DME TUNING
NOTE: When turning on the G1000 for use, the system remembers the last frequency used for DME tuning
FLIGHT
INSTRUMENTS
and the NAV1, NAV2, or HOLD state prior to shutdown.
EIS
Select NAV1, NAV2, or HOLD in the ADF/DME Tuning Window to tune the DME transceiver.
AUDIO PANEL
& CNS
DME
Modes
Figure 4-38 ADF/DME Tuning Window, DME Modes
Select the following DME transceiver pairings:
FLIGHT
MANAGEMENT
• NAV1 – Pairs the DME frequency from the selected NAV1 frequency.
• NAV2 – Pairs the DME frequency from the selected NAV2 frequency.
• HOLD – When in the HOLD position, the DME frequency remains paired with the last selected NAV
frequency.
HAZARD
AVOIDANCE
Selecting DME transceiver pairing:
1) Press the ADF/DME Softkey to display the ADF/DME Tuning Window.
2) Turn the small FMS Knob to select the DME tuning mode.
3) Press the ENT Key to complete the selection.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Pressing the CLR Key or FMS Knob while in the process of DME pairing cancels the data entry and reverts
back to the previously selected DME tuning state. Pressing the FMS Knob activates/deactivates the cursor in
the ADF/DME Tuning Window.
122
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
4.4 GTX 33 MODE S TRANSPONDER
FLIGHT
INSTRUMENTS
The GTX 33 Mode S Transponder provides Mode A, Mode C, and Mode S interrogation and reply capabilities.
Selective addressing or Mode Select (Mode S) capability includes the following features:
• Level-2 reply data link capability to exchange information between aircraft and Air Traffic Control (ATC)
facilities
• Surveillance identifier capability
EIS
• Flight ID (Flight Identification) reporting – The Mode S Transponder reports aircraft identification as the aircraft
registration.
• Altitude reporting
• Airborne status determination
AUDIO PANEL
& CNS
• Transponder capability reporting
• Mode S Enhanced Surveillance (EHS) requirements
FLIGHT
MANAGEMENT
• Acquisition squitter – Acquisition squitter, or short squitter, is the transponder 24-bit identification address. The transmission is sent periodically, regardless of the presence of interrogations. The purpose of acquisition
squitter is to enable Mode S ground stations and aircraft equipped with a Traffic Avoidance System (TAS) to
recognize the presence of Mode S-equipped aircraft for selective interrogation.
The Hazard Avoidance Section provides more details on traffic avoidance systems.
HAZARD
AVOIDANCE
TRANSPONDER CONTROLS
Transponder function is displayed on three levels of softkeys on the PFD: Top-level, Mode Selection, and
Code Selection. When the top-level XPDR Softkey is pressed, the Mode Selection softkeys appear: STBY, ON,
ALT, VFR, CODE, IDENT, BACK.
AFCS
When the CODE Softkey is selected, the number softkeys appear: 0, 1, 2, 3, 4, 5, 6, 7, IDENT, BKSP,
BACK. The digits 8 and 9 are not used for code entry. Selecting the numbered softkeys in sequence enters
the transponder code. If an error is made, selecting the BKSP Softkey moves the code selection cursor to the
previous digit. Selecting the BKSP Softkey again moves the cursor to the next previous digit.
ADDITIONAL
FEATURES
Selecting the BACK Softkey during code selection reverts to the Mode Selection Softkeys. Selecting the BACK
Softkey during mode selection reverts to the top-level softkeys.
The code can also be entered with the FMS Knob on the PFD or MFD/PFD Control Unit. Code entry must
be completed with either the softkeys or the FMS Knob, but not a combination of both.
APPENDICES
Selecting the IDENT Softkey while in Mode or Code Selection initiates the ident function and reverts to the
top-level softkeys.
After 45 seconds of transponder softkey inactivity, the system reverts back to the top-level softkeys.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
123
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
STBY
ON
ALT
GND
VFR
XPDR
IDENT
CODE
IDENT
BACK
ALERTS
EIS
Selecting the IDENT or BACK Softkey
returns to the top-level softkeys.
1
AUDIO PANEL
& CNS
0
2
3
4
5
6
7
IDENT
BKSP
BACK
ALERTS
Selecting the IDENT Softkey returns to the top-level softkeys.
Selecting the BACK Softkey returns to the mode selection softkeys.
FLIGHT
MANAGEMENT
Figure 4-39 Transponder Softkeys (PFD)
TRANSPONDER MODE SELECTION
Mode selection can be automatic (Ground and Altitude Modes) or manual (Standby, ON, and Altitude Modes).
The STBY, ON, and ALT Softkeys can be accessed by selecting the XPDR Softkey.
HAZARD
AVOIDANCE
Selecting a transponder mode:
1) Select the XPDR Softkey to display the Transponder Mode Selection Softkeys.
2) Select the desired softkey to activate the transponder mode.
AFCS
GROUND MODE
ADDITIONAL
FEATURES
Ground Mode is normally selected automatically when the aircraft is on the ground. The transponder
powers up in the last mode it was in when shut down. Ground Mode can be overridden by selecting any one
of the Mode Selection Softkeys. A green GND indication and transponder code appear in the mode field of
the Transponder Data Box. In Ground Mode, the transponder does not allow Mode A and Mode C replies,
but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations.
When Standby Mode has been selected on the ground, press the GND Softkey to return the transponder
to Ground Mode.
APPENDICES
GND
Mode
INDEX
Figure 4-40 Ground Mode
124
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
STANDBY MODE (MANUAL)
NOTE: In Standby Mode, the IDENT function is inoperative.
FLIGHT
INSTRUMENTS
Press the STBY Softkey at any time to select Standby Mode. In Standby, the transponder does not reply
to interrogations, but new codes can be entered. When Standby is selected, a white STBY indication and
transponder code appear in the mode field of the Transponder Data Box. In all other modes, these fields
appear in green.
EIS
STBY Mode (White
Code Number and
Mode)
Figure 4-41 Standby Mode
AUDIO PANEL
& CNS
MANUAL ON MODE
FLIGHT
MANAGEMENT
Press the ON Softkey at any time to select ON Mode. ON Mode generates Mode A and Mode S replies, but
Mode C altitude reporting is inhibited. In ON Mode, a green ON indication and transponder code appear in
the mode field of the Transponder Data Box.
ON Mode
(No Altitude
Reporting)
HAZARD
AVOIDANCE
Figure 4-42 ON Mode
ALTITUDE MODE (AUTOMATIC OR MANUAL)
AFCS
Altitude Mode is automatically selected when the aircraft becomes airborne. Press the ALT Softkey to
manually select Altitude Mode.
ADDITIONAL
FEATURES
If Altitude Mode is selected, a green ALT indication and transponder code appear in the mode field of the
Transponder Data Box, and all transponder replies requesting altitude information are provided with pressure
altitude information.
ALT Mode
(Mode C Altitude
Reporting)
APPENDICES
Figure 4-43 Altitude Mode
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
125
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
REPLY STATUS
FLIGHT
INSTRUMENTS
When the transponder sends replies to interrogations, a white R indication appears momentarily in the
reply status field of the Transponder Data Box.
Reply to
Interrogation
Figure 4-44 Reply Indication
EIS
ENTERING A TRANSPONDER CODE
Entering a transponder code with softkeys:
AUDIO PANEL
& CNS
1) Select the XPDR Softkey to display the Transponder Mode Selection Softkeys.
2) Select the CODE Softkey to display the Transponder Code Selection Softkeys, for digit entry.
FLIGHT
MANAGEMENT
3) Select the digit softkeys to enter the code in the code field. When entering the code, the next softkey in
sequence must be selected within 10 seconds, or the entry is cancelled and restored to the previous code. Select
the BKSP Softkey to move the code selection cursor to the previous digit. Five seconds after the fourth digit has
been entered, the transponder code becomes active.
HAZARD
AVOIDANCE
Entering
a Code
Figure 4-45 Entering a Code
Entering a transponder code with the PFD FMS Knob:
AFCS
1) Select the XPDR and the CODE Softkeys as in the previous procedure to enable code entry.
2) Turn the small FMS Knob on the PFD to enter the first two code digits.
3) Turn the large FMS Knob to move the cursor to the next code field.
ADDITIONAL
FEATURES
4) Enter the last two code digits with the small FMS Knob.
5) Press the ENT Key to complete code digit entry.
APPENDICES
Pressing the CLR Key or small FMS Knob before code entry is complete cancels code entry and restores the
previous code. Waiting for 10 seconds after code entry is finished activates the code automatically.
INDEX
Turn the Small
FMS Knob to
Enter Two Code
Digits at a Time
Press the ENT Key to
Complete Code Entry
Turn the Large FMS
Knob to Move the
Cursor to the Next
Code Field
Figure 4-46 Entering a Code with the FMS Knob
126
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
VFR CODE
Press the XPDR Softkey, then the VFR Softkey to display the pre-programmed VFR code in the code field of
the Transponder Data Box. Press the VFR Softkey again to restore the previous identification code.
FLIGHT
INSTRUMENTS
The pre-programmed VFR Code is set at the factory to 1200. If a VFR code change is required, contact a
Garmin-authorized service center for configuration.
VFR Code
EIS
Figure 4-47 VFR Code
AUDIO PANEL
& CNS
IDENT FUNCTION
NOTE: In Standby Mode, the IDENT Softkey is inoperative.
FLIGHT
MANAGEMENT
Select the IDENT Softkey to send a distinct identity indication to Air Traffic Control (ATC). The indication
distinguishes the identing transponder from all the others on the air traffic controller’s screen. The IDENT
Softkey appears on all levels of transponder softkeys. When the IDENT Softkey is selected, a green IDNT
indication is displayed in the mode field of the Transponder Data Box for a duration of 18 seconds.
After the IDENT Softkey is selected while in Mode or Code Selection, the system reverts to the top-level
softkeys.
HAZARD
AVOIDANCE
IDNT
Indication
Select the
IDENT Softkey
to Initiate the
ID Function
AFCS
Figure 4-48 IDENT Softkey and Indication
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
127
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
4.5 ADDITIONAL AUDIO PANEL FUNCTIONS
FLIGHT
INSTRUMENTS
POWER-UP
The Audio Panel performs a self-test during power-up. During the self-test all Audio Panel annunciator lights
illuminate for approximately two seconds. Once the self-test is completed, most of the settings are restored to
those in use before the unit was last turned off.
MONO/STEREO HEADSETS
EIS
Stereo headsets are recommended for use in this aircraft.
AUDIO PANEL
& CNS
Using a monaural headset in a stereo jack shorts the right headset channel output to ground. While this does
not damage the Audio Panel, a person listening on a monaural headset hears only the left channel in both ears.
If a monaural headset is used at one of the passenger positions, any other passenger using a stereo headset hears
audio in the left ear only.
SPEAKER
FLIGHT
MANAGEMENT
All of the radios can be heard over the cabin speaker. Press the SPKR Key to select and deselect the cabin
speaker. Speaker audio is muted when the PTT is pressed. Certain aural alerts and warnings (autopilot, traffic,
altitude) are always heard on the speaker, even when the speaker is not selected.
HAZARD
AVOIDANCE
The speaker volume is adjustable within a nominal range. Contact a Garmin-authorized service center for
volume adjustment.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 4-49 Passenger Address and Speaker Keys
128
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
INTERCOM
FLIGHT
INSTRUMENTS
The Audio Panel includes a four-position intercom system (ICS) and two stereo music inputs for the pilot,
copilot and up to four passengers. The intercom provides Pilot and Copilot isolation from the passengers and
aircraft radios.
EIS
Figure 4-50 Intercom Controls
PILOT KEY
Annunciator
COPLT KEY
Annunciator
Pilot Hears
Copilot Hears
OFF
OFF
Selected radios, aural
alerts, pilot, copilot,
passengers, MUSIC 1
Selected radios, aural
alerts, pilot, copilot,
passengers, MUSIC 1
Selected radios, aural alerts, pilot,
copilot, passengers, MUSIC 2
ON
OFF
Selected radios, aural
alerts, pilot
Copilot, passengers,
MUSIC 1
Copilot,
passengers,
MUSIC 2
OFF
ON
Selected radios,
aural alerts, pilot;
passengers, MUSIC 1
Copilot
Selected radios, aural alerts, pilot,
passengers, MUSIC 2
ON
ON
Selected radios, aural
alerts, pilot, copilot
Selected radios, aural
alerts, pilot, copilot
Passengers; MUSIC 2
AUDIO PANEL
& CNS
Passenger Hears
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
Table 4-1 ICS Isolation Modes
ADDITIONAL
FEATURES
Pilot isolation is selected when the PILOT Annunciator is illuminated. During Pilot isolation, the pilot can
hear the selected radios and aural alerts and warnings. The copilot and passengers can communicate with each
other. The copilot is isolated from aural alerts and warnings.
Copilot isolation is selected when the COPLT Annunciator is illuminated. The copilot is isolated from the
selected radios, aural alerts and warnings, and everyone else. The pilot and passengers can hear the selected
radios, aural alerts, and communicate with each other.
APPENDICES
When both the PILOT and COPLT Annunciators are illuminated, the pilot and copilot can hear the selected
radios, aural alerts, and communicate with each other. The passengers are isolated from the pilot and copilot
but can communicate with each other.
When both the PILOT and COPLT Annunciators are extinguished, everyone hears the selected radios, aural
alerts, and is able to communicate with everyone else.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
129
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
INTERCOM VOLUME AND SQUELCH
FLIGHT
INSTRUMENTS
The PILOT/PASS Knob controls volume or manual squelch adjustment for the pilot and copilot/passenger.
The small knob controls the pilot volume and squelch. The large knob controls the copilot/passenger volume
and squelch. The VOL and SQ annunciations at the bottom of the unit indicate which function the knob is
controlling. Pressing the PILOT/PASS Knob switches between volume and squelch control as indicated by
the VOL or SQ annunciation being illuminated.
The MAN SQ Key allows either automatic or manual control of the squelch setting.
EIS
• When the MAN SQ Annunciator is extinguished (Automatic Squelch is on), the PILOT/PASS Knob
controls only the volume (pressing the PILOT/PASS Knob has no effect on the VOL/SQ selection).
AUDIO PANEL
& CNS
• When the MAN SQ Annunciator is illuminated (Manual Squelch), the PILOT/PASS Knob controls
either volume or squelch (selected by pressing the PILOT/PASS Knob and indicated by the VOL or SQ
annunciation).
FLIGHT
MANAGEMENT
Manual Squelch Annunciator;
Off for Automatic Squelch, On
for Manual Squelch
Automatic/Manual Squelch
HAZARD
AVOIDANCE
Pilot Volume or Manual
Squelch. Press to switch
between VOL and SQ. Turn
to adjust Squelch when SQ
Annunciation is lit, Volume
when VOL Annunciation is lit.
Copilot/Passenger
Volume or
Manual Squelch
AFCS
Volume Annunciation
Squelch Annunciation
INDEX
APPENDICES
ADDITIONAL
FEATURES
Figure 4-51 Volume/Squelch Control
130
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
PASSENGER ADDRESS (PA) SYSTEM
FLIGHT
INSTRUMENTS
A passenger address system is available for delivering voice messages over the cabin speaker. When the PA
Key is selected on the Audio Panel, the COM MIC Annunciator is extinguished, and the active COM frequency
changes to white, indicating that there is no COM selected. A Push-to-Talk (PTT) must be pressed to deliver PA
announcements. The PA Annunciator flashes about once per second while the PTT is depressed.
EIS
PA Key is Selected on
the Audio Panel
AUDIO PANEL
& CNS
Figure 4-52 PA Key Selected for Cabin Announcements
FLIGHT
MANAGEMENT
CLEARANCE RECORDER AND PLAYER
The Audio Panel contains a digital clearance recorder that records up to 2.5 minutes of the selected COM
radio signal. Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes of recording time
have been reached, the recorder begins recording over the stored memory blocks, starting from the oldest
block.
HAZARD
AVOIDANCE
The PLAY Key controls the play function. Press the PLAY Key once to play the latest recorded memory block.
The PLAY Annunciator flashes to indicate when play is in progress. The PLAY Annunciator turns off after the
present memory block has finished playing.
Press the MKR/MUTE Key during play of a memory block to stop play. If a COM input signal is detected
during play of a recorded memory block, play is halted.
AFCS
Press the PLAY Key while audio is playing to play the previously recorded memory block. Each subsequent
press of the PLAY Key selects the previously recorded memory block.
Powering off the unit automatically clears all recorded blocks.
ADDITIONAL
FEATURES
MKR/MUTE
Key Stops Play
APPENDICES
PLAY Key
Controls the
Play Function
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
Figure 4-53 Marker Mute and Play Keys
131
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
SPLIT COM
NOTE: Split COM performance is affected by the distance between the COM antennas and the separation
FLIGHT
INSTRUMENTS
of the tuned frequencies. If the selected COM1 and COM2 frequencies are too close together, interference
may be heard during transmission on the other radio.
During Split COM operation, both the pilot and the copilot can transmit simultaneously over separate radios.
The pilot can still monitor NAV1, NAV2, ADF, DME, and MKR Audio as selected, but the copilot is only able
to monitor COM2.
AUDIO PANEL
& CNS
EIS
Pressing the COM 1/2 Key selects Split COM operation. The COM 1/2 Annunciator is illuminated indicating
Split COM operation. COM1 and COM2 frequencies are displayed in green indicating that both transceivers
are active. Split COM operation is cancelled by pressing the COM 1/2 Key again, at which time the annunciator
is extinguished.
FLIGHT
MANAGEMENT
When Split COM operation is selected, COM1 is used by the pilot and COM2 is used by the copilot. The
COM1 MIC Annunciator flashes when the pilot’s microphone PTT is pressed. The COM2 MIC Annunciator
flashes when the copilot’s microphone PTT is pressed.
HAZARD
AVOIDANCE
COM1 Radio is Used
by the Pilot
AFCS
COM2 Radio is Used
by the Copilot
INDEX
APPENDICES
ADDITIONAL
FEATURES
Figure 4-54 Split COM Operation
132
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
ENTERTAINMENT INPUTS
NOTE: MUSIC 1 and MUSIC 2 inputs cannot be completely turned off. Audio level for MUSIC 1 and MUSIC 2
FLIGHT
INSTRUMENTS
can be adjusted by a Garmin-authorized service center.
The Audio Panel provides two stereo auxiliary entertainment inputs: MUSIC 1 and MUSIC 2. These inputs
are compatible with popular portable entertainment devices such as MP3 and CD players. Two 3.5-mm
stereo phone jacks are installed in convenient locations for audio connection. The headphone outputs of the
entertainment devices are plugged into the MUSIC 1 or MUSIC 2 jacks.
EIS
The current ICS state of isolation affects the distribution of the entertainment input MUSIC 1 (see
Table 4‑1).
MUSIC 1
AUDIO PANEL
& CNS
MUSIC 1 can be heard by the pilot and copilot when both the PILOT and the COPLT Annunciators are
extinguished. MUSIC 1 can also be heard by the pilot when the COPLT Annunciator is illuminated and by
the copilot when the PILOT Annunciator is illuminated.
FLIGHT
MANAGEMENT
MUSIC 1 Muting
MUSIC 1 muting occurs when aircraft radio or marker beacon activity is heard. MUSIC 1 is always soft
muted when an interruption occurs from these sources. Soft muting is the gradual return of MUSIC 1 to
its original volume level. The time required for MUSIC 1 volume to return to normal is between one-half
and four seconds.
HAZARD
AVOIDANCE
MUSIC 2
MUSIC 2 can be heard only by the passengers and is never muted.
XM RADIO ENTERTAINMENT
AFCS
XM Radio audio from the Data Link Receiver may be heard by the pilot and passengers simultaneously
(optional: requires subscription to XM Radio Service). Refer to the Additional Features Section for more
details on the Data Link Receiver.
ADDITIONAL
FEATURES
Connecting a stereo input to either MUSIC 1 or MUSIC 2 jacks removes the XM Radio Audio from that input. For example, if passengers prefer their own music while the pilot listens to the XM Radio, the entertainment
audio should be connected to the MUSIC 2 jack.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
133
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
4.6 AUDIO PANEL PREFLIGHT PROCEDURE
FLIGHT
INSTRUMENTS
NOTE: If the pilot and/or copilot are using headsets that have a high/low switch or volume control knob,
verify that the switch is in the high position and the volume control on the headsets are at maximum volume
setting. On single‑pilot flights, verify that all other headsets are not connected to avoid excess noise in the
audio system.
NOTE: When the MAN SQ Key is pressed, the ICS squelch can be set manually by the pilot and copilot. If
EIS
manual squelch is set to full open (SQ annunciated and the knobs turned counterclockwise) background
noise is heard in the ICS system as well as during COM transmissions.
AUDIO PANEL
& CNS
After powering up the G1000 System, the following steps will aid in maximizing the use of the Audio Panel as
well as prevent pilot and copilot induced issues. These preflight procedures should be performed each time a
pilot boards the aircraft to ensure awareness of all audio levels in the Audio Panel and radios.
FLIGHT
MANAGEMENT
Automatic/Manual
Squelch
HAZARD
AVOIDANCE
Pilot and
Copilot ICS
Isolation Keys
Pilot Volume
or Manual
Squelch
Copilot/Passenger
Volume or
Manual Squelch
Squelch
Annunciation
AFCS
Volume
Annunciation
ADDITIONAL
FEATURES
Figure 4-55 Audio Panel Controls
Setting the Audio Panel during preflight:
1) Verify that the PILOT and COPLT Annunciators are extinguished.
APPENDICES
2) Verify that manual squelch is set to full open.
3) Turn the PILOT/PASS Knobs clockwise two full turns. This will set the headset intercom audio level to max
volume (least amount of attenuation).
4) Adjust radio volume levels (COM, NAV, etc.) to a suitable level.
5) Adjust the PILOT/PASS Knob volume to the desired intercom level.
INDEX
6) Reset squelch to automatic, or adjust to the appropriate level manually.
Once this procedure has been completed, the pilot and copilot can change settings, keeping in mind the notes
above.
134
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUDIO PANEL AND CNS
SYSTEM
OVERVIEW
4.7 ABNORMAL OPERATION
FLIGHT
INSTRUMENTS
Abnormal operation of the G1000 includes equipment failures of the G1000 components and failure of
associated equipment, including switches and external devices.
STUCK MICROPHONE
If the push-to-talk (PTT) Key becomes stuck, the COM transmitter stops transmitting after 35 seconds of
continuous operation. An alert appears on the PFD to advise the pilot of a stuck microphone.
EIS
The COM1 MIC or COM2 MIC Key Annunciator on the Audio Panel flashes as long as the PTT Key remains
stuck.
AUDIO PANEL
& CNS
Figure 4-56 Stuck Microphone Alert
FLIGHT
MANAGEMENT
COM TUNING FAILURE
In case of a COM system tuning failure, the emergency frequency (121.500 MHz) is automatically tuned in
the radio in which the tuning failure occurred. Depending on the failure mode, a red X may appear on the
frequency display.
HAZARD
AVOIDANCE
Emergency Channel
Loaded Automatically
Figure 4-57 COM Tuning Failure
AFCS
AUDIO PANEL FAIL-SAFE OPERATION
If there is a failure of the Audio Panel, a fail-safe circuit connects the pilot’s headset and microphone directly
to the COM1 transceiver. Audio will not be available on the speaker.
ADDITIONAL
FEATURES
REVERSIONARY MODE
The red DISPLAY BACKUP Button selects Reversionary Mode for both displays. Reversionary Mode
operation displays flight and engine information on both the PFD and MFD, in case of display failure.
APPENDICES
See the System Overview Section for more information on the DISPLAY BACKUP Button.
INDEX
Figure 4-58 Display Backup Button
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
135
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
AUDIO PANEL AND CNS
Blank Page
136
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
SECTION 5 FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
5.1 INTRODUCTION
The G1000 is an integrated flight, engine, communication, navigation and surveillance system. This section of
the Pilot’s Guide explains GPS navigation using the G1000.
EIS
The most prominent part of the G1000 are the two full color displays: one Primary Flight Display (PFD) and
one Multi Function Display (MFD). The information to successfully navigate the aircraft using the GPS sensors is
displayed on the PFD and the MFD. See examples in the Figure 5-1 and Figure 5-2. Detailed descriptions of GPS
navigation functions are discussed later in this section.
A brief description of the GPS navigation data on the PFD and MFD follows.
AUDIO PANEL
& CNS
Navigation mode indicates which sensor is providing the course data (e.g., GPS, VOR) and the flight plan phase
(e.g., Departure (DPRT), Terminal (TERM), Enroute (ENR), Oceanic (OCN), Approach (LNAV, LNAV+V, L/VNAV,
or LPV), or Missed Approach (MAPR)). L/VNAV and LPV approaches are only available with SBAS.
FLIGHT
MANAGEMENT
The Inset Map is a small version of the MFD Navigation Map and can be displayed in the lower left corner of
the PFD. When the system is in reversionary mode, the Inset Map is displayed in the lower right corner. The
Inset Map is displayed by selecting the INSET Softkey. Selecting the INSET Softkey again, then selecting the OFF
Softkey removes the Inset Map.
HAZARD
AVOIDANCE
The Navigation Map displays aviation data (e.g., airports, VORs, airways, airspaces), geographic data (e.g.,
cities, lakes, highways, borders), topographic data (map shading indicating elevation), and hazard data (e.g.,
traffic, terrain, weather). The amount of displayed data can be reduced by selecting the DCLTR Softkey. The
Navigation Map can be oriented four different ways: North Up (NORTH UP), Track Up (TRK UP), Desired Track
Up (DTK UP), or Heading Up (HDG UP).
AFCS
An aircraft icon is placed on the Navigation Map at the location corresponding to the calculated present position.
The aircraft position and the flight plan legs are accurately based on GPS calculations. The basemap upon which
these are placed are from a source with less resolution, therefore the relative position of the aircraft to map features
is not exact. The leg of the active flight plan currently being flown is shown as a magenta line on the navigation
map. The other legs are shown in white.
ADDITIONAL
FEATURES
There are 28 different map ranges available, from 500 feet to 2000 nm. The current range is indicated in the
lower right corner of the map and represents the top-to-bottom distance covered by the map. To change the map
range on any map, turn the Joystick counter-clockwise to zoom in ( -, decreasing), or clockwise to zoom out (+,
increasing).
APPENDICES
The Direct-to Window, the Flight Plan Window, the Procedures Window, and the Nearest Airports Window
can be displayed in the lower right corner of the PFD. Details of these windows are discussed in detail later in
the section.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
137
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
Navigation Status Box
Current Track
Indicator
Navigation Mode
Inset Map
AUDIO PANEL
& CNS
EIS
Location of:
- Direct To Window
- Flight Plan Window
- Procedures Window
- Nearest Airports Window
Figure 5-1 GPS Navigation Information on the PFD
FLIGHT
MANAGEMENT
Navigation Status Box
Map Orientation
Navigation Page Title
Navigation Map
HAZARD
AVOIDANCE
- Aviation Data
- Geographic Data
- Topographic Data
- Hazard Data
Aircraft Icon
at Present Position
Active Flight Plan Leg
ADDITIONAL
FEATURES
AFCS
Flight Plan Leg
Map Range
APPENDICES
Figure 5-2 GPS Navigation Information on the MFD Navigation Page
NAVIGATION STATUS BOX
INDEX
The Navigation Status Box located at the top of the PFD contains two fields displaying the following
information:
PFD Navigation Status Box
138
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
• Distance (DIS) and Bearing (BRG) to the next
waypoint or flight plan annunciations (e.g., ‘TOD
within 1 minute’)
• Bearing (BRG)
The symbols used in the PFD status bar are:
Symbol
Direct-to
Left Procedure Turn
Right Holding Pattern
• Desired Track (DTK)
• Endurance (END)
• Enroute Safe Altitude (ESA)
• Estimated Time of Arrival (ETA)
• Estimated Time Enroute (ETE)
• Fuel on Board (FOB)
• Fuel over Destination (FOD)
• Ground Speed (GS)
• Minimum Safe Altitude (MSA)
• True Air Speed (TAS)
Vector to Final
• Track Angle Error (TKE)
• Track (TRK)
• Vertical Speed Required (VSR)
HAZARD
AVOIDANCE
Left DME Arc
FLIGHT
MANAGEMENT
Left Holding Pattern
Right DME Arc
AUDIO PANEL
& CNS
Right Procedure Turn
• Distance (DIS)
EIS
Description
Active Leg
FLIGHT
INSTRUMENTS
The Navigation Status Box located at the top of the
MFD contains four data fields, each displaying one of
the following items:
SYSTEM
OVERVIEW
• Active flight plan leg (e.g., ‘D-> KICT’ or ‘KIXD ->
KCOS’) or flight plan annunciations (e.g., ‘Turn
right to 021˚ in 8 seconds’)
• Crosstrack Error (XTK)
AFCS
MFD Navigation Status Box
ADDITIONAL
FEATURES
The navigation information displayed in the four data fields can be selected on the MFD Data Bar Fields Box
on the AUX - System Setup Page. The default selections (in order left to right) are GS, DTK, TRK, and ETE.
Changing a field in the MFD Navigation Status Box:
1) Select the System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
APPENDICES
3) Turn the large FMS Knob to highlight the desired field number in the MFD Data Bar Fields Box.
4) Turn the small FMS Knob to display and scroll through the data options list.
5) Select the desired data.
6) Press the ENT Key. Selecting the DFLTS Softkey returns all fields to the default setting.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
139
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
5.2 USING MAP DISPLAYS
FLIGHT
INSTRUMENTS
Map displays are used extensively in the G1000 to provide situational awareness in flight. Most G1000 maps
can display the following information:
• Airports, NAVAIDs, airspaces, airways, land data
(highways, cities, lakes, rivers, borders, etc.) with
names
AUDIO PANEL
& CNS
EIS
• Map Pointer information (distance and bearing
to pointer, location of pointer, name, and other
pertinent information)
• Aircraft icon (representing present position)
• Nav range ring
• Fuel range ring
• Flight plan legs
• User waypoints
• Map range
• Track vector
• Wind direction and speed
• Topography scale
• Map orientation
• Topography data
• Icons for enabled map features
• Obstacle data
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
The information in this section applies to the following maps unless otherwise noted:
• All Map Group Pages (MAP)
• Flight Plan Pages (FPL)
• All Waypoint Group Pages (WPT)
• Direct-to Window
• AUX - Trip Planning
• PFD Inset Map
• All Nearest Group Pages (NRST)
• Procedure Loading Pages
MAP ORIENTATION
APPENDICES
ADDITIONAL
FEATURES
AFCS
Maps are shown in one of four different orientation options, allowing flexibility in determining aircraft
position relative to other items on the map (north up) or for determining where map items are relative to where
the aircraft is going (track up, desired track up, or heading up). The map orientation is shown in the upper
right corner of the map.
INDEX
Figure 5-3 Map Orientation
140
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
• North up (NORTH UP) aligns the top of the map display to north (default setting).
• Track up (TRK UP) aligns the top of the map display to the current ground track.
• Desired track up (DTK UP) aligns the top of the map display to the desired course.
FLIGHT
INSTRUMENTS
• Heading up (HDG UP) aligns the top of the map display to the current aircraft heading.
NOTE: When panning or reviewing active flight plan legs in a non-North Up orientation, the map does not
show the map orientation nor the wind direction and speed.
EIS
NOTE: Map orientation can only be changed on the Navigation Map Page. Any other displays that show
navigation data reflect the orientation selected for the Navigation Map Page:
AUDIO PANEL
& CNS
Changing the Navigation Map orientation:
1) With the Navigation Map Page displayed, press the MENU Key. The cursor flashes on the ‘Map Setup’ option.
FLIGHT
MANAGEMENT
Map Setup
Selection
HAZARD
AVOIDANCE
Figure 5-4 Navigation Map Page Menu Window
2) Press the ENT Key to display the Map Setup Window.
AFCS
3) Turn the large FMS Knob, or press the ENT Key once, to select the ‘ORIENTATION’ field.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
141
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Map Group Selection
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Orientation Field
Figure 5-5 Map Setup Menu Window - Map Group
FLIGHT
MANAGEMENT
4) Turn the small FMS Knob to select the desired orientation.
5) Press the ENT Key to select the new orientation.
6) Press the FMS Knob to return to the base page.
HAZARD
AVOIDANCE
MAP RANGE
AFCS
There are 28 different map ranges available, from 500 feet to 2000 nm. The current range is indicated in
the lower right corner of the map and represents the top-to-bottom distance covered by the map. When the
map range is decreased to a point that exceeds the capability of the G1000 to accurately represent the map,
a magnifying glass icon is shown to the left of the map range. To change the map range turn the Joystick
counter-clockwise to decrease the range, or clockwise to increase the range.
APPENDICES
ADDITIONAL
FEATURES
Range Overzoom
INDEX
Figure 5-6 Map Range
142
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
AUTO ZOOM
FLIGHT
INSTRUMENTS
Auto zoom allows the G1000 to change the map display range to the smallest range clearly showing the
active waypoint. Auto zoom can be overridden by adjusting the range with the Joystick, and remains until
the active waypoint changes, a terrain or traffic alert occurs, the aircraft takes off, or the manual override times
out (timer set on Map Setup Window).
EIS
If a terrain caution or warning occurs, any map page displaying TAWS/TERRAIN data automatically adjusts
to the smallest map range clearly showing the highest priority alert. If a new traffic advisory alert occurs, any
map page capable of displaying traffic advisory alerts automatically adjusts to the smallest map range clearly
showing the traffic advisory. When terrain or traffic alerts clear, the map returns to the previous auto zoom
range based on the active waypoint.
AUDIO PANEL
& CNS
The auto zoom function can be turned on or off independently for the PFD and MFD. Control of the ranges
at which the auto zoom occurs is done by setting the minimum and maximum ‘look forward’ times (set on
the Map Setup Window for the Map Group). These settings determine the minimum and maximum distance
to display based upon the aircraft’s ground speed.
FLIGHT
MANAGEMENT
• Waypoints that are long distances apart cause the map range to increase to a point where many details on
the map are decluttered. If this is not acceptable, lower the maximum look ahead time to a value that limits
the auto zoom to an acceptable range.
• Waypoints that are very short distances apart cause the map range to decrease to a point where situational
awareness may not be what is desired. Increase the minimum look ahead time to a value that limits the auto
zoom to a minimum range that provides acceptable situational awareness.
HAZARD
AVOIDANCE
• Flight plans that have a combination of long and short legs cause the range to increase and decrease as
waypoints sequence. To avoid this, auto zoom can be disabled or the maximum/minimum times can be
adjusted.
• The ‘time out’ time (configurable on the Map Setup Page for the Map Group) determines how long auto
zoom is overridden by a manual adjustment of the range knob. At the expiration of this time, the auto
zoom range is restored. Setting the ‘time out’ value to zero causes the manual override to never time out.
AFCS
• When the maximum ‘look forward’ time is set to zero, the upper limit becomes the maximum range available
(2000 nm).
• When the minimum ‘look forward’ time is set to zero, the lower limit becomes 1.5 nm.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
143
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Auto Zoom:
FLIGHT
INSTRUMENTS
Off, MFD Only, PFD Only, All On
AUDIO PANEL
& CNS
EIS
Manual Range Override
Expiration Time
Maximum Look Forward Time
Minimum Look Forward Time
Figure 5-7 Map Setup Menu Window - Map Group, Auto Zoom
Configuring automatic zoom:
FLIGHT
MANAGEMENT
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.
HAZARD
AVOIDANCE
4) Press the ENT Key.
5) Highlight the ‘AUTO ZOOM’ field.
6) Select ‘Off’, ‘MFD Only’, ‘PFD Only’, or ‘ALL On’.
7) Press the ENT Key to accept the selected option. The flashing cursor highlights the ‘MAX LOOK FWD’ field.
Times are from zero to 999 minutes.
AFCS
8) Use the FMS Knobs to set the time. Press the ENT Key.
9) Repeat step 8 for ‘MIN LOOK FWD’ (zero to 99 minutes) and ‘TIME OUT’ (zero to 99 minutes).
INDEX
APPENDICES
ADDITIONAL
FEATURES
10) Press the FMS Knob to return to the Navigation Map Page.
144
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
MAP PANNING
Map panning allows the pilot to:
• View parts of the map outside the displayed range without adjusting the map range
FLIGHT
INSTRUMENTS
• Highlight and select locations on the map
• Review information for a selected airport, NAVAID or user waypoint
• Designate locations for use in flight planning
• View airspace and airway information
EIS
When the panning function is selected by pressing the Joystick, the Map Pointer flashes on the map display.
A window also appears at the top of the map display showing the latitude/longitude position of the pointer,
the bearing and distance to the pointer from the aircraft’s present position, and the elevation of the land at the
position of the pointer.
AUDIO PANEL
& CNS
Map Pointer
Information
FLIGHT
MANAGEMENT
Map Pointer
HAZARD
AVOIDANCE
AFCS
Figure 5-8 Navigation Map - Map Pointer Activated
ADDITIONAL
FEATURES
NOTE: The map is normally centered on the aircraft’s position. If the map has been panned and there has
APPENDICES
been no pointer movement for about 60 seconds, the map reverts back to centered on the aircraft position
and the flashing pointer is removed.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
145
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
When the Map Pointer is placed on an object, the name of the object is highlighted (even if the name was
not originally displayed on the map). When any map feature or object is selected on the map display, pertinent
information is displayed.
EIS
Information about
Point of Interest
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Map Pointer
on POI
Figure 5-9 Navigation Map - Map Pointer on Point of Interest
HAZARD
AVOIDANCE
When the Map Pointer crosses an airspace boundary, the boundary is highlighted and airspace information
is shown at the top of the display. The information includes the name and class of airspace, the ceiling in feet
above Mean Sea Level (MSL), and the floor in feet MSL.
ADDITIONAL
FEATURES
AFCS
Information
about Airspace
INDEX
APPENDICES
Map Pointer
on Airspace
Figure 5-10 Navigation Map - Map Pointer on Airspace
146
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Panning the map:
1) Press the Joystick to display the Map Pointer.
2) Move the Joystick to move the Map Pointer around the map.
FLIGHT
INSTRUMENTS
3) Press the Joystick to remove the Map Pointer and recenter the map on the aircraft’s current position.
Reviewing information for an airport, NAVAID, or user waypoint:
1) Place the Map Pointer on a waypoint.
2) Press the ENT Key to display the Waypoint Information Page for the selected waypoint.
EIS
3) Select the GO BACK Softkey, the CLR Key, or the ENT Key to exit the Waypoint Information Page and return to
the Navigation Map showing the selected waypoint.
AUDIO PANEL
& CNS
NAVAID
Information
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
GO BACK Softkey
Figure 5-11 Navigation Map - Information Window - NAVAID
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
147
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Viewing airspace information for a special-use or controlled airspace:
1) Place the Map Pointer on an open area within the boundaries of an airspace.
FLIGHT
INSTRUMENTS
2) Press the ENT Key to display an options menu.
3) ‘Review Airspaces’ should already be highlighted, if not select it. Press the ENT Key to display the Airspace
Information Page for the selected airspace.
EIS
4) Press the CLR or ENT Key to exit the Airspace Information Page.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Airspace
Information
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 5-12 Navigation Map - Information Window - Airspace
148
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
MEASURING BEARING AND DISTANCE
FLIGHT
INSTRUMENTS
Distance and bearing from the aircraft’s present position to any point on the viewable navigation map may be
calculated using the ‘Measure Bearing and Distance’ selection from Navigation Map page menu. The bearing
and distance tool displays a dashed Measurement Line and a Measure Pointer to aid in graphically identifying
points with which to measure. Lat/Long, distance and elevation data for the Measure Pointer is provided in a
window at the top of the navigation map.
Measuring bearing and distance between any two points:
1) Press the MENU Key (with the Navigation Map Page displayed).
EIS
2) Highlight the ‘Measure Bearing/Distance’ field.
3) Press the ENT Key. A Measure Pointer is displayed on the map at the aircraft’s present position.
AUDIO PANEL
& CNS
4) Move the Joystick to place the reference pointer at the desired location. The bearing and distance are displayed
at the top of the map. Elevation at the current pointer position is also displayed. Pressing the ENT Key changes
the starting point for measuring.
Measurement
Information
FLIGHT
MANAGEMENT
5) To exit the Measure Bearing/Distance option, press the Joystick; or select ‘Stop Measuring’ from the Page
Menu and press the ENT Key.
Pointer Lat/Long
HAZARD
AVOIDANCE
Measurement Line
AFCS
ADDITIONAL
FEATURES
Figure 5-13 Navigation Map - Measuring Bearing and Distance
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
149
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
TOPOGRAPHY
FLIGHT
INSTRUMENTS
All navigation maps can display various shades of topography colors representing land elevation, similar
to aviation sectional charts. Topographic data can be displayed or removed as described in the following
procedures.
Navigation Map
Topographic Data
EIS
Navigation Map
Black Background
AUDIO PANEL
& CNS
TOPO Softkey
Not Enabled
TOPO Softkey
Enabled
FLIGHT
MANAGEMENT
TOPO Off
TOPO On
Figure 5-14 Navigation Map - Topographic Data
Displaying/removing topographic data on all pages displaying navigation maps:
HAZARD
AVOIDANCE
1) Select the MAP Softkey (the INSET Softkey for the PFD Inset Map).
2) Select the TOPO Softkey.
3) Select the TOPO Softkey again to remove topographic data from the Navigation Map. When topographic data
is removed from the page, all navigation data is presented on a black background.
AFCS
Displaying/removing topographic data (TOPO DATA) using the Navigation Map Page Menu:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
ADDITIONAL
FEATURES
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.
4) Press the ENT Key.
5) Highlight the ‘TOPO DATA’ field.
APPENDICES
6) Select ‘On’ or ‘Off’.
INDEX
7) Press the FMS Knob to return to the Navigation Map Page.
150
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
TOPO DATA
Range
EIS
TOPO DATA
On/Off
AUDIO PANEL
& CNS
Figure 5-15 Navigation Map Setup Menu - TOPO DATA Setup
The topographic data range is the maximum map range on which topographic data is displayed.
FLIGHT
MANAGEMENT
NOTE: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the
PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g., a setting
of 100 nm removes the item at ranges above 100 nm on MFD navigation maps, while the PFD Inset Map
removes the same item at 50 nm).
HAZARD
AVOIDANCE
Selecting a topographical data range (TOPO DATA):
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
AFCS
3) Select the ‘Map’ group.
4) Press the ENT Key.
5) Highlight the ‘TOPO DATA’ range field. TOPO ranges are from 500 ft to 2000 nm.
ADDITIONAL
FEATURES
6) To change the TOPO range setting, turn the small FMS Knob to display the range list.
7) Select the desired range using the small FMS Knob.
8) Press the ENT Key.
9) Press the FMS Knob to return to the Navigation Map Page.
APPENDICES
In addition, the Navigation Map can display a topographic scale (located in the lower right hand side of the
map) showing a scale of the terrain elevation and current elevation values.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
151
SYSTEM
OVERVIEW
Maximum Displayed Elevation
FLIGHT
INSTRUMENTS
FLIGHT MANAGEMENT
Aircraft Altitude (MSL)
Minimum Displayed Elevation
Range of
Displayed
Elevations
AUDIO PANEL
& CNS
EIS
Ground Elevation at Map Pointer
Location (only visible when Map
Pointer is displayed)
Figure 5-16 Navigation Map - TOPO SCALE
FLIGHT
MANAGEMENT
Displaying/removing the topographic scale (TOPO SCALE):
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group and press the ENT Key.
HAZARD
AVOIDANCE
4) Highlight the ‘TOPO SCALE’ field.
5) Select ‘On’ or ‘Off’.
ADDITIONAL
FEATURES
AFCS
6) Press the FMS Knob to return to the Navigation Map Page.
APPENDICES
TOPO SCALE
On/Off
INDEX
Figure 5-17 Navigation Map Setup Menu - TOPO SCALE Setup
152
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
MAP SYMBOLS
FLIGHT
INSTRUMENTS
This section discusses the types of land and aviation symbols that can be displayed. Each listed type of symbol
can be turned on or off, and the maximum range to display each symbol can be set. The decluttering of the
symbols from the map using the DCLTR Softkey is also discussed.
LAND SYMBOLS
The following items are configured on the land menu:
Land Symbols
Symbol
Default
Maximum
Range (nm) Range (nm)
EIS
(Text label size can be None, Small, Medium (Med), or Large
(Lrg))
Latitude/Longitude (LAT/LON)
Off
2000
Interstate Highway (FREEWAY)
300
800
International Highway (FREEWAY)
300
800
US Highway (NATIONAL HWY)
30
80
State Highway (LOCAL HWY)
15
30
8
15
Railroads (RAILROAD)
15
30
LARGE CITY (> 200,000)
800
1500
MEDIUM CITY (> 50,000)
100
200
SMALL CITY (> 5,000)
States and Provinces (STATE/PROV)
20
800
50
1500
Rivers and Lakes (RIVER/LAKE)
200
500
USER WAYPOINT
150
300
HAZARD
AVOIDANCE
N/A
FLIGHT
MANAGEMENT
Local Road (LOCAL ROAD)
AUDIO PANEL
& CNS
Highways and Roads
AFCS
ADDITIONAL
FEATURES
APPENDICES
Table 5-1 Land Symbol Information
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
153
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
AVIATION SYMBOLS
The following items are configured on the aviation menu:
Aviation Symbols
FLIGHT
INSTRUMENTS
(Text label size can be None, Small, Medium (Med),
or Large (Lrg))
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Default
Maximum
Range (nm) Range (nm)
Active Flight Plan Leg (ACTIVE FPL)
2000
2000
Non-active Flight Plan Leg (ACTIVE FPL)
2000
2000
2000
250
150
50
3
Off
15
2000
500
300
100
20
100
30
Non-directional Beacon (NDB WAYPOINT)
15
30
VOR (VOR WAYPOINT)
150
300
Class B Airspace/TMA (CLASS B/TMA)
200
500
Class C Airspace/TCA (CLASS C/TCA)
200
500
Class D Airspace (CLASS D)
150
300
Restricted Area (RESTRICTED)
200
500
Military Operations Area [MOA(MILITARY)]
200
500
Other/Air Defense Interdiction Zone (OTHER/ADIZ)
200
500
Temporary Flight Restriction (TFR)
500
2000
Active Flight Plan Waypoint (ACTIVE FPL WPT)
Large Airports (LARGE APT)
Medium Airports (MEDIUM APT)
Small Airports (SMALL APT)
Taxiways (SAFETAXI)
Runway Extension (RWY EXTENSION)
Intersection (INT WAYPOINT)
APPENDICES
Symbol
See Airports, NAVAIDs
See Additional Features
N/A
INDEX
Table 5-2 Aviation Symbol Information
154
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
SYMBOL SETUP
All pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed
totally (turned off).
FLIGHT
INSTRUMENTS
Displaying/removing all land symbols:
1) Press the MENU Key with the Navigation Map Page displayed. The Page Menu is displayed and the cursor
flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Group Menu is displayed and the cursor flashes on the ‘Map’ option.
EIS
3) Highlight the ‘LAND DATA’ field.
4) Select ‘On’ or ‘Off’.
5) Press the FMS Knob to return to the Navigation Map Page.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
LAND DATA
On/Off
HAZARD
AVOIDANCE
AFCS
Figure 5-18 Navigation Map Setup Menu - LAND DATA Setup
The label size (TEXT) sets the size at which labels appear on the display (none, small, medium, and large).
The range (RNG) sets the maximum range at which items appear on the display.
ADDITIONAL
FEATURES
Selecting a ‘Land’ or ‘Aviation’ group item text size and range:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
APPENDICES
3) Select the ‘Land’ or ‘Aviation’ group.
4) Press the ENT Key. The cursor flashes on the first field.
5) Select the desired land option.
6) Select the desired text size.
INDEX
7) Press the ENT Key to accept the selected size.
8) Select the desired range.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
155
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
9) Press the ENT Key to accept the selected range.
FLIGHT
INSTRUMENTS
10) Press the FMS Knob to return to the Navigation Map Page.
AUDIO PANEL
& CNS
EIS
Text Label Size
(None, Small, Med, or Lrg)
Maximum Display Range
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Figure 5-19 Navigation Map Setup Menu - LAND GROUP Setup
Maximum Display Range
ADDITIONAL
FEATURES
AFCS
Text Label Size
(None, Small, Med, or Lrg)
APPENDICES
Figure 5-20 Navigation Map Setup Menu - AVIATION GROUP Setup
NOTE: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the
INDEX
PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g., a setting
of 100 nm removes the item at ranges above 100 nm on MFD navigation maps, while the PFD Inset Map
removes the same item at 50 nm).
156
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
MAP DECLUTTER
The declutter feature allows the pilot to progressively step through four levels of removing map information.
The declutter level is displayed in the DCLTR Softkey and next to the Declutter Menu Option.
FLIGHT
INSTRUMENTS
Declutter Level
EIS
DCLTR Softkey
Navigation Map Page Menu
Figure 5-21 Navigation Map - Declutter Level Indications
AUDIO PANEL
& CNS
Decluttering the map:
Select the DCLTR Softkey with the Navigation Map Page displayed. The current declutter level is shown. With
each softkey selection, another level of map information is removed.
FLIGHT
MANAGEMENT
Or:
1) Press the MENU Key with the Navigation Map Page displayed.
2) Select ‘Declutter’. The current declutter level is shown.
3) Press the ENT Key.
HAZARD
AVOIDANCE
Decluttering the PFD Inset Map:
1) Select the INSET Softkey.
2) Select the DCLTR Softkey. The current declutter level is shown. With each selection, another level of map
information is removed.
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
157
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Table 5-3 lists the items displayed at each declutter level. The ‘X’ represents map items displayed for the
various levels of declutter.
Item
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Flight Plan Route Lines
Flight Plan Route Waypoints
Rivers/Lakes
Topography Data
International Borders
Track Vector
Navigation Range Ring
Fuel Range Ring
Terrain Data
Traffic
Airways
NEXRAD
XM Lightning Data
Airports
Runway Labels
Restricted
MOA (Military)
User Waypoints
Latitude/Longitude Grid
NAVAIDs
Class B Airspaces/TMA
Class C Airspaces/TCA
Class D Airspaces
Other Airspaces/ADIZ
TFRs
Obstacles
Land/Country Text
Cities
Roads
Railroads
State/Province Boundaries
River/Lake Names
No Declutter Declutter-1 Declutter-2 Declutter-3
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
INDEX
Table 5-3 Navigation Map Items Displayed by Declutter Level
158
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
AIRWAYS
FLIGHT
INSTRUMENTS
This airways discussion is based upon the North American airway structure. The airway structure in places
other than North America vary by location, etc. and are not discussed in this book. Low Altitude Airways (or
Victor Airways) primarily serve smaller piston-engine, propeller-driven airplanes on shorter routes and at lower
altitudes. Airways are eight nautical miles wide and start 1,200 feet above ground level (AGL) and extend up
to 18,000 feet mean sea level (MSL). Low Altitude Airways are designated with a “V” before the airway number
(hence the name “Victor Airways”) since they run primarily between VORs.
EIS
High Altitude Airways (or Jet Routes) primarily serve airliners, jets, turboprops, and turbocharged piston
aircraft operating above 18,000 feet MSL. Jet Routes start at 18,000 feet MSL and extend upward to 45,000 feet
MSL (altitudes above 18,000 feet are called “flight levels” and are described as FL450 for 45,000 feet MSL). Jet
Routes are designated with a “J” before the route number.
AUDIO PANEL
& CNS
Low Altitude Airways are drawn in gray (the same shade used for roads). High Altitude Airways are drawn
in green. When both types of airways are displayed, High Altitude Airways are drawn on top of Low Altitude
Airways.
When airways are selected for display on the map, the airway waypoints (VORs, NDBs and Intersections) are
also displayed.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Low Altitude
Airway
(Victor Airway)
AFCS
High Altitude
Airway
(Jet Route)
ADDITIONAL
FEATURES
APPENDICES
Figure 5-22 Airways on MFD Navigation Page
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
159
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Airways may be displayed on the map at the pilot’s discretion using either a combination of AIRWAYS Softkey
presses, or menu selections using the MENU Key from the Navigation Map Page. The Airway range can also be
programmed to only display Airways on the MFD when the map range is at or below a specific number.
FLIGHT
INSTRUMENTS
Displaying/removing airways:
1) Select the MAP Softkey.
2) Select the AIRWAYS Softkey. Both High and Low Altitude Airways are displayed (AIRWY ON).
3) Select the softkey again to display Low Altitude Airways only (AIRWY LO).
EIS
4) Select the softkey again to display High Altitude Airways only (AIRWY HI).
5) Select the softkey again to remove High Altitude Airways. No airways are displayed (AIRWAYS).
Or:
AUDIO PANEL
& CNS
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT Key.
FLIGHT
MANAGEMENT
4) Turn the large FMS Knob to highlight the ‘AIRWAYS’ field.
5) Turn the FMS Knob to select ‘Off’, ‘All’, ‘LO Only’, or ‘HI Only’, and press the ENT Key.
HAZARD
AVOIDANCE
6) Press the FMS Knob to return to the Navigation Map Page.
Airway Display Selection
Off, All, LO Only, HI Only
Low Altitude Airway Range
High Altitude Airway Range
AFCS
Figure 5-23 Navigation Map Setup Menu - AIRWAYS Setup
The airway range is the maximum map range on which airways are displayed.
ADDITIONAL
FEATURES
Selecting an airway range (LOW ALT AIRWAY or HI ALT AIRWAY):
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT Key.
APPENDICES
4) Highlight the ‘LOW ALT AIRWAY’ or ‘HI ALT AIRWAY’ range field.
5) To change the range setting, turn the small FMS Knob to display the range list.
6) Select the desired range using the small FMS Knob.
7) Press the ENT Key.
INDEX
8) Press the FMS Knob to return to the Navigation Map Page.
160
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
The following range items are configurable on the airways menu:
Airway Type
Symbol
High Altitude Airway (HI ALT AIRWAY)
300
FLIGHT
INSTRUMENTS
Low Altitude Airway (LOW ALT AIRWAY)
Default
Maximum
Range (nm) Range (nm)
200
500
500
Table 5-4 Airway Range Information
EIS
TRACK VECTOR
AUDIO PANEL
& CNS
The Navigation Map can display a track vector that is useful in minimizing track angle error. The track vector
is a solid light blue line segment extended to a predicted location. The track vector look-ahead time is selectable
(30 sec, 60 sec (default), 2 min, 5 min, 10 min, 20 min) and determines the length of the track vector. The track
vector shows up to 90 degrees of a turn for the 30 and 60 second time settings.
FLIGHT
MANAGEMENT
Track Vector
HAZARD
AVOIDANCE
Figure 5-24 Navigation Map -Track Vector
Displaying/removing the track vector:
AFCS
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.
ADDITIONAL
FEATURES
4) Press the ENT Key.
5) Highlight the ‘TRACK VECTOR’ field.
APPENDICES
6) Select ‘On’ or ‘Off’. Press the ENT Key to accept the selected option. The flashing cursor highlights the look
ahead time field. Use the FMS Knob to select the desired time. Press the ENT Key.
7) Press the FMS Knob to return to the Navigation Map Page.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
161
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Wind Vector On/Off
EIS
Nav Range Ring On/Off
Track Vector
- On/Off
- Look Ahead Time
AUDIO PANEL
& CNS
Fuel Range
- On/Off
- Fuel Reserve Time
Figure 5-25 Navigation Map Setup Menu -TRACK VECTOR, WIND VECTOR, NAV RANGE RING, FUEL RANGE RING Setup
FLIGHT
MANAGEMENT
WIND VECTOR
HAZARD
AVOIDANCE
The map displays a wind vector arrow in the upper right-hand portion of the screen. Wind vector information
is displayed as a white arrow pointing in the direction in which the wind is moving for wind speeds greater than
or equal to 1 kt.
Wind Direction
Wind Speed
Figure 5-26 Navigation Map - Wind Vector
AFCS
NOTE: The wind vector is not displayed until the aircraft is moving. It is not displayed on the Waypoint
Information pages.
ADDITIONAL
FEATURES
Displaying/removing the wind vector:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
APPENDICES
3) Select the ‘Map’ group.
4) Press the ENT Key.
5) Highlight the ‘WIND VECTOR’ field.
6) Select ‘On’ or ‘Off’.
INDEX
7) Press the FMS Knob to return to the Navigation Map Page.
162
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
NAV RANGE RING
The Nav Range Ring shows the direction of travel (ground track) on a rotating compass card. The range is
determined by the map range. The range is 1/4 of the map range (e.g., 37.5 nm on a 150 nm map).
FLIGHT
INSTRUMENTS
Range (radius)
EIS
AUDIO PANEL
& CNS
Nav Range Ring
FLIGHT
MANAGEMENT
Figure 5-27 Navigation Map - Nav Range Ring
NOTE: The Nav Range Ring is not displayed on the Waypoint Information pages, Nearest pages, or Direct-to
HAZARD
AVOIDANCE
Window map.
Displaying/removing the Nav Range Ring:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
AFCS
3) Select the ‘Map’ group.
4) Press the ENT Key.
ADDITIONAL
FEATURES
5) Highlight the ‘NAV RANGE RING’ field.
6) Select ‘On’ or ‘Off’.
7) Press the FMS Knob to return to the Navigation Map Page.
APPENDICES
NOTE: The Nav Range Ring is referenced to either magnetic or true north, based on the selection on the AUX
- System Setup Page.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
163
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FUEL RANGE RING
FLIGHT
INSTRUMENTS
The map can display a fuel range ring which shows the remaining flight distance. A dashed green circle
indicates the selected range to reserve fuel. A solid green circle indicates the total endurance range. If only
reserve fuel remains, the range is indicated by a solid yellow circle.
Total Endurance Range
AUDIO PANEL
& CNS
EIS
Time to Reserve Fuel
FLIGHT
MANAGEMENT
Range to Reserve Fuel
Figure 5-28 Navigation Map - Fuel Range Ring
HAZARD
AVOIDANCE
Displaying/removing the fuel range ring and selecting a fuel range time:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.
AFCS
4) Press the ENT Key.
5) Highlight the ‘FUEL RNG (RSV)’ field.
6) Select ‘On’ or ‘Off’.
ADDITIONAL
FEATURES
7) Highlight the fuel reserve time field. This time should be set to the amount of flight time equal to the amount
of fuel reserve desired.
8) To change the reserve fuel time, enter a time (00:00 to 23:59; hours:minutes). The default setting is 00:45
minutes.
APPENDICES
9) Press the ENT Key.
INDEX
10) Press the FMS Knob to return to the Navigation Map Page.
164
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FIELD OF VIEW (SVS)
FLIGHT
INSTRUMENTS
The map can display the boundaries of the PFD Synthetic Vision System (SVS) lateral field of view. The field
of view is shown as two dashed lines forming a V shape in front of the aircraft symbol on the map. This is only
available if SVS is installed on the aircraft.
EIS
Lateral Field
of View
Boundaries
AUDIO PANEL
& CNS
Figure 5-29 Navigation Map - Field of View
FLIGHT
MANAGEMENT
Displaying/removing the field of view:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
HAZARD
AVOIDANCE
3) Select the ‘Map’ group.
4) Press the ENT Key.
5) Highlight the ‘FIELD OF VIEW’ field.
6) Select ‘On’ or ‘Off’.
AFCS
7) Press the FMS Knob to return to the Navigation Map Page.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
165
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
SELECTED ALTITUDE INTERCEPT ARC
FLIGHT
INSTRUMENTS
The map can display the location along the current track where the aircraft will intercept the selected altitude.
The location will be shown as a light blue arc when the aircraft is actually climbing or descending.
AUDIO PANEL
& CNS
EIS
Range to
Altitude Arc
Figure 5-30 Navigation Map - Range to Altitude Arc
FLIGHT
MANAGEMENT
Displaying/removing the selected altitude intercept arc:
1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option.
2) Press the ENT Key. The Map Setup Menu is displayed.
3) Select the ‘Map’ group.
HAZARD
AVOIDANCE
4) Press the ENT Key.
5) Highlight the ‘SEL ALT ARC’ field.
6) Select ‘On’ or ‘Off’.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
7) Press the FMS Knob to return to the Navigation Map Page.
166
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
5.3 WAYPOINTS
FLIGHT
INSTRUMENTS
Waypoints are predetermined geographical positions (internal database) or pilot-entered positions, and are
used for all phases of flight planning and navigation.
Communication and navigation frequencies can be tuned “automatically” from various Waypoint Information
(WPT) pages, Nearest (NRST) pages, and the Nearest Airports Window (on PFD). This auto-tuning feature
simplifies frequency entry over manual tuning. Refer to the Audio Panel and CNS section for details on autotuning.
Facility
Entry Field
- Waypoint Identifier
- Type (symbol)
- Facility Name
- City
FLIGHT
MANAGEMENT
City Entry Field
AUDIO PANEL
& CNS
Identifier Entry Field
EIS
Waypoints can be selected by entering the ICAO identifier, entering the name of the facility, or by entering
the city name. See the System Overview section for detailed instructions on entering data in the G1000. As a
waypoint identifier, facility name, or location is entered, the G1000’s Spell’N’Find™ feature scrolls through the
database, displaying those waypoints matching the characters which have been entered to that point. A direct-to
navigation leg to the selected waypoint can be initiated by pressing the Direct-to Key on any of the waypoint
pages.
HAZARD
AVOIDANCE
Entered Waypoint on
Map
Map Area Showing
Entered Waypoint
AFCS
Waypoint Location
ADDITIONAL
FEATURES
Figure 5-31 Waypoint Information Window
APPENDICES
If duplicate entries exist for the entered facility name or location, additional entries may be viewed by continuing
to turn the small FMS Knob during the selection process. If duplicate entries exist for an identifier, a Duplicate
Waypoints Window is displayed when the ENT Key is pressed.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
167
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
Identifier with
Duplicates
AUDIO PANEL
& CNS
EIS
Duplicate
Waypoints
FLIGHT
MANAGEMENT
Duplicate Message
Figure 5-32 Waypoint Information Window - Duplicate Identifier
AIRPORTS
HAZARD
AVOIDANCE
NOTE: ‘North Up’ orientation on the Airport Information Page cannot be changed; the pilot needs to be
aware of proper orientation if the Navigation Map orientation is different from the Airport Information Page
Map.
ADDITIONAL
FEATURES
AFCS
The Airport Information Page is the first page in WPT group and allows the pilot to view airport information,
load frequencies (COM, NAV, and lighting), review runways, and review instrument procedures that may be
involved in the flight plan. See the Audio Panel and CNS Section for more information on loading frequencies
(auto-tuning). After engine startup, the Airport Information Page defaults to the airport where the aircraft is
located. After a flight plan has been loaded, it defaults to the destination airport. On a flight plan with multiple
airports, it defaults to the airport which is the current active waypoint.
INDEX
APPENDICES
In addition to displaying a map of the currently selected airport and surrounding area, the Airport Information
Page displays airport information in three boxes labeled ‘AIRPORT’, ‘RUNWAYS’, and ‘FREQUENCIES’. For
airports with multiple runways, information for each runway is available. This information is viewed on the
Airport Information Page by pressing the INFO softkey until INFO-1 is displayed.
168
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Airport Information
FLIGHT
INSTRUMENTS
- ID/Facility/City
- Usage Type/Region
- Lat/Long/Elev
- Fuel Available
- Time Zone (UTC Offset)
Navigation Map
Showing Selected
Airport
Runway Information
- Designation
- Length/Width/Surface
- Lighting Available
EIS
Airport/Runway
Diagram
COM/NAV Freq. Info.
AUDIO PANEL
& CNS
- Identification
- Frequency
- Availability
- Additional Information
Softkeys
FLIGHT
MANAGEMENT
Figure 5-33 Airport Information Page
The following descriptions and abbreviations are used on the Airport Information Page:
• Usage type: Public, Military, Private, or Heliport
• Runway surface type: Hard, Turf, Sealed, Gravel, Dirt, Soft, Unknown, or Water
HAZARD
AVOIDANCE
• Runway lighting type: No Lights, Part Time, Full Time, Unknown, or PCL Freq (for pilot-controlled
lighting)
• COM Availability: TX (transmit only), RX (receive only), PT (part time), i (additional information available)
AFCS
Airport Directory
Information
Airport Information
- ID/Facility/City
- Usage Type/Region
ADDITIONAL
FEATURES
APPENDICES
INDEX
Softkeys
Figure 5-34 Airport Directory Page Example
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
169
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
The AOPA directory information is viewed on the Airport Directory Page by pressing the INFO softkey until
INFO-2 is displayed. The following are types of AOPA airport directory information shown (if available) on
the Airport Directory Page:
FLIGHT
INSTRUMENTS
• Airport:
Identifier, Site
Number, Name, City, State
• Phones: Phone/Fax Numbers
AUDIO PANEL
& CNS
EIS
• Hours: Facility Hours, Light
Hours, Tower Hours, Beacon
Hours
• Location: Sectional, Magnetic
Variation
• Frequencies: Type/Frequency
FLIGHT
MANAGEMENT
• Transportation:
Ground
Transportation Type Available
HAZARD
AVOIDANCE
• Approach: Approach Facility
Name, Frequency, Frequency
Parameter
• Traffic Pattern Altitudes
(TPA): Aircraft Class/Altitude
• Weather:
Service Type,
Frequency, Phone Number
• Flight Service Station (FSS):
FSS Name, Phone Numbers
• Runway: Headings, Length,
Width, Obstructions, Surface
• Obstructions: General Airport
Obstructions
• Special
Operations
at
Airport
• Instrument
Approaches:
Published
Approach,
Frequency
• NAVAIDS: Type, Identifier,
Frequency, Radial, Distance
• Noise:
Noise Abatement
Procedures
• Services Available: Category,
Specific Service
• Charts: Low Altitude Chart
Number
• FBO: Type, Frequencies,
Services, Fees, Fuel, Credit
Cards, Phone/Fax Numbers
• Notes: Airport Notes
• Pilot Controlled Lighting:
High/Med/Low Clicks/Second
Selecting an airport for review by identifier, facility name, or location:
1) From the Airport Information Page, press the FMS Knob.
2) Use the FMS Knobs and enter an identifier, facility name, or location.
AFCS
3) Press the ENT Key.
4) Press the FMS Knob to remove the cursor.
ADDITIONAL
FEATURES
Selecting a runway:
1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor.
2) Turn the large FMS Knob to place the cursor in the ‘RUNWAYS’ Box, on the runway designator.
3) Turn the small FMS Knob to display the desired runway (if more than one) for the selected airport.
APPENDICES
4) To remove the flashing cursor, press the FMS Knob.
Viewing a destination airport:
INDEX
From the Airport Information Page press the MENU Key. Select ‘View Destination Airport’. The Destination
Airport is displayed.
170
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
The Airport Frequencies Box uses the descriptions and abbreviations listed in the following table:
Navigation Frequencies
ILS
LOC
FLIGHT
INSTRUMENTS
EIS
Communication Frequencies
Approach * Control
Pre-Taxi
Arrival *
CTA *
Radar
ASOS
Departure * Ramp
ATIS
Gate
Terminal *
AWOS
Ground
TMA *
Center
Helicopter
Tower
Class B *
Multicom
TRSA *
Class C *
Other
Unicom
Clearance
AUDIO PANEL
& CNS
* May include Additional Information
Table 5-5 Airport Frequency Abbreviations
FLIGHT
MANAGEMENT
A departure, arrival, or approach can be loaded using the softkeys on the Airport Information Page. See the
Procedures section for details. METARs or TAFs applicable to the selected airport can be selected for display (see
the Hazard Avoidance section for details about weather).
HAZARD
AVOIDANCE
The G1000 provides a NRST Softkey on the PFD, which gives the pilot quick access to nearest airport
information (very useful if an immediate landing is required). The Nearest Airports Window displays a list
of up to 25 nearest airports (three entries can be displayed at one time). If there are more than three they are
displayed in a scrollable list. If there are no nearest airports available, “NONE WITHIN 200NM” is displayed.
Bearing/Distance to Airport
Airport Identifier/
Type
Approach Available
AFCS
Length of Longest
Runway
COM Freq. Info.
- Identification
- Frequency
ADDITIONAL
FEATURES
Additional Airports
(within 200 nm)
APPENDICES
NRST Softkey
Figure 5-35 Nearest Airports Window on PFD
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
171
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
Pressing the ENT Key displays the PFD Airport Information Window for the highlighted airport. Pressing the
ENT Key again returns to the Nearest Airports Window with the cursor on the next airport in the list. Continued
presses of the ENT Key sequences through the information pages for all airports in the Nearest Airports list.
Airport Information
- ID/Type/City
- Facility
EIS
Airport Information
- Usage/Time/Elev
- Region
Airport Information
AUDIO PANEL
& CNS
- Lat/Long
FLIGHT
MANAGEMENT
Figure 5-36 Airport Information Window on PFD
HAZARD
AVOIDANCE
The Nearest Airports Page on the MFD is first in the group of NRST pages because of its potential use in
the event of an in-flight emergency. In addition to displaying a map of the currently selected airport and
surrounding area, the page displays nearest airport information in five boxes labeled ‘NEAREST AIRPORTS’,
‘INFORMATION’, ‘RUNWAYS’, ‘FREQUENCIES’, and ‘APPROACHES’. INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
The selected airport is indicated by a white arrow, and a dashed white line is drawn on the navigation map
from the aircraft position to the nearest airport. Up to five nearest airports, one runway, up to three frequencies,
and up to three approaches are visible at one time. If there are more than can be shown, each list can be scrolled.
If there are no items for display in a boxed area, text indicating that fact is displayed. The currently selected
airport remains in the list until it is unselected.
172
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Nearest Airports
FLIGHT
INSTRUMENTS
- ID/Type
- Bearing/Distance
Airport Information
- Facility/City/Elevation
Nearest Airport
Runway Information
- Designation/Surface
- Length/Width
Navigation Map
Showing Nearest
Airport
EIS
COM/NAV Freq. Info.
- Identification
- Frequency
Approaches Available
AUDIO PANEL
& CNS
LD APR Softkey (only
available if an approach is
highlighted)
Window Selection
Softkeys
Figure 5-37 Nearest Airport Page
FLIGHT
MANAGEMENT
Viewing information for a nearest airport on the PFD:
1) Select the NRST Softkey to display the Nearest Airports Window. Press the FMS Knob to activate the cursor.
HAZARD
AVOIDANCE
2) Highlight the airport identifier with the FMS Knob and press the ENT Key to display the Airport Information
Window.
3) To return to the Nearest Airports Window press the ENT Key (with the cursor on ‘BACK’) or press the CLR
Key. The cursor is now on the next airport in the nearest airports list. (Repeatedly pressing the ENT Key
moves through the airport list, alternating between the Nearest Airports Window and the Airport Information
Window.)
AFCS
4) Press the CLR Key or the NRST Softkey to close the PFD Nearest Airports Window.
Viewing information for a nearest airport on the MFD:
ADDITIONAL
FEATURES
1) Turn the large FMS Knob to select the NRST page group.
2) Turn the small FMS Knob to select the Nearest Airports Page (it is the first page of the group, so it may already
be selected). If there are no Nearest Airports available, “NONE WITHIN 200 NM” is displayed.
APPENDICES
3) Select the APT Softkey; or press the FMS Knob; or press the MENU Key, highlight ‘Select Airport Window’ and
press the ENT Key. The cursor is placed in the ‘NEAREST AIRPORTS’ Box. The first airport in the nearest airports
list is highlighted.
4) Turn the FMS Knob to highlight the desired airport. (Pressing the ENT Key also moves to the next airport.)
5) Press the FMS Knob to remove the flashing cursor.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
173
SYSTEM
OVERVIEW
Viewing runway information for a specific airport:
FLIGHT
INSTRUMENTS
FLIGHT MANAGEMENT
2) Turn the small FMS Knob to select the desired runway.
1) With the Nearest Airports Page displayed, select the RNWY Softkey; or press the MENU Key, highlight ‘Select
Runway Window’; and press the ENT Key. The cursor is placed in the ‘RUNWAYS’ Box.
3) Press the FMS Knob to remove the flashing cursor.
See the Audio Panel and CNS Section for frequency selection and the Procedures section for approaches.
EIS
The Nearest Airports Box on the System Setup Page defines the minimum runway length and surface type
used when determining the 25 nearest airports to display on the MFD Nearest Airports Page. A minimum
runway length and/or surface type can be entered to prevent airports with small runways or runways that are
not appropriately surfaced from being displayed. Default settings are 0 feet (or meters) for runway length and
“HARD/SOFT” for runway surface type.
AUDIO PANEL
& CNS
Selecting nearest airport surface matching criteria:
1) Use the FMS Knob to select the System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
FLIGHT
MANAGEMENT
3) Turn the large FMS Knob to highlight the runway surface field in the Nearest Airports Box.
4) Turn the small FMS Knob to select the desired runway option (ANY, HARD ONLY, HARD/SOFT, WATER).
5) Press the ENT Key.
HAZARD
AVOIDANCE
6) Press the FMS Knob to remove the flashing cursor.
Selecting nearest airport minimum runway length matching criteria:
1) Use the FMS Knob to select the System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
AFCS
3) Turn the large FMS Knob to highlight the minimum length field in the Nearest Airport Box.
4) Use the FMS Knob to enter the minimum runway length (zero to 25,000 feet) and press the ENT Key.
APPENDICES
ADDITIONAL
FEATURES
5) Press the FMS Knob to remove the flashing cursor.
Nearest Airport Criteria
INDEX
- Type of Runway Surface
- Minimum Runway Length
Figure 5-38 System Setup Page - Nearest Airport Selection Criteria
174
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
INTERSECTIONS
NOTE: The VOR displayed on the Intersection Information Page is the nearest VOR, not necessarily the VOR
FLIGHT
INSTRUMENTS
used to define the intersection.
The Intersection Information Page is used to view information about intersections. In addition to displaying
a map of the currently selected intersection and surrounding area, the Intersection Information Page displays
intersection information in three boxes labeled ‘INTERSECTION’, ‘INFORMATION’, and ‘NEAREST VOR’.
EIS
Intersection Identifier
Intersection Info
Navigation Map
Showing Selected
Intersection
AUDIO PANEL
& CNS
- Region
- Lat/Long
Nearest VOR Info
- Identifier/Type (symbol)
- Radial to VOR
- Distance to VOR
Selected
Intersection
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 5-39 Intersection Information Page
Selecting an intersection:
AFCS
1) With the Intersection Information Page displayed, enter an identifier in the Intersection Box.
2) Press the ENT Key.
ADDITIONAL
FEATURES
3) Press the FMS Knob to remove the flashing cursor.
Or:
1) With the Nearest Intersections Page displayed, press the FMS Knob.
2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest Intersection Box.
APPENDICES
3) Press the FMS Knob to remove the flashing cursor.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
175
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
The Nearest Intersections Page can be used to quickly find an intersection close to the flight path. In addition
to displaying a map of the surrounding area, the page displays information for up to 25 nearest intersections in
three boxes labeled ‘NEAREST INT’, ‘INFORMATION’, and ‘REFERENCE VOR’.
FLIGHT
INSTRUMENTS
The selected intersection is indicated by a white arrow. Up to eleven Intersections are visible at a time. If
there are more than can be shown, the list can be scrolled. If there are no items for display, text indicating that
fact is displayed.
EIS
NOTE: The list only includes waypoints that are within 200 nm.
AUDIO PANEL
& CNS
Intersection Information
- Identifier/Symbol
- Bearing/Distance to
intersection from
aircraft position
FLIGHT
MANAGEMENT
Navigation Map
Showing Nearest
Intersection
Intersection Lat/Long
Reference VOR Info
HAZARD
AVOIDANCE
Nearest Intersection
- Identifier/Type (symbol)
- VOR Frequency
- Bearing/Distance to VOR
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 5-40 Nearest Intersections Page
176
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
NDBS
FLIGHT
INSTRUMENTS
The NDB Information Page is used to view information about NDBs. In addition to displaying a map of
the currently selected NDB and surrounding area, the page displays NDB information in four boxes labeled
‘NDB’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST AIRPORT’.
NDB Identifier/Type
- Facility Name
- Nearest City
Navigation Map
Showing Selected
NDB
NDB Information
EIS
- Type
- Region
- Lat/Long
NDB Frequency
AUDIO PANEL
& CNS
Selected NDB
Nearest Airport Info
- Identifier/Type (symbol)
- Bearing/Distance to
Airport
FLIGHT
MANAGEMENT
Figure 5-41 NDB Information Page
HAZARD
AVOIDANCE
NOTE: Compass locator (LOM, LMM): a low power, low or medium frequency radio beacon installed in
conjunction with the instrument landing system. When LOM is used, the locator is at the Outer Marker;
when LMM is used, the locator is at the Middle Marker.
AFCS
Selecting an NDB:
1) With the NDB Information Page displayed, enter an identifier, the name of the NDB, or the city in which it’s
located in the NDB Box.
ADDITIONAL
FEATURES
2) Press the ENT Key.
3) Press the FMS Knob to remove the flashing cursor.
Or:
APPENDICES
1) With the Nearest NDB Page displayed, press the FMS Knob
2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest NDB Box.
3) Press the FMS Knob to remove the flashing cursor.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
177
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
The Nearest NDB Page can be used to quickly find a NDB close to the flight path. In addition to displaying
a map of the surrounding area, the page displays information for up to 25 nearest NDBs in three boxes labeled
‘NEAREST NDB’, ‘INFORMATION’, and ‘FREQUENCY’.
EIS
FLIGHT
INSTRUMENTS
A white arrow before the NDB identifier indicates the selected NDB. Up to eleven NDBs are visible at a time.
If there are more than can be shown, each list can be scrolled. The list only includes waypoints that are within
200nm. If there are no NDBs in the list, text indicating that there are no nearest NDBs is displayed. If there are
no nearest NDBs in the list, the information and frequency fields are dashed.
NDB Identifier/Symbol
Navigation Map
Showing Selected
NDB
AUDIO PANEL
& CNS
- Bearing/Distance to
NDB from aircraft
position
FLIGHT
MANAGEMENT
NDB Information
- Facility Name/City
- Type
- Lat/Long
Nearest NDB
HAZARD
AVOIDANCE
NDB Frequency
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 5-42 Nearest NDB Page
178
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
VORS
FLIGHT
INSTRUMENTS
The VOR Information Page can be used to view information about VOR and ILS signals (since ILS signals
can be received on a NAV receiver), or to quickly auto-tune a VOR or ILS frequency. Localizer information
cannot be viewed on the VOR Information Page. If a VOR station is combined with a TACAN station it is
listed as a VORTAC on the VOR Information Page and if it includes only DME, it is displayed as VOR-DME.
In addition to displaying a map of the currently selected VOR and surrounding area, the VOR Information
Page displays VOR information in four boxes labeled ‘VOR’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST
AIRPORT’.
EIS
VOR Identifier/Type
- Facility Name
- Nearest City
AUDIO PANEL
& CNS
Navigation Map
Showing Selected
VOR
VOR Information
- Class/Magnetic Variation
- Region
- Lat/Long
VOR Frequency
FLIGHT
MANAGEMENT
Selected VOR
Nearest Airport Info
- Identifier/Type (symbol)
- Bearing/Distance to
Airport
HAZARD
AVOIDANCE
Figure 5-43 VOR Information Page
AFCS
The VOR classes used in the VOR information box are: LOW ALTITUDE, HIGH ALTITUDE, and
TERMINAL.
Selecting a VOR:
ADDITIONAL
FEATURES
1) With the VOR Information Page displayed, enter an identifier, the name of the VOR, or the city in which it’s
located in the VOR Box.
2) Press the ENT Key.
3) Press the FMS Knob to remove the flashing cursor.
APPENDICES
Or:
1) With the Nearest VOR Page displayed, press the FMS Knob or select the VOR Softkey.
2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest VOR Box.
3) Press the FMS Knob to remove the flashing cursor.
190-00552-05 Rev. A
INDEX
Or:
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
179
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
1) With the Nearest VOR Page displayed, press the MENU Key.
2) Highlight ‘Select VOR Window’, and press the ENT Key.
FLIGHT
INSTRUMENTS
3) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest VOR Box.
4) Press the FMS Knob to remove the flashing cursor.
EIS
The Nearest VOR Page can be used to quickly find a VOR station close to the aircraft. Also, a NAV frequency
from a selected VOR station can be loaded from the Nearest VOR Page. In addition to displaying a map of
the surrounding area, the Nearest VOR Page displays information for up to 25 nearest VOR stations in three
boxes labeled ‘NEAREST VOR’, ‘INFORMATION’, and ‘FREQUENCY’. The list only includes waypoints that
are within 200 nm.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
A white arrow before the VOR identifier indicates the selected VOR. Up to eleven VORs are visible at a
time. If there are more than can be shown, each list can be scrolled. If there are no VORs in the list, text
indicating that there are no nearest VORs is displayed. If there are no nearest VORs in the list, the information
is dashed.
VOR Identifier/Symbol
HAZARD
AVOIDANCE
Navigation Map
Showing Nearest
VOR
- Bearing/Distance to VOR
from aircraft position
VOR Information
- Facility Name/City
- Class/Magnetic Variation
- Lat/Long
Nearest VOR
AFCS
VOR Frequency
INDEX
APPENDICES
ADDITIONAL
FEATURES
Figure 5-44 Nearest VOR Page
180
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
USER WAYPOINTS
FLIGHT
INSTRUMENTS
The G1000 can create and store up to 1,000 user-defined waypoints. User waypoints can be created from any
map page (except PFD Inset Map, AUX-Trip Planning Page, or Procedure Pages) by selecting a position on the
map using the Joystick, or from the User Waypoint Information Page by referencing a bearing/distance from
an existing waypoint, bearings from two existing waypoints, or latitude and longitude. Once a waypoint has
been created, it can be renamed, deleted, or moved. Temporary user waypoints are erased upon system power
down.
User Waypoint Info
User Wpt Comment
Navigation Map
Showing Selected
User Waypoint
Reference Wpt/Info
Selected User
Waypoint
User Waypoint List
EIS
- Identifier
- Temporary/Normal
- Waypoint Type
AUDIO PANEL
& CNS
- Identifier/Rad/Dist or
- Identifiers/Radials or
- Region/Lat/Long
FLIGHT
MANAGEMENT
- Identifier
- Comment
# User Wpts Used
HAZARD
AVOIDANCE
GO BACK displayed if
User Wpt was created
on map page
Softkeys
Figure 5-45 User Waypoint Information Page
AFCS
Selecting a User Waypoint:
1) With the User Waypoint Information Page displayed, enter the name of the User Waypoint, or scroll to the
desired waypoint in the User Waypoint List using the large FMS Knob.
ADDITIONAL
FEATURES
2) Press the ENT Key.
3) Press the FMS Knob to remove the flashing cursor.
Or:
1) With the Nearest User Waypoints Page displayed, press the FMS Knob.
APPENDICES
2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest USR Box.
3) Press the FMS Knob to remove the flashing cursor.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
181
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Nearest User Wpt List
- Identifier
- Bearing/Distance from
aircraft position
FLIGHT
INSTRUMENTS
Navigation Map
Showing Selected
User Waypoint
EIS
User Waypoint Info
- Comment
- Lat/Long
AUDIO PANEL
& CNS
Selected User
Waypoint
Reference Wpt Info
- Identifier
- Radial/Distance
FLIGHT
MANAGEMENT
Figure 5-46 Nearest User Waypoint Page
CREATING USER WAYPOINTS
User waypoints can be created from the User Waypoint Information Page in the following ways:
HAZARD
AVOIDANCE
Creating user waypoints from the User Waypoint Information Page:
1) Select the NEW Softkey, or press the MENU Key and select ‘Create New User Waypoint’.
2) Enter a user waypoint name (up to six characters).
3) Press the ENT Key. The current aircraft position is the default location of the new waypoint.
AFCS
4) If desired, define the type and location of the waypoint in one of the following ways:
a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint
identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs.
ADDITIONAL
FEATURES
Or:
b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier,
the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs.
Or:
APPENDICES
c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into
the INFORMATION window using the FMS Knobs.
5) Press the ENT Key to accept the new waypoint.
6) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor
to “TEMPORARY” and selecting the ENT Key to check or uncheck the box.
INDEX
7) Press the FMS Knob to remove the flashing cursor.
Or:
182
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
1) Press the FMS Knob to activate the cursor.
2) Enter a user waypoint name (up to six characters).
FLIGHT
INSTRUMENTS
3) Press the ENT Key. The message ‘Are you sure you want to create the new User Waypoint AAAAAA?’ is
displayed.
4) With ‘YES’ highlighted, press the ENT Key.
5) If desired, define the type and location of the waypoint in one of the following ways:
a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint
identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs.
EIS
Or:
b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier,
the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs.
AUDIO PANEL
& CNS
Or:
c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into
the INFORMATION window using the FMS Knobs.
FLIGHT
MANAGEMENT
6) Press the ENT Key to accept the new waypoint.
7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor
to “TEMPORARY” and selecting the ENT Key to check or uncheck the box.
8) Press the FMS Knob to remove the flashing cursor.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 5-47 User Waypoint Information Page Menu
Creating user waypoints from map pages:
APPENDICES
1) Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint.
2) Press the ENT Key. The User Waypoint Information Page is displayed with the captured position.
NOTE: If the pointer has highlighted a map database feature, one of three things happens upon pressing
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
the ENT Key: 1) information about the selected feature is displayed instead of initiating a new waypoint,
2) a menu pops up allowing a choice between ‘Review Airspaces’ or ‘Create User Waypoint’, or 3) a new
waypoint is initiated with the default name being the selected map item.
183
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
3) Enter a user waypoint name (up to six characters).
4) Press the ENT Key to accept the selected name. The first reference waypoint box is highlighted.
FLIGHT
INSTRUMENTS
5) If desired, define the type and location of the waypoint in one of the following ways:
a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint
identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs.
Or:
b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier,
the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs.
EIS
Or:
AUDIO PANEL
& CNS
c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into
the INFORMATION window using the FMS Knobs.
6) Press the ENT Key to accept the new waypoint.
7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor
to “TEMPORARY” and selecting the ENT Key to check or uncheck the box.
FLIGHT
MANAGEMENT
8) Press the FMS Knob to remove the flashing cursor.
9) Select the GO BACK Softkey to return to the map page.
EDITING USER WAYPOINTS
HAZARD
AVOIDANCE
Editing a user waypoint comment or location:
1) With the User Waypoint Information Page displayed, press the FMS Knob to activate the cursor.
2) Select a user waypoint in the User Waypoint List, if required, and press the ENT Key.
3) Move the cursor to the desired field.
AFCS
4) Turn the small FMS Knob to make any changes.
5) Press the ENT Key to accept the changes.
6) Press the FMS Knob to remove the flashing cursor.
ADDITIONAL
FEATURES
Renaming user waypoints:
1) Highlight a user waypoint in the User Waypoint List. Select the RENAME Softkey, or press the MENU Key and
select ‘Rename User Waypoint’.
APPENDICES
2) Enter a new name.
3) Press the ENT Key. The message ‘Do you want to rename the user waypoint AAAAAA to BBBBBB?’ is
displayed.
4) With ‘YES’ highlighted, press the ENT Key.
INDEX
5) Press the FMS Knob to remove the flashing cursor.
184
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Changing the location of an existing waypoint to the aircraft present position:
1) Enter a waypoint name or select the waypoint in the User Waypoint List, then press the ENT Key.
2) Press the MENU Key.
FLIGHT
INSTRUMENTS
3) Select ‘Use Present Position’.
4) Press the ENT Key twice. The new waypoint’s location is saved.
5) Press the FMS Knob to remove the flashing cursor.
EIS
A system generated comment for a user waypoint incorporates the reference waypoint identifier, bearing,
and distance. If a system generated comment has been edited, a new comment can be generated.
Resetting the comment field to the system generated comment:
1) Enter a waypoint name or select the waypoint in the User Waypoint List, then press the ENT Key.
AUDIO PANEL
& CNS
2) Press the MENU Key.
3) Select ‘Auto Comment’.
4) Press the ENT Key. The generated comment is based on the reference point used to define the waypoint.
FLIGHT
MANAGEMENT
The default type of user waypoint (normal or temporary) can be changed using the user waypoint information
page menu. Temporary user waypoints are automatically deleted upon the next power cycle.
Changing the user waypoint storage duration default setting:
1) With the User Waypoint Information Page displayed, press the MENU Key.
HAZARD
AVOIDANCE
2) Move the cursor to select ‘Waypoint Setup’, and press the ENT Key.
3) Select ‘NORMAL’ or ‘TEMPORARY’ as desired, and press the ENT Key.
4) Press the FMS Knob to remove the flashing cursor and return to the User Waypoint Information Page.
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
185
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
DELETING USER WAYPOINTS
Deleting a single user waypoint:
FLIGHT
INSTRUMENTS
1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field.
2) Select the DELETE Softkey or press the CLR Key. ‘Yes’ is highlighted in the confirmation window.
3) Press the ENT Key.
4) Press the FMS Knob to remove the flashing cursor.
Or:
EIS
1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field.
2) Press the MENU Key.
AUDIO PANEL
& CNS
3) Select ‘Delete User Waypoint’.
4) Press the ENT Key twice to confirm the selection.
5) Press the FMS Knob to remove the flashing cursor.
FLIGHT
MANAGEMENT
NOTE: The option to ‘Delete All User Waypoints’ is not available while the aircraft is in flight.
Deleting all user waypoints:
1) Highlight a User Waypoint in the User Waypoint List.
HAZARD
AVOIDANCE
2) Press the MENU Key.
3) Select ‘Delete All User Waypoints’.
4) Press the ENT Key twice to confirm the selection.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
5) Press the FMS Knob to remove the flashing cursor.
186
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
5.4 AIRSPACES
FLIGHT
INSTRUMENTS
The G1000 can display the following types of airspaces: Class B/TMA, Class C/TCA, Class D, Restricted, MOA
(Military), Other Airspace, Air Defense Interdiction Zone (ADIZ), and Temporary Flight Restriction (TFR).
Class D Airspace
MOA (Military)
Class B Airspace
EIS
Restricted Area
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Class C Airspace
Alert Area
AFCS
ADIZ
ADDITIONAL
FEATURES
Warning Area
APPENDICES
Figure 5-48 Airspaces
The Nearest Airspaces Page, Airspace Alerts Window, and Airspace Alerts on the PFD provide additional
information about airspaces and the location of the aircraft in relationship to them.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
187
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off.
This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the
Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an
airspace.
An altitude buffer is also provided which “expands” the vertical range above or below an airspace. For example,
if the buffer is set at 500 feet, and the aircraft is more than 500 feet above/below an airspace, an alert message is
not generated, but if the aircraft is less than 500 feet above/below an airspace and projected to enter it, the pilot
is notified with an alert message. The default setting for the altitude buffer is 200 feet.
EIS
Changing the altitude buffer distance setting:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
AUDIO PANEL
& CNS
3) Turn the large FMS Knob to highlight the altitude buffer field in the Airspace Alerts Box.
4) Use the FMS Knob to enter an altitude buffer value and press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.
FLIGHT
MANAGEMENT
Turning an airspace alert on or off:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the desired field in the Airspace Alerts Box.
HAZARD
AVOIDANCE
4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF.
AFCS
5) Press the FMS Knob to remove the flashing cursor.
Airspace Alerts Box
APPENDICES
ADDITIONAL
FEATURES
- Airspace Altitude Buffer
- Alert On/Off
(Default Settings Shown)
DFLTS Softkey
INDEX
Figure 5-49 System Setup Page - Airspace Alerts
188
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Map ranges for the airspace boundaries are selected from the Aviation Group in the Map Setup Menu. See Table
5-2 for the default and maximum ranges for each type of airspace and the symbol used to define the airspace
area.
FLIGHT
INSTRUMENTS
The Nearest Airspaces Page can be used to quickly find airspaces close to the flight path. In addition, a selected
frequency associated with the airspace can be loaded from the Nearest Airspaces Page. In addition to displaying
a map of airspace boundaries and surrounding area, the Nearest Airspaces Page displays airspace information in
four boxes labeled ‘AIRSPACE ALERTS’, ‘AIRSPACE, AGENCY’, ‘VERTICAL LIMITS’, and ‘FREQUENCIES’.
Airspace 1
Airspace/Agency Info
- Airspace Type
- Controlling Agency
Airspace 2
FLIGHT
MANAGEMENT
Airspace Vertical Limits
- Ceiling
- Floor
Airspace 3
Associated Frequencies
HAZARD
AVOIDANCE
- Type
- Availability/Info
- Frequency
Softkeys
AUDIO PANEL
& CNS
- Name
- Proximity (Ahead, Inside,
Ahead < 2nm, Within 2nm)
- Time till Intercept (only if
Ahead or Ahead < 2nm)
EIS
Airspace Alerts Info
Figure 5-50 Nearest Airspaces Page
AFCS
Airspace alerts and associated frequencies are shown in scrollable lists on the Nearest Airspaces Page. The
ALERTS and FREQ softkeys place the cursor in the respective list. The FREQ Softkey is enabled only if one or
more frequencies exist for a selected airspace.
Selecting and viewing an airspace alert with its associated information:
ADDITIONAL
FEATURES
1) Select the Nearest Airspaces Page.
2) Select the ALERTS Softkey; or press the FMS Knob; or press the MENU Key, highlight ‘Select Alerts Window’,
and press the ENT Key. The cursor is placed in the ‘AIRSPACE ALERTS’ Box.
3) Select the desired airspace.
APPENDICES
4) Press the FMS Knob to remove the flashing cursor.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
189
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Selecting the PFD ALERTS Softkey displays the message window on the PFD. The following airspace alerts are
displayed in the message window:
EIS
FLIGHT
INSTRUMENTS
Message
INSIDE ARSPC – Inside airspace.
ARSPC AHEAD – Airspace ahead –
less than 10 minutes.
ARSPC NEAR – Airspace near and
ahead.
ARSPC NEAR – Airspace near
– less than 2 nm.
Comments
The aircraft is inside the airspace.
Special use airspace is ahead of aircraft. The aircraft penetrates the airspace within 10
minutes.
Special use airspace is near and ahead of the aircraft position.
Special use airspace is within 2 nm of the aircraft position.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Table 5-6 PFD Airspace Alert Messages
190
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
5.5 DIRECT-TO-NAVIGATION
FLIGHT
INSTRUMENTS
The Direct-to method of navigation, initiated by pressing the Direct-to Key on either the MFD or PFD, is
quicker to use than a flight plan when the desire is to navigate to a single point such as a nearby airport.
Once a direct-to is activated, the G1000 establishes a point-to-point course line from the present position to the
selected direct-to destination. Course guidance is provided until the direct-to is replaced with a new direct-to or
flight plan, or cancelled.
EIS
A vertical navigation (VNV) direct-to creates a descent path (and provides guidance to stay on the path) from
the current altitude to a selected altitude at the direct-to waypoint. Vertical navigation is based on barometric
altitudes, not on GPS altitude, and is used for cruise and descent phases of flight.
The Direct-to Window allows selection and activation of direct-to navigation. The Direct-to Window displays
selected direct-to waypoint data on the PFD and the MFD.
AUDIO PANEL
& CNS
Direct-to Point Info
FLIGHT
MANAGEMENT
- Identifier/Symbol/Region
- Facility Name
- City
VNV Constraints
- Altitude at Arrival
- Along Track Offset
Map of Selected Point
HAZARD
AVOIDANCE
Location of Destination
- Bearing/Distance
AFCS
Desired Course
Figure 5-51 Direct-to Window - MFD
ADDITIONAL
FEATURES
Direct-to Point Info
- Identifier/Symbol/City
- Facility Name
APPENDICES
VNV Constraints
- Altitude at Arrival
- Along Track Offset
Direct-to Point Info
- Bearing/Distance
- Desired Course
INDEX
Activation Command
Figure 5-52 Direct-to Window - PFD
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
191
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Any waypoint can be entered as a direct-to destination from the Direct-to Window.
Entering a waypoint identifier, facility name, or city as a direct-to destination:
FLIGHT
INSTRUMENTS
1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan wayoint as the default
selection or a blank waypoint field if no flight plan is active).
EIS
2) Turn the small FMS Knob clockwise to begin entering a waypoint identifier (turning it counter-clockwise brings
up the waypoint selection submenu - press the CLR Key to remove it), or turn the large FMS Knob to select the
facility name, or city field and turn the small FMS Knob to begin entering a facility name or city. If duplicate
entries exist for the entered facility or city name, additional entries can be viewed by turning the small FMS
Knob during the selection process.
3) Press the ENT Key. The ‘Activate?’ field is highlighted.
AUDIO PANEL
& CNS
4) Press the ENT Key to activate the direct-to.
Any waypoint contained in the active flight plan can be selected as a direct-to waypoint from the Direct-to
Window, the Active Flight Plan Page, or the Active Flight Plan Window.
Waypoint Submenu
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
- Flight Plan Waypoints
- Nearest Airports
- Recent Waypoints
- User Waypoints
- Airway Waypoints
(only available when
active leg is part of an
airway)
Figure 5-53 Waypoint Submenu
Selecting an active flight plan waypoint as a direct-to destination:
AFCS
1) While navigating an active flight plan, press the Direct-to Key. The Direct-to Window is displayed with the
active flight plan waypoint as the default selection.
ADDITIONAL
FEATURES
2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated
only when navigating a flight plan).
3) Select the desired waypoint.
4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
APPENDICES
5) Press the ENT Key again to activate the direct-to.
Or:
1) Select the Active Flight Plan Page on the MFD, or the Active Flight Plan Window on the PFD.
2) Select the desired waypoint.
INDEX
3) Press the Direct-to Key.
4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
5) Press the ENT Key again to activate the direct-to.
192
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Any NRST, RECENT, USER, or AIRWAY waypoint can be selected as a direct-to destination in the Direct-to
Window.
Selecting a NRST, RECENT, USER, or AIRWAY waypoint as a direct-to destination:
FLIGHT
INSTRUMENTS
1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan destination as the
default selection or a blank destination if no flight plan is active).
2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated
only when navigating a flight plan).
3) Turn the small FMS Knob clockwise to display the NRST, RECENT, USER, or AIRWAY waypoints.
EIS
4) Turn the large FMS Knob clockwise to select the desired waypoint.
5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
AUDIO PANEL
& CNS
6) Press the ENT Key again to activate the direct-to.
FLIGHT
MANAGEMENT
The Direct-to Window can be displayed from any page and allows selection and activation of direct-to navigation.
If the direct-to is initiated from any page except the WPT pages, the default waypoint is the active flight plan
waypoint (if a flight plan is active) or a blank waypoint field. Direct-to requests on any WPT page defaults to the
displayed waypoint.
Selecting any waypoint as a direct-to destination:
1) Select the page or window containing the desired waypoint type and select the desired waypoint.
HAZARD
AVOIDANCE
2) Press the Direct-to Key to display the Direct-to Window with the selected waypoint as the direct-to
destination.
3) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
4) Press ENT again to activate the direct-to.
Selecting a nearby airport as a direct-to destination:
AFCS
1) Press the NRST Softkey on the PFD; or turn the FMS Knob to display the Nearest Airports Page and press the
FMS Knob.
2) Select the desired airport (the nearest one is already selected).
ADDITIONAL
FEATURES
3) Press the Direct-to Key.
4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
5) Press the ENT Key again to activate the direct-to.
APPENDICES
Direct-to destinations may also be selected by using the pointer on the navigation map pages. If no airport,
NAVAID, or user waypoint exists at the desired location, a temporary waypoint named ‘MAPWPT’ is automatically
created at the location of the map arrow.
Selecting a waypoint as a direct-to destination using the pointer:
1) From a navigation map page, press the Joystick to display the pointer.
INDEX
2) Move the Joystick to place the pointer at the desired destination location.
3) If the pointer is placed on an existing airport, NAVAID, or user waypoint, the waypoint name is highlighted.
4) Press the Direct-to Key to display the Direct-to Window with the selected point entered as the direct-to
destination.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
193
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
6) Press the ENT Key again to activate the direct-to.
FLIGHT
INSTRUMENTS
Cancelling a Direct-to:
1) Press the Direct-to Key to display the Direct-to Window.
2) Press the MENU Key.
EIS
3) With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a flight plan is still active, the G1000 resumes
navigating the flight plan along the closest leg.
Page Menu
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
- Cancel Direct-To
Navigation
Figure 5-54 Direct-to Window - Cancelling Direct-to Navigation
AFCS
When navigating a direct-to, the G1000 sets a direct great circle course to the selected destination. The course
to a destination can also be manually selected using the course field (‘COURSE’) on the Direct-to Window.
Selecting a manual direct-to course:
ADDITIONAL
FEATURES
1) Press the Direct-to Key. The Direct-to Window is displayed with the destination field highlighted.
2) Highlight the course field.
3) Enter the desired course.
APPENDICES
4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
5) Press the ENT Key again to activate the direct-to.
Reselecting the direct course from the current position:
1) Press the Direct-to Key. The Direct-to Window is displayed with the destination field highlighted.
INDEX
2) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
3) Press the ENT Key again to activate the direct-to.
194
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
A direct-to with altitude constraints creates a descent path (and provides guidance to stay on the path) from
the aircraft’s current altitude to the altitude of the direct-to waypoint. The altitude is reached at the waypoint,
or at the specified distance along the flight path if an offset distance has been entered. All VNV altitudes prior
to the direct-to destination are removed from the active flight plan upon successful activation of the direct-to.
All VNV altitudes following the direct-to waypoint are retained. See the section on Vertical Navigation for more
information regarding the use and purpose of VNV altitudes and offset distances.
Entering a VNV altitude and along-track offset for the waypoint:
1) Press the Direct-to Key to display the Direct-to Window.
EIS
2) Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
3) Enter the desired altitude.
4) Press the ENT Key. The option to select MSL or AGL is now displayed.
AUDIO PANEL
& CNS
5) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
6) Press the ENT Key. The cursor is now flashing in the VNV offset distance field.
7) Enter the desired along-track distance before the waypoint.
FLIGHT
MANAGEMENT
8) Press the ENT Key. The ‘Activate?’ field is highlighted.
9) Press the ENT Key to activate.
Removing a VNV altitude constraint:
1) Press the Direct-to Key to display the Direct-to Window.
HAZARD
AVOIDANCE
2) Press the MENU Key.
3) With ‘Clear Vertical Constraints’ highlighted, press the ENT Key.
AFCS
Page Menu
- Clear Vertical Navigation
Constraints
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 5-55 Direct-to Window - Clearing Vertical Constraints
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
195
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
5.6 FLIGHT PLANNING
FLIGHT
INSTRUMENTS
Flight planning on the G1000 consists of building a flight plan by entering waypoints one at a time, adding
waypoints along airways, and inserting departures, airways, arrivals, or approaches as needed. The G1000 allows
flight planning information to be entered from either the MFD or PFD. The flight plan is displayed on maps using
different line widths, colors, and types, based on the type of leg and the segment of the flight plan currently being
flown (departure, enroute, arrival, approach, or missed approach).
Flight Plan Leg Type
Symbol
EIS
Active non-heading Leg
AUDIO PANEL
& CNS
Active heading Leg
Non-heading Leg in the current flight segment
FLIGHT
MANAGEMENT
Heading Leg not in the current flight segment
Non-heading Leg not in the active flight segment
HAZARD
AVOIDANCE
Turn Anticipation Arc
Table 5-7 Flight Plan Leg Symbols
ADDITIONAL
FEATURES
AFCS
Up to 99 flight plans with up to 99 waypoints each can be created and stored in memory. One flight plan can be
activated at a time and becomes the active flight plan. The active flight plan is erased when the system is turned
off and overwritten when another flight plan is activated. When storing flight plans with an approach, departure,
or arrival, the G1000 uses the waypoint information from the current database to define the waypoints. If the
database is changed or updated, the G1000 automatically updates the information if the procedure has not been
modified. If an approach, departure, or arrival procedure is no longer available, the procedure is deleted from the
affected stored flight plan(s), and an alert is displayed (see Miscellaneous Messages in Appendix A) advising that
one or more stored flight plans need to be edited.
APPENDICES
Whenever an approach, departure, or arrival procedure is loaded into the active flight plan, a set of approach,
departure, or arrival waypoints is inserted into the flight plan along with a header line describing the instrument
procedure the pilot selected. The original enroute portion of the flight plan remains active (unless an instrument
procedure is activated) when the procedure is loaded.
INDEX
When the database is updated, the airways need to be reloaded also. Each airway segment is reloaded from
the database given the entry waypoint, the airway identifier and the exit waypoint. This reloads the sequence of
waypoints between the entry and exit waypoints (the sequence may change when the database is updated). The
update of an airway can fail during this process. If that happens, the airway waypoints are changed to regular
(non-airway) flight plan waypoints, and an alert is displayed (see Miscellaneous Messages in Appendix A).
196
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
The following could cause the airway update to fail:
• Airway identifier, entry waypoint or exit waypoint not found in the new database.
FLIGHT
INSTRUMENTS
• Airway entry/exit waypoint is not an acceptable waypoint for the airway – either the waypoint is no longer on
the airway, or there is a new directional restriction that prevents it being used.
• Loading the new airway sequence would exceed the capacity of the flight plan.
FLIGHT PLAN CREATION
There are three methods to create or modify a flight plan:
EIS
• Active Flight Plan Page on the MFD (create/modify the active flight plan)
• Active Flight Plan Window on the PFD (create/modify the active flight plan)
• Flight Plan Catalog Page on the MFD (create/modify a stored flight plan)
AUDIO PANEL
& CNS
Active FPL Waypoint List
Active Flight
Plan Leg
FLIGHT
MANAGEMENT
- Comment
- Procedure Header
- Waypoint Identifier
- Airway Identifier
- Desired Track to Waypoint
- Distance to Waypoint
- Waypoint Altitude Constraint
HAZARD
AVOIDANCE
Vertical Navigation Profile
Turn Anticipation Arc
Non-Active,
Flight Plan Leg
AFCS
- Active Vertical WPT Alt/ID
- Vertical Speed Target
- Flight Path Angle
- Vertical Speed Target
- Time to Top of Descent
- Vertical Deviation
Figure 5-56 Active Flight Plan Page
ADDITIONAL
FEATURES
Active Flight Plan Comment
APPENDICES
Active Flight
Plan Leg
Active Flight Plan Waypoint List
- Waypoint ID
- Desired Track to Waypoint
- Distance to Waypoint
- Airway Identifier
INDEX
Figure 5-57 Active Flight Plan Window on PFD
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
197
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Catalog Contents
FLIGHT
INSTRUMENTS
- # Used
- # Empty
Flight Plan List
- Comment
EIS
Selected Flight
Plan Map
AUDIO PANEL
& CNS
Selected FPL Info
- Departure Waypoint
- Destination Waypoint
- Total Flight Plan Distance
- Enroute Safe Altitude
Softkeys
FLIGHT
MANAGEMENT
Figure 5-58 Flight Plan Catalog Page
The active flight plan is listed on the active Flight Plan Page on the MFD, and in the Active Flight Plan
Window on the PFD. It is the flight plan to which the G1000 is currently providing guidance, and is shown
on the navigation maps. Stored flight plans are listed on the Flight Plan Catalog Page, and are available for
activation (becomes the active flight plan).
HAZARD
AVOIDANCE
Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
AFCS
3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway
waypoints).
ADDITIONAL
FEATURES
4) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of
waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered.
5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint.
INDEX
APPENDICES
6) When all waypoints have been entered, press the FMS Knob to remove the cursor.
198
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
FLIGHT
INSTRUMENTS
3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New Flight Plan’, and press the ENT Key to
display a blank flight plan for the first empty storage location.
4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a
waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints).
EIS
5) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of
waypoints and press the ENT Key.
6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
AUDIO PANEL
& CNS
7) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new
flight plan is now in the list.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
199
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Flight plans can be imported from an SD Card or exported to an SD Card from the Stored Flight Plan Page.
Importing a Flight Plan from an SD Card
FLIGHT
INSTRUMENTS
1) Insert the SD card containing the flight plan in the top card slot on the MFD.
2) Press the FPL Key to display the Active Flight Plan Page on the MFD.
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
4) Press the FMS Knob to activate the cursor.
5) Turn either FMS Knob to highlight an empty or existing flight plan.
EIS
6) Press the IMPORT Softkey; or press the MENU Key, select “Import Flight Plan”, and press the ENT Key.
If an empty slot is selected, a list of the available flight plans on the SD card will be displayed.
AUDIO PANEL
& CNS
Or:
FLIGHT
MANAGEMENT
If an existing flight plan is selected, an “Overwrite existing flight plan? OK or CANCEL” prompt is displayed.
Press the ENT Key to choose to overwrite the selected flight plan and see the list of available flight plans on the
SD card. If overwriting the existing flight plan is not desired, select “CANCEL” using the FMS Knob, press the
ENT Key, select another flight plan slot, and press the IMPORT Softkey again.
7) Turn the small FMS Knob to highlight the desired flight plan for importing.
8) Press the ENT Key to initiate the import.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
9) Press the ENT Key again to confirm the import.
Import/Export Softkeys
List of Flight Plans to Import &
Details for the Selected File
Import Successful
INDEX
Figure 5-59 Flight Plan Import
200
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
NOTE: If the imported flight plan contains a waypoint with a name that duplicates the name of a waypoint
FLIGHT
INSTRUMENTS
already stored on the system, the system compares the coordinates of the imported waypoint with those of
the existing waypoint. If the coordinates are different, the imported waypoint is automatically renamed by
adding characters to the end of the name.
Exporting a Flight Plan to an SD Card
1) Insert the SD card into the top card slot on the MFD.
2) Press the FPL Key to display the Active Flight Plan Page on the MFD.
EIS
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
4) Press the FMS Knob to activate the cursor.
AUDIO PANEL
& CNS
5) Turn the large FMS Knob to highlight the flight plan to be exported.
6) Press the EXPORT Softkey; or press the MENU Key, select “Export Flight Plan”.
7) If desired, change the name for the exported file by turning the large FMS Knob to the left to highlight the
name, then use the small and large FMS knobs to enter the new name, and press the ENT Key.
FLIGHT
MANAGEMENT
8) Press the ENT Key to initiate the export.
9) Press the ENT Key to confirm the export.
NOTE: The exported flight plan will not contain any procedures or airways.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
Import/Export Softkeys
Stored Flight Plan to be Exported &
Exported Flight Plan Name
Export Successful
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
Figure 5-60 Flight Plan Export
201
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
ADDING WAYPOINTS TO AN EXISTING FLIGHT PLAN
FLIGHT
INSTRUMENTS
Waypoints can be added to the active flight plan or any stored flight plan. Choose the flight plan, select the
desired point of insertion, enter the waypoint, and it is added in front of the selected waypoint. Flight plans
are limited to 99 waypoints (including waypoints within airways and procedures). If the number of waypoints
in the flight plan exceeds 99, the message “Flight plan is full. Remove unnecessary waypoints.” appears and the
new waypoint(s) are not added to the flight plan.
Stored Flight Plan Selected
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
- Memory Slot
- Comment
- Procedure Identifier
- Waypoint Identifier
- Airway Identifier
- Desired Track to Waypoint
- Distance to Waypoint
- Waypoint Altitude Constraint
HAZARD
AVOIDANCE
Softkeys
ADDITIONAL
FEATURES
AFCS
Figure 5-61 Stored Flight Plan Page
APPENDICES
Flight Plan Full Message
Figure 5-62 Active Flight Plan Page - FPL Full
Adding a waypoint to a stored flight plan:
INDEX
1) On the Flight Plan Catalog Page, press the FMS Knob to activate the cursor.
2) Highlight the desired flight plan.
202
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
3) Select the EDIT Softkey; or press the ENT Key, turn the large FMS Knob clockwise to select “EDIT” and press
the ENT Key. The Stored Flight Plan Page is displayed.
FLIGHT
INSTRUMENTS
4) Select the point in the flight plan to add the new waypoint. The new waypoint is placed directly in front of the
highlighted waypoint.
5) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway
waypoints).
EIS
6) Enter the identifier, facility, or city name of the waypoint or select a waypoint from the submenu of waypoints
and press the ENT Key. The new waypoint now exists in the flight plan.
NOTE: If the identifier entered in the Waypoint Information Window has duplicates, a Duplicate Waypoint
AUDIO PANEL
& CNS
Window is displayed. Use the FMS Knob to select the correct waypoint.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
Figure 5-63 Duplicate Waypoints Window
Adding a waypoint to the active flight plan:
ADDITIONAL
FEATURES
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (not required on the PFD).
APPENDICES
3) Select the point in the flight plan before which to add the new waypoint. The new waypoint is placed directly
in front of the highlighted waypoint.
4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway
waypoints).
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
5) Enter the identifier, facility, or city name of the waypoint or select a waypoint from the submenu of waypoints
and press the ENT Key. The active flight plan is modified as each waypoint is entered.
203
SYSTEM
OVERVIEW
Creating and adding user waypoints to the active flight plan:
FLIGHT
INSTRUMENTS
FLIGHT MANAGEMENT
2) Select the LD WPT Softkey; or press the MENU Key, select ‘Load Waypoint’, and press the ENT Key. The user
waypoint is created with a name of USRxxx (using the next available in sequence) and is added to the end of
the active flight plan.
1) Press the Joystick to activate the panning function on the Active Flight Plan Page and pan to the map location
of the desired user waypoint.
ADDING AIRWAYS TO A FLIGHT PLAN
AUDIO PANEL
& CNS
EIS
Airways can be added to the active flight plan or any stored flight plan. Choose a flight plan (add the desired
airway entry point if not already in the flight plan), select the waypoint after the desired airway entry point,
select the airway, and it is added in front of the selected waypoint. An airway can only be loaded if there is a
waypoint in the flight plan that is part of the desired airway and is not part of an arrival or approach procedure.
The G1000 also anticipates the desired airway and exit point based on loaded flight plan waypoints.
Airway Entry Waypoint
FLIGHT
MANAGEMENT
Selected Airway
Airways Available at TOP
Airway Waypoint
Sequence
AFCS
HAZARD
AVOIDANCE
Preview of
Selected Airway
ADDITIONAL
FEATURES
Figure 5-64 Select Airway Page - Selecting Airway
Adding an airway to a flight plan:
1) Press the FPL Key.
APPENDICES
2) Press the FMS Knob to activate the cursor (not required on the PFD).
3) Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. If this waypoint is not
a valid airway entry point, a valid entry point should be entered at this time.
INDEX
4) Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey, or press the MENU Key and
select “Load Airway”. The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu
item is available only when a valid airway entry waypoint has been chosen (the waypoint ahead of the cursor
position).
204
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are
shown first in the list, followed by “all” altitude airways, and then high altitude airways.
FLIGHT
INSTRUMENTS
6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is
highlighted.
7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted.
Airway Entry Waypoint
Selected Airway
EIS
Selected Exit Point
Preview of
Selected Airway
AUDIO PANEL
& CNS
Selected Airway
Exit Point
Airway Exit Points
Available
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 5-65 Select Airway Page - Selecting Exit Point
AFCS
ADDITIONAL
FEATURES
Inserted Airway Header
- Airway Identifier: [airway
identifier].[exit waypoint identifier]
(e.g., V4.SLN)
APPENDICES
INDEX
Figure 5-66 Active Flight Plan Page - Airway Inserted
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
205
SYSTEM
OVERVIEW
RESTRICTIONS ON ADDING AIRWAYS
FLIGHT
INSTRUMENTS
FLIGHT MANAGEMENT
Airway “UR975” in North Africa has more complicated directional restrictions within the list of airway
waypoints AMANO, VAKOR, LIBRO, NELDA, DIRKA, GZO, KOSET, and SARKI:
Some airways have directional restrictions on all or part of the route. Airway “A2” in Europe has a directional
restriction over the whole route such that it can be flown only in the direction MTD-ABB-BNE-DEVAL.
• Starting from AMANO, the airway can be flown only to LIBRO.
• Starting from SARKI, the airway can be flown only to LIBRO.
EIS
• Between NELDA and GZO, the airway can be flown in either direction.
In the US, airways that are “one-way” for specified hours of operation are not uncommon. These airways
are always bidirectional in the G1000 database.
AUDIO PANEL
& CNS
The system only allows correct airway sequences to be inserted. If the pilot subsequently inverts the flight
plan, the system inverts the airway waypoint sequence and removes the airway header. ADDING PROCEDURES TO A STORED FLIGHT PLAN
FLIGHT
MANAGEMENT
The G1000 allows the pilot to insert pre-defined instrument procedures from the navigation database into a
flight plan. The procedures are designed to facilitate routing of traffic leaving an airport (departure), arriving at
an airport (arrival), and landing at an airport (approach). See the procedures section for more details.
HAZARD
AVOIDANCE
Flight Plan Name
AFCS
Flight Plan
Waypoint List
Softkeys
ADDITIONAL
FEATURES
Load Departure Load Arrival Load Approach Activate Flight Plan
INDEX
APPENDICES
Figure 5-67 Stored Flight Plan Page
206
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
DEPARTURE (DP)
FLIGHT
INSTRUMENTS
A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can
be loaded at a time in a flight plan. The route is defined by selection of a departure, the transition waypoints,
and a runway.
Departure Airport
EIS
Selected
Departure
Departures Available at
KMCI
AUDIO PANEL
& CNS
Preview of
Selected
Departure
Departure Waypoint
Sequence
FLIGHT
MANAGEMENT
Figure 5-68 Departure Loading Page - Selecting the Departure
HAZARD
AVOIDANCE
Loading a departure procedure into a stored flight plan:
1) Select a stored flight plan from the Flight Plan Catalog Page.
2) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and press the ENT Key. The Stored
Flight Plan Page is displayed.
AFCS
3) Select the LD DP Softkey; or press the MENU Key, select “Load Departure”, and press the ENT Key. The
Departure Loading Page is displayed.
4) Select a departure. Press the ENT Key.
ADDITIONAL
FEATURES
5) Select a transition for the selected departure. Press the ENT Key.
6) Select a runway served by the selected departure, if required. Press the ENT Key.
7) Press the ENT Key to load the selected departure procedure.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
207
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Departure Airport
FLIGHT
INSTRUMENTS
Selected
Departure
Selected Runway
Preview of
Selected
Departure
Selected Transition
Departure Transition
Points Available
AUDIO PANEL
& CNS
EIS
Selected
Departure End
Point
FLIGHT
MANAGEMENT
Figure 5-69 Departure Loading Page - Selecting Transition
Inserted Departure Header
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
- Departure Identifier: [departure
airport]-[departure runway].
[departure transition].
[departure end point]
(e.g., KMKC-ALL.WLDCT2.ICT)
INDEX
APPENDICES
Figure 5-70 Stored Flight Plan Page - Departure Inserted
208
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
ARRIVAL (STAR)
FLIGHT
INSTRUMENTS
A Standard Terminal Arrival (STAR) is loaded at the destination airport in the flight plan. Only one arrival
can be loaded at a time in a flight plan. The route is defined by selection of an arrival, the transition waypoints,
and a runway.
Destination Airport
Selected Arrival
EIS
Arrivals Available at
KCOS
Selected Runway
AUDIO PANEL
& CNS
Arrival Waypoint
Sequence
Preview of
Selected Arrival
FLIGHT
MANAGEMENT
Figure 5-71 Arrival Loading Page - Selecting the Arrival
HAZARD
AVOIDANCE
Loading an arrival procedure into a stored flight plan:
1) Select a stored flight plan from the Flight Plan Catalog Page.
2) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and press the ENT Key. The Stored
Flight Plan Page is displayed.
AFCS
3) Select the LD STAR Softkey; or press the MENU Key, select “Load Arrival”, and press the ENT Key. The Arrival
Loading Page is displayed.
4) Select an arrival. Press the ENT Key.
ADDITIONAL
FEATURES
5) Select a transition for the selected arrival. Press the ENT Key.
6) Select a runway served by the selected arrival, if required. Press the ENT Key.
7) Press the ENT Key to load the selected arrival procedure.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
209
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Destination Airport
FLIGHT
INSTRUMENTS
Selected Arrival
Selected Transition
Transitions Available
with DBRY1
Arrival Waypoint
Sequence
AUDIO PANEL
& CNS
EIS
Preview of
Selected Arrival
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Figure 5-72 Arrival Loading Page - Selecting the Transition
Inserted Arrival Header
ADDITIONAL
FEATURES
AFCS
- Arrival Identifier:
[arrival airport]-[arrival transition].
[arrival].[arrival runway]
(e.g., KCOS-ALS.DBRY1.ALL)
INDEX
APPENDICES
Figure 5-73 Stored Flight Plan Page - Arrival Inserted
210
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
APPROACH (APPR)
FLIGHT
INSTRUMENTS
An Approach Procedure (APPR) can be loaded at any airport that has an approach available. Only one
approach can be loaded at a time in a flight plan. The route for a selected approach is defined by designating
transition waypoints.
Destination Airport
EIS
Selected
Approach
Approaches Available
at KCOS
Preview of
Selected
Approach
AUDIO PANEL
& CNS
Barometric Minimum
Approach Waypoint
Sequence
FLIGHT
MANAGEMENT
Figure 5-74 Approach Loading Page - Selecting the Approach
HAZARD
AVOIDANCE
Loading an approach procedure into a stored flight plan:
1) Select a stored flight plan from the Flight Plan Catalog Page.
AFCS
2) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and press the ENT Key. The Stored
Flight Plan Page is displayed.
3) Select the LD APR Softkey; or press the MENU Key, select “Load Approach”, and press the ENT Key. The
Approach Loading Page is displayed.
ADDITIONAL
FEATURES
4) Select an approach. Press the ENT Key.
5) Select a transition for the selected approach. Press the ENT Key.
6) Press the ENT Key to load the selected approach procedure.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
211
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
Selected
Approach
EIS
Destination Airport
Preview of
Selected
Approach
Selected Transition
Transitions Available with
Selected Approach
Barometric Minimum
Approach Waypoint
Sequence
AUDIO PANEL
& CNS
Load Approach?
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Figure 5-75 Approach Loading Page - Selecting the Transition
Inserted Approach Header
ADDITIONAL
FEATURES
AFCS
- Approach Identifier: [approach
airport].[runway and approach type]
INDEX
APPENDICES
Figure 5-76 Stored Flight Plan Page - Approach Inserted
212
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FLIGHT PLAN STORAGE
FLIGHT
INSTRUMENTS
The G1000 can store up to 99 flight plans, numbered 1 through 99. The active flight plan is erased when
the G1000 is powered off or when another flight plan is activated. Details about each stored flight plan can be
viewed on the Flight Plan Catalog Page and on the Stored Flight Plan Page.
Viewing information about a stored flight plan:
1) Press the FPL Key on the MFD to display the Active Flight Plan Page.
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
EIS
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired flight plan.
4) The Flight Plan Information is displayed showing departure, destination, total distance, and enroute safe altitude
information for the selected Flight Plan.
AUDIO PANEL
& CNS
5) Select the EDIT Softkey to open the Stored Flight Plan Page and view the waypoints in the flight plan.
6) Press the FMS Knob to exit the Stored Flight Plan Page.
FLIGHT
MANAGEMENT
Flight Plan Name
(Comment)
Selected Flight Plan
HAZARD
AVOIDANCE
Preview of Selected
Flight Plan
Stored Flight Plan Info
AFCS
- Departure Airport
- Destination Airport
- Total Flight Plan Distance
- Enroute Safe Altitude
ADDITIONAL
FEATURES
Stored FPL Editing Softkeys
Figure 5-77 Stored Flight Plan Information
Storing an active flight plan from the Active Flight Plan Page or the Active Flight Plan Window:
APPENDICES
1) Press the MENU Key.
2) Highlight ‘Store Flight Plan’.
3) Press the ENT Key.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
4) With ‘OK’ highlighted, press the ENT Key. The flight plan is stored in the next available position in the flight
plan list on the Flight Plan Catalog Page.
213
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
ACTIVATE A FLIGHT PLAN
FLIGHT
INSTRUMENTS
Activating a stored flight plan erases the active flight plan and replaces it with the flight plan being activated.
Inverting a stored flight plan reverses the waypoint order, erases the active flight plan, and replaces it with the
flight plan being activated (the stored flight plan is not changed).
Activating a stored flight plan on the MFD:
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.
EIS
3) Select the ACTIVE Softkey; or press the MENU Key, highlight ‘Activate Flight Plan’, and press the ENT Key. The
‘Activate Stored Flight Plan?’ window is displayed.
AUDIO PANEL
& CNS
4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
Inverting and activating a stored flight plan on the MFD:
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
FLIGHT
MANAGEMENT
2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.
3) Select the INVERT Softkey; or press the MENU Key, highlight ‘Invert & activate FPL?’, and press the ENT Key.
The ‘Invert and activate stored flight plan?’ window is displayed.
HAZARD
AVOIDANCE
4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
COPY A FLIGHT PLAN
AFCS
The G1000 allows copying a flight plan into a new flight plan memory slot, allowing editing, etc., without
affecting the original flight plan. This can be used to duplicate an existing stored flight plan for use in creating
a modified version of the original stored flight plan.
Copying a stored flight plan on the MFD:
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
ADDITIONAL
FEATURES
2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.
3) Select the COPY Softkey; or press the MENU Key, highlight ‘Copy Flight Plan’, and press the ENT Key. The
‘Copy to Flight Plan XX?’ window is displayed.
APPENDICES
4) With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel the request, press the CLR Key, or
highlight ‘CANCEL’ and press the ENT Key.
DELETE A STORED FLIGHT PLAN
Individual or all stored flight plans can be deleted from the G1000 memory.
INDEX
Deleting a stored flight plan:
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.
214
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
3) Select the DELETE Softkey; press the CLR Key; or press the MENU Key, highlight ‘Delete Flight Plan’, and press
the ENT Key. The ‘Delete Flight Plan XX?’ window is displayed.
FLIGHT
INSTRUMENTS
4) With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel the request, press the CLR Key, or
highlight ‘CANCEL’ and press the ENT Key.
NOTE: The option to delete all stored flight plans is not available while the aircraft is in flight.
Deleting all stored flight plans:
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
EIS
2) Press the MENU Key.
3) Highlight ‘Delete All’ and press the ENT Key. A ‘Delete all flight plans?’ confirmation window is displayed.
AUDIO PANEL
& CNS
4) With ‘OK’ highlighted, press the ENT Key to delete all flight plans. To cancel the request, press the CLR Key, or
highlight ‘CANCEL’ and press the ENT Key.
FLIGHT PLAN EDITING
FLIGHT
MANAGEMENT
The active flight plan or any stored flight plan can be edited. The edits made to the active flight plan affect
navigation as soon as they are entered.
DELETING THE ACTIVE FLIGHT PLAN
HAZARD
AVOIDANCE
The G1000 allows deleting an active flight plan. Deleting the active flight plan suspends navigation by the
G1000.
Deleting the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
AFCS
2) Press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key. The ‘Delete all waypoints in flight
plan?’ window is displayed.
3) With ‘OK’ highlighted, press the ENT Key to delete the active flight plan. To cancel the request, press the CLR
Key, or highlight ‘CANCEL’ and press the ENT Key.
ADDITIONAL
FEATURES
DELETING FLIGHT PLAN ITEMS
Individual waypoints, entire airways, and entire procedures can be deleted from a flight plan. Some waypoints
in the final approach segment (such as the FAF or MAP) can not be deleted individually. Attempting to delete
a waypoint that is not allowed results in a window displaying ‘Invalid flight plan modification.’
APPENDICES
Deleting an individual waypoint from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the waypoint to be deleted.
INDEX
3) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
215
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Deleting an entire airway from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
FLIGHT
INSTRUMENTS
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the white header of the airway to be deleted.
3) Press the CLR Key. The ‘Remove <airway name>?’ window is displayed.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
EIS
5) Press the FMS Knob to remove the flashing cursor.
Deleting an entire procedure from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
AUDIO PANEL
& CNS
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the white header of the procedure to be deleted.
3) Press the CLR Key. The ‘Remove <procedure name> from flight plan?’ window is displayed.
FLIGHT
MANAGEMENT
4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.
Or:
HAZARD
AVOIDANCE
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the MENU Key to display the Page Menu and turn the FMS Knob to highlight ‘Remove <procedure>’.
3) Press the ENT Key. The ‘Remove <procedure name> from flight plan?’ window is displayed.
AFCS
4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
Deleting an individual waypoint from a stored flight plan:
1) Press the FPL Key to display the Active Flight Plan Page.
ADDITIONAL
FEATURES
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.
APPENDICES
5) Turn the large FMS Knob to highlight the waypoint to be deleted.
6) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed.
7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
INDEX
8) Press the FMS Knob to remove the flashing cursor.
216
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Deleting an entire airway from a stored flight plan:
1) Press the FPL Key to display the Active Flight Plan Page.
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
FLIGHT
INSTRUMENTS
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.
5) Turn the large FMS Knob to highlight the white header of the airway to be deleted.
EIS
6) Press the CLR Key. The ‘Remove <airway name>?’ window is displayed.
7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
AUDIO PANEL
& CNS
8) Press the FMS Knob to remove the flashing cursor.
Deleting an entire procedure from a stored flight plan:
1) Press the FPL Key to display the Active Flight Plan Page.
FLIGHT
MANAGEMENT
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.
HAZARD
AVOIDANCE
5) Turn the large FMS Knob to highlight the white header of the procedure to be deleted.
6) Press the CLR Key. The ‘Remove <procedure name> from flight plan?’ window is displayed.
7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
8) Press the FMS Knob to remove the flashing cursor.
AFCS
Or:
1) Press the FPL Key to display the Active Flight Plan Page.
ADDITIONAL
FEATURES
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.
APPENDICES
5) Press the MENU Key to display the Page Menu and turn the FMS Knob to highlight ‘Remove <procedure>’.
6) Press the ENT Key. The ‘Remove <procedure name> from flight plan?’ window is displayed.
7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
8) Press the FMS Knob to remove the flashing cursor.
217
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
CHANGING FLIGHT PLAN COMMENTS (NAMES)
The comment field (or name) of each flight plan can be changed to something that is useful for identification.
FLIGHT
INSTRUMENTS
Changing the active flight plan comment:
1) Press the FPL Key to display the Active Flight Plan Page.
2) Press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the comment field.
3) Use the FMS Knobs to edit the comment.
4) Press the ENT Key to accept the changes.
EIS
5) Press the FMS Knob to remove the flashing cursor.
Changing a stored flight plan comment:
AUDIO PANEL
& CNS
1) Press the FPL Key to display the Active Flight Plan Page.
2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited.
FLIGHT
MANAGEMENT
4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored
Flight Plan Page is displayed.
5) Turn the large FMS Knob to highlight the comment field.
6) Use the FMS Knobs to edit the comment.
HAZARD
AVOIDANCE
7) Press the ENT Key to accept the changes.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
8) Press the FMS Knob to remove the flashing cursor.
218
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
ALONG TRACK OFFSETS
FLIGHT
INSTRUMENTS
A waypoint having an “along track offset” distance from an existing waypoint can be entered into a flight plan.
Along track offset waypoints lie along the path of the existing flight plan, and can be used to make the system
reach a specified altitude before or after reaching the specified flight plan waypoint. Offset distances can be
entered from 1 to 99 nm in increments of 1 nm. Entering a negative offset distance results in an along track
offset waypoint inserted before the selected waypoint, whereas entering a positive offset distance results in an
along track offset waypoint inserted after the selected waypoint. Multiple offset waypoints are allowed.
EIS
A waypoint must be adjacent to its parent waypoint in the flight plan, so the system limits the along-track
distance to less than the length of the leg before or after the selected waypoint. If the selected waypoint is the
active waypoint, the distance is limited to less than the distance to go to the active waypoint. Assigning an along
track offset to a leg with indeterminate length is not permitted. An along track offset is not allowed at or after
the final approach fix of an approach.
AUDIO PANEL
& CNS
An along track offset distance cannot be modified once entered. If the along track offset distance must be
changed, the existing along track offset waypoint must be deleted and a new one created with the new offset
distance.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Along Track Offset
Waypoint and
Distance from Flight
Plan Waypoint
Along Track
Offset Waypoint
and Distance
AFCS
ADDITIONAL
FEATURES
Figure 5-78 Along Track Offset
Entering an along track offset distance:
APPENDICES
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the waypoint for the along track offset.
3) Select the ATK OFST Softkey (MFD only); or press the MENU Key, highlight ‘Create ATK Offset Waypoint’, and
press the ENT Key.
INDEX
4) Enter a positive or negative offset distance in the range of +/- 1 to 99 nm (limited by leg distances).
5) Press the ENT Key to create the offset waypoint.
6) Press the FMS Knob to remove the flashing cursor.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
219
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
PARALLEL TRACK
FLIGHT
INSTRUMENTS
The Parallel Track (PTK) feature allows creation of a parallel course offset of 1 to 50 nm left or right of the
current flight plan. When Parallel Track is activated, the course line drawn on the map pages shows the parallel
course, and waypoint names have a lower case “p” placed after the identifier.
Using direct-to, loading an approach, a holding pattern, or editing and activating the flight plan automatically
cancels Parallel Track. Parallel Track is also cancelled if a course change occurs greater than 120° or the parallel
tracks overlap as a result of the course change.
AUDIO PANEL
& CNS
EIS
NOTE: Vertical navigation is unavailable while the Parallel Track feature is active.
FLIGHT
MANAGEMENT
Active Flight Plan prior to
Parallel Track
HAZARD
AVOIDANCE
Selecting Parallel
Track
AFCS
Figure 5-79 Active Flight Plan Window - Selecting Parallel Track
Activating parallel track:
ADDITIONAL
FEATURES
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed
with the direction field highlighted.
APPENDICES
3) Turn the small FMS Knob to select ‘Left’ or ‘Right’ and press the ENT Key. The ‘DISTANCE’ field is highlighted.
4) Turn the small FMS Knob to enter a distance from 1-99 nm and press the ENT Key. ‘ACTIVATE PARALLEL
TRACK’ is highlighted.
INDEX
5) Press the ENT Key to activate parallel track. Press the FMS Knob or the CLR Key to cancel the parallel track
activation.
220
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Offset Direction
Offset Distance
FLIGHT
INSTRUMENTS
Activation Prompt
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-80 Parallel Track Window
HAZARD
AVOIDANCE
Parallel Track Waypoints
Original Track
AFCS
- TIFTO-p
- TOP-p
- ...
- LAA-p
- ...
Activating Parallel Track
affects the active flight
plan from the current
position on (will not affect
an approach
Parallel Track
ADDITIONAL
FEATURES
APPENDICES
Figure 5-81 Parallel Track Active
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
If the parallel track proposed by the offset direction and distance is not allowed by the system, the activation
prompt is displayed, but disabled. Parallel Track cannot be activated if a course is set using direct-to or if the
active leg is the first leg of the departure procedure. Attempting to activate parallel track with these conditions
results in the message ‘Parallel Track Unavailable Invalid Route Geometry’. If an approach leg is active the status
indicates that the system is unable to activate the parallel track with the message ‘Parallel Track Unavailable
221
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
Approach Leg Active’. If the offset direction and distance results in an unreasonable route geometry the status
indicates that the system is unable to activate the parallel track because of invalid geometry.
Subdued Prompt
(Unavailable)
Unavailable Status
AUDIO PANEL
& CNS
EIS
Invalid
Geometry
Approach
Active
FLIGHT
MANAGEMENT
Figure 5-82 Parallel Track Unavailable
HAZARD
AVOIDANCE
If the active leg is not a track between two fixes (TF) or a course to a fix (DF) leg, the status
indicates that the system is unable to activate the parallel track because parallel track is not available for the
active leg type.
Offset Direction &
Distance Subdued
(Unavailable)
AFCS
Cancel Prompt
ADDITIONAL
FEATURES
Active Status
Figure 5-83 Cancelling Parallel Track
APPENDICES
Cancelling parallel track:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed
with ‘CANCEL PARALLEL TRACK?’ highlighted.
INDEX
3) Press the ENT Key.
222
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
ACTIVATING A FLIGHT PLAN LEG
The G1000 allows selection of a highlighted leg as the “active leg” (the flight plan leg which is currently
used for navigation guidance).
FLIGHT
INSTRUMENTS
Activating a flight plan leg:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight
the destination waypoint for the desired leg.
EIS
3) Select the ACT LEG Softkey (MFD only); or press the MENU Key, highlight ‘Activate Leg’, and press the ENT Key.
A confirmation window is displayed with ‘ACTIVATE’ highlighted.
AUDIO PANEL
& CNS
4) Press the ENT Key to activate the flight plan leg. To cancel, press the CLR Key, or highlight ‘CANCEL’ and press
the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.
FLIGHT
MANAGEMENT
Current Active Leg
HAZARD
AVOIDANCE
Selected Destination
Waypoint
AFCS
Activate Leg Softkey
ADDITIONAL
FEATURES
Figure 5-84 Active Flight Plan Page - Selecting the Leg Destination Waypoint
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
223
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
EIS
New Active
Flight Plan Leg
AUDIO PANEL
& CNS
Confirmation Window
FLIGHT
MANAGEMENT
Figure 5-85 Active Flight Plan Page - New Active Leg
INVERTING A FLIGHT PLAN
Any flight plan may be inverted (reversed) for navigation back to the original departure point.
HAZARD
AVOIDANCE
Inverting the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
2) Press the MENU Key, highlight ‘Invert Flight Plan’, and press the ENT Key. An ‘Invert Active Flight Plan?’
confirmation window is displayed.
3) Select ‘OK’.
AFCS
4) Press the ENT Key to invert and activate the active flight plan. To cancel, press the CLR Key, or highlight
‘CANCEL’ and press the ENT Key.
ADDITIONAL
FEATURES
Inverting and activating a stored flight plan:
1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan.
APPENDICES
3) Select the INVERT Softkey; or press the MENU Key, highlight ‘Invert & activate FPL?’, and press the ENT Key.
The ‘Invert and activate stored flight plan?’ window is displayed.
INDEX
4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and
press the ENT Key.
224
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FLIGHT PLAN VIEWS
FLIGHT
INSTRUMENTS
Information about flight plans can be viewed in more than one way. The active flight plan can be configured
to show cumulative distance over the length of the flight plan or the distance for each leg of the flight plan;
and the active flight plan can be viewed in a narrow or wide view. In the wide view, additional information is
displayed: Fuel Remaining (FUEL REM), Estimated Time Enroute (ETE), Estimated Time of Arrival (ETA), and
Bearing to the waypoint (BRG).
Switching between leg-to-leg waypoint distance and cumulative waypoint distance:
1) Press the FPL Key on the MFD to display the Active Flight Plan Page.
EIS
2) Select the VIEW Softkey to display the CUM and LEG-LEG Softkeys.
3) Select the CUM Softkey to view cumulative waypoint distance, or select the LEG-LEG Softkey to view leg-to-leg
waypoint distance.
AUDIO PANEL
& CNS
4) Select the BACK Softkey to return to the top level active flight plan softkeys.
Active Flight Plan Leg to Leg Distance
Active Flight Plan Cumulative Distance
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey
Figure 5-86 Active Flight Plan - Leg to Leg vs. Cumulative Distance
Switching between wide and narrow view:
APPENDICES
1) Press the FPL Key on the MFD to display the Active Flight Plan Page.
2) Select the VIEW Softkey to display the WIDE and NARROW Softkeys.
3) Select the WIDE Softkey to display the wide view, or select the NARROW Softkey to display the narrow view.
4) Select the BACK Softkey to return to the top level active flight plan softkeys.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
225
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Active Flight Plan Cumulative Distance
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Active Flight Plan Leg to Leg Distance
FLIGHT
MANAGEMENT
WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey
Figure 5-87 Active Flight Plan - Wide vs. Narrow View
COLLAPSING AIRWAYS
HAZARD
AVOIDANCE
The G1000 allows airways on the active flight plan to be collapsed or expanded from the Active Flight Plan
Page/Window. When airways have been collapsed, it is indicated on the airway heading.
When airways are collapsed, leg-to-leg computed values such as DIS or ETE shown for the exit waypoint
reflect the total of all the legs on the airway that have been hidden in the collapsed display. The DTK value is
inhibited because it is not usable in this context.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
The Active Flight Plan Page always keeps the following three waypoints visible: “From” waypoint, “To”
waypoint, and the “Next” waypoint. To prevent one or more of these waypoints from being hidden in a collapsed
airway segment, the airway segment that contains either the “To” or the “Next” waypoint is automatically
expanded. When an airway is loaded, airways are automatically expanded to facilitate flight plan review.
226
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Q3.FEPOT Airway
FLIGHT
INSTRUMENTS
Collapsed View
Expanded View
EIS
Figure 5-88 Expanded/Collapsed Airways
AUDIO PANEL
& CNS
Collapsing/expanding the airways in the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
FLIGHT
MANAGEMENT
2) Press the MENU Key, highlight ‘Collapse Airways’ or ‘Expand Airways’, and press the ENT Key. The airways are
collapsed/expanded.
CLOSEST POINT OF FPL
HAZARD
AVOIDANCE
‘Closest Point of FPL’ calculates the bearing and closest distance at which a flight plan passes a reference
waypoint, and creates a new user waypoint along the flight plan at the location closest to a chosen reference
waypoint.
Determining the closest point along the active flight plan to a selected waypoint:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
AFCS
2) Press the MENU Key, highlight ‘Closest Point Of FPL’’, and press the ENT Key. A window appears with the
reference waypoint field highlighted.
ADDITIONAL
FEATURES
3) Enter the identifier of the reference waypoint and press the ENT Key. The G1000 displays the bearing (BRG) and
distance (DIS) to the closest point along the flight plan to the selected reference waypoint and creates a user
waypoint at this location. The name for the new user waypoint is derived from the identifier of the reference
waypoint.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
227
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
5.7 VERTICAL NAVIGATION
FLIGHT
INSTRUMENTS
NOTE: The G1000 supports vertical navigation for all lateral leg types except for CA, CI, FA, FM, HA, HM, PI,
VA, VD, VI, VR, and VM. Vertical constraints are not retained in stored flight plans.
EIS
The G1000 system Vertical Navigation (VNV) feature provides vertical profile guidance during the enroute
and teminal phases of flight. Guidance based on specified altitudes at waypoints in the active flight plan or to a
direct-to waypoint is provided. It includes vertical path guidance to a descending path, which is provided as a
linear deviation from the desired path. The desired path is defined by a line joining two waypoints with specified
altitudes or as a vertical angle from a specified waypoint/altitude. The vertical waypoints are integrated into the
active flight plan. Both manual and autopilot-coupled guidance are supported.
Current Vertical Navigation Profile
Current Vertical Navigation Profile
Enabled (valid data)
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Disabled (fields dashed)
ENBL VNV Softkey
CNCL VNV Softkey
ADDITIONAL
FEATURES
Figure 5-89 Enabling/Disabling Vertical Navigation
Enabling VNV guidance:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
APPENDICES
2) Select the ENBL VNV Softkey; or press the MENU Key, highlight ‘Enable VNV’, and press the ENT Key. Vertical
navigation is enabled, and vertical guidance begins with the waypoint shown in the CURRENT VNV PROFILE box
(defaults first waypoint in the active flight plan with an altitude enabled for vertical navigation (e.g., HABUK)).
Disabling VNV guidance:
INDEX
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Select the CNCL VNV Softkey; or press the MENU Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical
navigation is disabled.
228
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
Canceling vertical navigation results in vertical deviation (V DEV), vertical speed required (VS REQ), and time
to top of descent/bottom of descent (TIME TO TOD/BOD) going invalid. The Vertical Deviation Indicator (VDI)
and Required Vertical Speed Indicator (RVSI) on the PFD are removed, and the V DEV, VS REQ, and TIME TO
TOD items displayed in the CURRENT VNV PROFILE box are dashed. VNV remains disabled until manually
enabled. Vertical guidance in reversionary mode can only be enabled for a direct-to waypoint.
AUDIO PANEL
& CNS
Current Vertical Navigation Profile
EIS
The G1000 allows a vertical navigation direct-to to any waypoint in the active flight plan with an altitude
constraint “designated” for vertical guidance. Selecting the VNV Direct-to Softkey on the Active Flight Plan Page
allows the flight plan to be flown, while vertical guidance based on the altitude constraint at the VNV direct-to
waypoint is provided. The altitude change begins immediately and is spread along the flight plan from current
position to the vertical direct-to waypoint, not just along the leg for the direct-to waypoint. A direct-to with
altitude constraint activated by pressing the Direct-to Key also provides vertical guidance, but would bypass
flight plan waypoints between the current position in the flight plan and the direct-to waypoint. A top of descent
(TOD) point is computed based on the default flight path angle; descent begins once the TOD is reached.
Current Vertical Navigation Profile
Prior to VNV Direct-to
After VNV Direct-to
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
VNV Direct-To Softkey
VNV PROF Softkey
ADDITIONAL
FEATURES
Figure 5-90 Vertical Navigation Direct-To
Activating a vertical navigation direct-to:
APPENDICES
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired waypoint.
NOTE: The selected waypoint must have a designated altitude constraint (light blue number) to be used. If
not, the first waypoint in the flight plan with a designated altitude constraint is selected.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
3) Select the VNV Direct-To Softkey; or press the MENU Key, highlight ‘VNV Direct-To’, and press the ENT Key.
An ‘Activate vertical Direct-to to: NNNNNFT at XXXXXX?’ confirmation window is displayed.
229
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
4) Press the ENT Key. Vertical guidance begins to the altitude constraint for the selected waypoint.
5) Press the FMS Knob to remove the flashing cursor.
FLIGHT
INSTRUMENTS
The vertical navigation profile can be modified by directly entering a vertical speed target (VS TGT) and/or flight
path angle (FPA) in the CURRENT VNV PROFILE box.
Modifying the VS TGT and FPA:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
EIS
2) Select the VNV PROF Softkey; or press the MENU Key, highlight ‘Select VNV Profile Window’, and press the
ENT Key. The cursor is now located in the CURRENT VNV PROFILE box.
3) Turn the FMS Knobs as needed to edit the values.
AUDIO PANEL
& CNS
4) Press the FMS Knob to remove the flashing cursor.
ALTITUDE CONSTRAINTS
FLIGHT
MANAGEMENT
The G1000 system can use altitude constraints associated with lateral waypoints to give guidance for vertical
navigation. These altitudes are, depending on the specific instance, manually entered or retrieved from the
published altitudes in the navigation database. The navigation database only contains altitudes for procedures
that call for “Cross at” altitudes. If the procedure states “Expect to cross at,” then the altitude is not in the
database. In this case the altitude may be entered manually.
Displayed Text
Examples
HAZARD
AVOIDANCE
Cross AT
or ABOVE
5,000 ft
Large White Text
Large Light Blue Text
Cross AT
2,300 ft
AFCS
Small Light Blue Text
Cross AT
or BELOW
3,000 ft
Small Light Blue
Subdued Text
ADDITIONAL
FEATURES
Altitude Constraint
Examples
Small White Text with
Altitude Restriction Bar
INDEX
APPENDICES
Figure 5-91 Waypoint Altitude Constraints
230
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
Light Blue Text
Light Blue Subdued Text
The system cannot use this
altitude in determining vertical
speed and deviation guidance
because of an invalid constraint
condition.
Small
Text
Altitude is designated for use in giving
vertical speed and deviation guidance.
Altitude has been retrieved from the
navigation database or has been entered
manually and matches a published
altitude in the navigation database.
The system cannot use this
altitude in determining vertical
speed and deviation guidance
because of an invalid constraint
condition.
EIS
Altitude has been entered manually.
Altitude is designated for use in giving
vertical speed and deviation guidance.
Altitude does not match the published
altitude in navigation database or no
published altitude exists.
FLIGHT
INSTRUMENTS
Large Altitude calculated by the system
Text estimating the altitude of the aircraft as
it passes over the navigation point. This
altitude is provided as a reference and is
not designated to be used in determining
vertical speed and deviation guidance.
Altitude is not designated to be used in
determining vertical speed and deviation
guidance. Altitude has been retrieved
from the navigation database and is
provided as a reference.
SYSTEM
OVERVIEW
White Text
AUDIO PANEL
& CNS
Table 5-8 Altitude Constraint Size and Color Coding
FLIGHT
MANAGEMENT
Altitudes associated with arrival and approach procedures are “auto-designated”. This means the system
automatically uses the altitudes loaded with the arrival or approach for giving vertical speed and deviation
guidance. Note that these altitudes are displayed as blue text up to, but not including, the FAF. The FAF is
always a “reference only” altitude and cannot be designated, unless the selected approach does not provide
vertical guidance. In this case, the FAF altitude can be designated.
HAZARD
AVOIDANCE
Altitudes that have been designated for use in vertical guidance can be “un-designated” using the CLR Key.
The altitude is now displayed only as a reference. It is not used to give vertical guidance. Other displayed
altitudes may change due to re-calculations or be rendered invalid as a result of manually changing an altitude
to a non-designated altitude.
Designating a waypoint altitude to be used for vertical guidance:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
AFCS
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude.
3) Turn the small FMS Knob to enter editing mode.
4) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance.
ADDITIONAL
FEATURES
Designating a procedure waypoint altitude to be used for vertical guidance:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude.
APPENDICES
3) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
Altitude constraints are displayed and entered in feet mean sea level (MSL) values to the nearest hundred. An
altitude constraint in feet above ground level (AGL) format is supported for airports. When a database altitude
restriction is displayed, the G1000 allows entry of a different altitude when creating a waypoint, effectively
overriding the database restriction (only before the FAF). When a database altitude restriction of type “AT or
ABOVE” or “AT or BELOW” is activated, the system uses the “AT” portion of the restriction to define the vertical
profile.
231
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
An altitude constraint is invalid if:
• Meeting the constraint requires the aircraft to climb
FLIGHT
INSTRUMENTS
• Meeting the constraint requires the maximum flight path angle or maximum vertical speed to be exceeded
• The altitude constraint results in a TOD behind the aircraft present position
• The constraint is within a leg type for which altitude constraints are not supported
• The altitude constraint is added to the FAF of an approach that provides vertical guidance (i.e., ILS or GPS
SBAS approach)
EIS
• The altitude constraint is added to a waypoint past the FAF.
Entering/modifiying an altitude constraint:
AUDIO PANEL
& CNS
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.
FLIGHT
MANAGEMENT
3) Enter an altitude constraint value using the FMS Knobs. To enter altitudes as a flight level, turn the small
FMS Knob counter-clockwise past zero or clockwise past 9 on the first character, and the system automatically
changes to show units of Flight Level. Turn the large FMS Knob clockwise to highlight the first zero and enter
the three digit flight level.
4) Press the ENT Key to accept the altitude constraint; if the selected waypoint is an airport, an additional choice
is displayed. Turn the small FMS Knob to choose ‘MSL’ or ‘AGL’, and press the ENT Key to accept the altitude.
HAZARD
AVOIDANCE
Altitude constraints can be modified or deleted after having been added to the flight plan. In the event
an altitude constraint is deleted and the navigation database contains an altitude restriction for the lateral
waypoint, the G1000 displays the altitude restriction from the database provided no predicted altitude
can be provided. The G1000 also provides a way to reinstate a published altitude constraint that has been
edited.
AFCS
Deleting an altitude constraint provided by the navigation database:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.
ADDITIONAL
FEATURES
3) Press the CLR Key. A ‘Remove VNV altitude constraint?’ confirmation window is displayed.
4) Select ‘OK’ and press the ENT Key.
Deleting an altitude constraint that has been manually entered:
APPENDICES
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.
3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is
displayed.
INDEX
4) Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is deleted (it is replaced by a system
calculated altitude, if available).
232
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Reverting a manually entered altitude constraint back to the navigation database value:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.
FLIGHT
INSTRUMENTS
3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is
displayed.
4) Select ‘REVERT’ and press the ENT Key. The altitude is changed to the navigation database value.
5) Press the FMS Knob to remove the flashing cursor.
EIS
Modifying a system calculated altitude constraint:
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint.
AUDIO PANEL
& CNS
3) Press the CLR Key. An ‘Edit or Revert to published VNV altitude of nnnnnFT?’ confirmation window is
displayed.
4) Select ‘EDIT’ and press the ENT Key.
FLIGHT
MANAGEMENT
5) Edit the value using the FMS Knobs, and press the ENT Key.
6) Press the FMS Knob to remove the flashing cursor.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
233
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
5.8 PROCEDURES
FLIGHT
INSTRUMENTS
The G1000 can access the whole range of instrument procedures available. Departures (DPs), arrivals (STARs),
and non-precision and precision approaches (APPRs) are stored within the database and can be loaded using the
Procedures (PROC) Key.
AUDIO PANEL
& CNS
EIS
The selected procedure for the departure or arrival airport is added to the active flight plan. No waypoints are
required to be in the active flight plan to load procedures; however, if the departure and arrival airport are already
loaded, the procedure loading window defaults to the appropriate airport, saving some time selecting the correct
airport on the Procedure Loading Page. Whenever an approach is selected, the choice to either “load” or “activate”
is given. “Loading” adds the approach to the end of the flight plan without immediately using it for navigation
guidance. This allows continued navigation via the intermediate waypoints in the original flight plan, but keeps
the procedure available on the Active Flight Plan Page for quick activation when needed. “Activating” also adds
the procedure to the end of the flight plan but immediately begins to provide guidance to the first waypoint in
the approach.
DEPARTURES
FLIGHT
MANAGEMENT
A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can be
loaded at a time in a flight plan. If a departure is loaded when another departure is already in the active flight
plan, the new departure replaces the previous departure. The route is defined by selection of a departure, the
transition waypoints, and a runway.
HAZARD
AVOIDANCE
LOADING A DEPARTURE INTO THE ACTIVE FLIGHT PLAN
Loading a departure into the active flight plan using the PROC Key:
1) Press the PROC Key. The Procedures Window is displayed.
2) Highlight ‘SELECT DEPARTURE’.
AFCS
3) Press the ENT Key. The Departure Loading Page is displayed.
4) Use the FMS Knob to select an airport and press the ENT Key.
5) Select a departure from the list and press the ENT Key.
ADDITIONAL
FEATURES
6) Select a runway (if required) and press the ENT Key.
7) Select a transition (if required) and press the ENT Key. ‘LOAD?’ is highlighted.
INDEX
APPENDICES
8) Press the ENT Key to load the departure procedure.
234
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Departure Airport
Available Procedure Actions
FLIGHT
INSTRUMENTS
EIS
Departure Preview
AUDIO PANEL
& CNS
Loaded Procedures
Departure Choices
Figure 5-92 Departure Selection
FLIGHT
MANAGEMENT
Selected Departure
Loaded Departure
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Procedure Loading Page Selection Softkeys
Figure 5-93 Departure Loading
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
235
SYSTEM
OVERVIEW
Viewing available departures at an airport:
FLIGHT
INSTRUMENTS
2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and
press the ENT Key.
EIS
FLIGHT MANAGEMENT
5) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor
moves to the Transition box (only if there are available transitions). The departure is previewed on the map.
1) From the Airport Information Page (first page in the WPT group), select the DP Softkey. The Departure Information
Page is displayed, defaulting to the airport displayed on the Airport information Page.
3) Turn the large FMS Knob to highlight the Departure. The departure is previewed on the map.
4) Turn the small FMS Knob to view the available departures. Press the ENT Key to select the departure. The cursor
moves to the Runway box. The departure is previewed on the map.
AUDIO PANEL
& CNS
6) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor
moves to the Sequence box. The departure is previewed on the map.
7) Select the INFO-x Softkey to return to the Airport Information Page.
REMOVING A DEPARTURE FROM THE ACTIVE FLIGHT PLAN
FLIGHT
MANAGEMENT
When plans change while flying IFR, departures can be easily removed from the Active Flight Plan.
Removing a departure procedure from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
HAZARD
AVOIDANCE
2) Press the MENU Key, and highlight ‘Remove Departure’.
3) Press the ENT Key. A confirmation window is displayed listing the departure procedure.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT
Key.
AFCS
Or:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD)
2) Press the FMS Knob, and turn to highlight the departure header in the active flight plan.
ADDITIONAL
FEATURES
3) Press the CLR Key. A confirmation window is displayed listing the departure procedure.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT
Key.
INDEX
APPENDICES
5) Press the FMS Knob to remove the flashing cursor.
236
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
ARRIVALS
FLIGHT
INSTRUMENTS
A Standard Terminal Arrival (STAR) can be loaded at any airport that has one available. Only one arrival
can be loaded at a time in a flight plan. If an arrival is loaded when another arrival is already in the active
flight plan, the new arrival replaces the previous arrival. The route is defined by selection of an arrival, the
transition waypoints, and a runway.
LOADING AN ARRIVAL INTO THE ACTIVE FLIGHT PLAN
Loading an arrival into the active flight plan using the PROC Key:
EIS
1) Press the PROC Key. The Procedures Window is displayed.
2) Highlight ‘SELECT ARRIVAL’.
3) Press the ENT Key. The Arrival Loading Page is displayed.
AUDIO PANEL
& CNS
4) Use the FMS Knob to select an airport and press the ENT Key.
5) Select an arrival from the list and press the ENT Key.
6) Select a transition (if required) and press the ENT Key.
FLIGHT
MANAGEMENT
7) Select a runway (if required) and press the ENT Key. ‘LOAD?’ is highlighted.
8) Press the ENT Key to load the arrival procedure.
Destination Airport
Available Procedure Actions
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Arrival Preview
Arrival Choices
APPENDICES
Loaded Procedures
Figure 5-94 Arrival Selection
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
237
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Loaded Arrival
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Selected Arrival
Procedure Loading Page Selection Softkeys
FLIGHT
MANAGEMENT
Figure 5-95 Arrival Loading
Viewing available arrivals at an airport:
1) From the Airport Information Page (first page in the WPT group), select the STAR Softkey. The Arrival Information
Page is displayed, defaulting to the airport displayed on the Airport Information Page.
HAZARD
AVOIDANCE
2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and
press the ENT Key.
3) Turn the large FMS Knob to highlight the Arrival. The arrival is previewed on the map.
AFCS
4) Turn the small FMS Knob to view the available arrivals. Press the ENT Key to select the arrival. The cursor moves
to the Transition box. The arrival is previewed on the map.
5) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor
moves to the Runway box. The arrival is previewed on the map.
ADDITIONAL
FEATURES
6) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor
moves to the Sequence box. The arrival is previewed on the map.
7) Select the INFO-x Softkey to return to the Airport Information Page.
REMOVING AN ARRIVAL FROM THE ACTIVE FLIGHT PLAN
APPENDICES
When plans change while flying IFR, arrivals can be easily removed from the Active Flight Plan.
Removing an arrival from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
INDEX
2) Press the MENU Key, and highlight ‘Remove Arrival’.
238
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
3) Press the ENT Key. A confirmation window is displayed listing the arrival procedure.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT
Key.
FLIGHT
INSTRUMENTS
Or:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob, and turn to highlight the arrival header in the active flight plan.
3) Press the CLR Key. A confirmation window is displayed listing the arrival procedure.
EIS
4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT
Key.
5) Press the FMS Knob to remove the flashing cursor.
AUDIO PANEL
& CNS
APPROACHES
NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some published approach procedures
for the desired airport may not be displayed in the list of available approaches.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
An Approach Procedure (APPR) can be loaded at any airport that has one available, and provides guidance
for non-precision and precision approaches to airports with published instrument approach procedures.
Only one approach can be loaded at a time in a flight plan. If an approach is loaded when another approach
is already in the active flight plan, the new approach replaces the previous approach. The route is defined by
selection of an approach and the transition waypoints.
AFCS
Whenever an approach is selected, the choice to either “load” or “activate” is given. “Loading” adds the
approach to the end of the flight plan without immediately using it for navigation guidance. This allows
continued navigation via the intermediate waypoints in the original flight plan, but keeps the procedure
available on the Active Flight Plan Page for quick activation when needed. “Activating” also adds the
procedure to the end of the flight plan but immediately begins to provide guidance to the first waypoint in
the approach.
ADDITIONAL
FEATURES
When selecting an approach, a “GPS” designation to the right of the procedure name indicates the procedure
can be flown using the GPS receiver. Some procedures do not have this designation, meaning the GPS
receiver can be used for supplemental navigation guidance only. If the GPS receiver cannot be used for
primary guidance, the appropriate navigation receiver must be used for the selected approach (e.g., VOR or
ILS). The final course segment of ILS approaches, for example, must be flown by tuning the NAV receiver to
the proper frequency and selecting that NAV receiver on the CDI.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
239
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
INSTRUMENTS
The G1000 SBAS GPS allows for flying LNAV, LNAV/VNAV, and LPV approaches according to the published
chart. LNAV+V is a standard LNAV approach with advisory vertical guidance provided for assistance in
maintaining a constant vertical glidepath similar to an ILS glideslope on approach. This guidance is displayed
on the G1000 PFD in the same location as the ILS glideslope using a magenta diamond. In all cases where
LNAV+V is indicated by the system during an approach, LNAV minima are used. The active approach type
is annunciated on the HSI as shown in the following table:
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
HSI Annunciation
Description
LNAV
GPS approach using published LNAV
minima
LNAV+V
GPS approach using published LNAV
minima. Advisory vertical guidance is
provided
L/VNAV
GPS approach using published LNAV/
(available only if VNAV minima
SBAS equipped)
LPV
GPS approach using published LPV
(available only if minima
SBAS equipped
Example on HSI
Approach Type
- LNAV
- LNAV+V
- L/VNAV
- LPV
Table 5-9 Approach Types
LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN
HAZARD
AVOIDANCE
Loading an approach into the active flight plan using the PROC Key:
1) Press the PROC Key. The Procedures Window is displayed.
2) Highlight ‘SELECT APPROACH’, and press the ENT Key. The Approach Loading Page is displayed.
AFCS
3) Use the FMS Knob to select an airport and press the ENT Key.
4) Select an approach from the list and press the ENT Key.
5) Select a transition (if required) and press the ENT Key.
ADDITIONAL
FEATURES
6) Minimums
a) To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’ or ‘RAD ALT’ (optional), and press the ENT Key.
Turn the small FMS Knob to select the altitude, and press the ENT Key.
Or:
APPENDICES
b) To skip setting minimums, press the ENT Key.
7) Press the ENT Key with ‘LOAD?’ highlighted to load the approach procedure; or turn the large FMS Knob to
highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure.
NOTE: When GPS is not approved for the selected final approach course, the message ‘NOT APPROVED
INDEX
FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to a NAV
receiver to fly the final course of the approach.
240
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Destination Airport
Available Procedure Actions
FLIGHT
INSTRUMENTS
EIS
Approach Preview
AUDIO PANEL
& CNS
Loaded Procedures
Approach Choices
Figure 5-96 Approach Selection
FLIGHT
MANAGEMENT
Selected Approach
Loaded Approach
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Procedure Loading Page Selection Softkeys
Figure 5-97 Approach Loading
APPENDICES
Viewing available approaches at an airport:
1) From the Airport Information Page (first page in the WPT group), select the APR Softkey. The Approach
Information Page is displayed, defaulting to the airport displayed on the Airport information Page.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and
press the ENT Key.
241
SYSTEM
OVERVIEW
3) Press the FMS Knob, then turn the large FMS Knob to highlight the Approach. The approach is previewed on
the map.
FLIGHT
INSTRUMENTS
FLIGHT MANAGEMENT
5) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor
moves to the Minimums box. The approach is previewed on the map.
4) Turn the small FMS Knob to view the available approaches. Press the ENT Key to select the approach. The
cursor moves to the Transition box. The approach is previewed on the map.
6) Turn the small FMS Knob to select BARO (or optional RAD ALT) minimums on or off. Press the ENT Key.
EIS
a) When minimums are selected on, the cursor moves to the minimum altitude field . Use the small FMS Knob to
select the altitude. Press the ENT Key. The cursor moves to the Sequence box. The approach is previewed on
the map.
Or:
AUDIO PANEL
& CNS
b) When minimums are selected off, the cursor moves to the Sequence box. The approach is previewed on the
map.
7) Press the INFO-x Softkey to return to the Airport Information Page.
FLIGHT
MANAGEMENT
Loading an approach into the active flight plan from the Nearest Airport Page:
1) Select the Nearest Airports Page.
2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired nearest airport. The airport is
previewed on the map.
HAZARD
AVOIDANCE
3) Select the APR Softkey; or press the MENU Key, highlight ‘Select Approach Window’, and press the ENT Key.
4) Turn the FMS Knob to highlight the desired approach.
5) Select the LD APR Softkey; or press the MENU Key, highlight ‘Load Approach’, and press the ENT Key. The
Approach Loading Page is displayed with the transitions field highlighted.
AFCS
6) Turn the FMS Knob to highlight the desired transition, and press the ENT Key.
7) Minimums
ADDITIONAL
FEATURES
a) To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’ or ‘RAD ALT’ (optional), and press the ENT Key.
Turn the small FMS Knob to select the altitude, and press the ENT Key.
Or:
b) To skip setting minimums, press the ENT Key.
INDEX
APPENDICES
8) Press the ENT Key with ‘LOAD?’ highlighted to load the arrival procedure; or turn the large FMS Knob to
highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure. The G1000 continues
navigating the current flight plan until the approach is activated. When GPS is not approved for the selected
final approach course, the message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to the
approach, but the HSI must to be switched to a NAV receiver to fly the final course of the approach.
242
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
ACTIVATING AN APPROACH
A previously loaded approach can be activated from the Procedures Window.
FLIGHT
INSTRUMENTS
Activating a previously loaded approach:
1) Press the PROC Key. The Procedures Window is displayed with ‘Activate Approach’ highlighted.
2) Press the ENT Key to activate the approach.
EIS
In many cases, it may be easiest to “load” the full approach while still some distance away, enroute to the
destination airport. Later, if vectored to final, use the steps above to select ‘Activate Vector-To-Final’ — which
makes the inbound course to the FAF waypoint active.
Activating a previously loaded approach with vectors to final:
1) Press the PROC Key to display the Procedures Window.
AUDIO PANEL
& CNS
2) Highlight ‘ACTIVATE VECTOR-TO-FINAL’ and press the ENT Key.
Loading and activating an approach using the MENU Key:
FLIGHT
MANAGEMENT
1) From the Approach Loading Page, press the MENU Key. The page menu is displayed with ‘Load & Activate
Approach’ highlighted.
2) Press the ENT Key. When GPS is not approved for the selected final approach course, the message ‘NOT
APPROVED FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to
a NAV receiver to fly the final course of the approach.
HAZARD
AVOIDANCE
REMOVING AN APPROACH FROM THE ACTIVE FLIGHT PLAN
When plans change while flying IFR, approaches can be easily removed from the Active Flight Plan.
Removing an approach from the active flight plan:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
AFCS
2) Press the MENU Key, and highlight ‘Remove Approach’.
3) Press the ENT Key. A confirmation window is displayed listing the approach procedure.
ADDITIONAL
FEATURES
4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight ‘CANCEL’ and press the ENT Key.
Or:
1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD).
2) Press the FMS Knob, and turn to highlight the approach header in the active flight plan.
APPENDICES
3) Press the CLR Key. A confirmation window is displayed listing the approach procedure.
4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight ‘CANCEL’ and press the ENT Key.
5) Press the FMS Knob to remove the flashing cursor.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
243
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
MISSED APPROACH
Activating a missed approach in the active flight plan:
FLIGHT
INSTRUMENTS
1) Press the PROC Key.
2) Turn the FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3) Press the ENT Key. The aircraft automatically sequences to the MAHP.
Or:
EIS
Press the Go-Around Button.
COURSE TO ALTITUDE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not
part of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along
the runway centerline until the required altitude required to safely make the first turn toward the MAHP
is exceeded. In this case, if the aircraft altitude is below the specified altitude (6,368 feet) after crossing
the MAP, a direct-to is established to provide a course on runway heading until an altitude of 6,368 feet
reached. After reaching 6,368 feet, a direct-to is established to the published MAHP (in this case MOGAL).
If the aircraft altitude is above the specified altitude after crossing the MAP, a direct-to is established to the
published fix (MOGAL) to begin the missed approach procedure. The altitude constraint value defaults to
400 feet AGL when there is no Course to Altitude defined in the published procedure.
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
In some missed approach procedures this Course to Altitude leg may be part of the published procedure.
For example, the procedure dictates a climb to 5,500 feet, then turn left and proceed to the Missed Approach
Hold Point (MAHP). In this case, The altitude would be labeled appear in the list of waypoints as ‘5500ft’.
Again, if the aircraft altitude is lower than the prescribed altitude, a direct-to is established on a Course to
Altitude leg when the missed approach procedure is activated.
APPENDICES
Course to Altitude Leg
INDEX
Figure 5-98 Course to Altitude
244
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
5.9 TRIP PLANNING
FLIGHT
INSTRUMENTS
The G1000 allows the pilot to view trip planning information, fuel information, and other information for
a specified flight plan or flight plan leg based on automatic data, or based on manually entered data. Weight
planning is also available, based on fuel sensor data and the active flight plan (to estimate remaining fuel).
TRIP PLANNING
All of the input of data needed for calculation and viewing of the statistics is done on the Trip Planning Page
located in the AUX Page Group.
EIS
Selected Flight Plan Segment
- FPL Number/Cumulative Legs (CUM or REM) or Leg Number (NN)
- Waypoints Defining Selected Flight Plan/Flight Plan Leg
AUDIO PANEL
& CNS
Trip Planning Page Mode
Preview of Selected
Flight Plan/
Flight Plan Leg
- Automatic/Manual
Trip Input Data (sensor/pilot)
Trip Statistics
HAZARD
AVOIDANCE
Desired Track Distance Est. Time Enroute Est. Time of Arrival Enroute Safe Altitude Sunrise Time (local) Sunset Time (local) -
FLIGHT
MANAGEMENT
- Departure Time (local)
- Ground Speed
- Fuel Flow
- Fuel On Board Aircraft
- Calibrated Airspeed
- Indicated Altitude
- Barometric Pressure
- Total Air Temperature
Other Statistics
- Density Altitude
- True Airspeed (TAS)
Fuel Statistics
Efficiency Total Endurance Remaining Fuel Remaining Endurance Fuel Required Total Range -
AFCS
Softkeys
- Automatic/Manual Page Mode
- Flight Plan/Waypoint Mode
Figure 5-99 Trip Planning Page
ADDITIONAL
FEATURES
The trip planning inputs are based on sensor inputs (automatic page mode) or on pilot inputs (manual page
mode). Some additional explanation of the sources for some of the inputs is as follows:
APPENDICES
• Departure time (DEP TIME) - This defaults to the current time in automatic page mode. The computations
are from the aircraft present position, so the aircraft is always just departing.
• Calibrated airspeed (CALIBRATED AS) - The primary source is from the air data system, and the secondary
source of information is GPS ground speed.
• Indicated altitude (IND ALTITUDE) - The primary source is the barometric altitude, and the secondary source
of information is GPS altitude.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
245
SYSTEM
OVERVIEW
TRIP STATISTICS
FLIGHT
INSTRUMENTS
FLIGHT MANAGEMENT
In flight plan mode (FPL) with a stored flight plan selected (NN), and the entire flight plan (CUM) selected,
the waypoints are the starting and ending waypoints of the selected flight plan.
The trip statistics are calculated based on the selected starting and ending waypoints and the trip planning
inputs.
In flight plan mode (FPL) with a stored flight plan selected (NN), and a specific leg (NN) selected, the
waypoints are the endpoints of the selected leg.
EIS
In flight plan mode (FPL) with the active flight plan selected (00), and the remaining flight plan (REM)
selected, the ‘from’ waypoint is the present position of the aircraft and the ‘to’ waypoint is the endpoint of the
active flight plan.
AUDIO PANEL
& CNS
In flight plan mode (FPL) with the active flight plan selected (00), and a specific leg (NN) selected, the
‘from’ waypoint is the current aircraft position and the ‘to’ waypoint is the endpoint of the selected leg.
In waypoint (WPTS) mode these are manually selected waypoints (if there is an active flight plan, these
default to the endpoints of the active leg).
FLIGHT
MANAGEMENT
Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has already
been flown.
• Desired Track (DTK) - DTK is shown as nnn° and is the desired track between the selected waypoints. It is dashed unless only a single leg is selected.
• Distance (DIS) - The distance is shown in tenths of units up to 99.9, and in whole units up to 9999. HAZARD
AVOIDANCE
• Estimated time enroute (ETE) - ETE is shown as hours:minutes until less than an hour, then it is shown
as minutes:seconds.
• Estimated time of arrival (ETA) - ETA is shown as hours:minutes and is the local time at the
destination.
AFCS
- If a flight plan other than the active flight plan is selected it shows the ETA by adding to the departure
time all of the ETEs of the legs up to the selected leg. If the entire flight plan is selected, then the ETA
is calculated as if the last leg of the flight plan was selected.
ADDITIONAL
FEATURES
- If in waypoint mode then the ETA is the ETE added to the departure time.
- If the active flight plan is selected the ETA reflects the current position of the aircraft and the current
leg being flown. The ETA is calculated by adding to the current time the ETEs of the current leg up to
and including the selected leg. If the entire flight plan is selected, then the ETA is calculated as if the
last leg of the flight plan was selected.
APPENDICES
• Enroute safe altitude (ESA) - The ESA is shown as nnnnnFT
INDEX
• Destination sunrise and sunset times (SUNRISE, SUNSET) - These times are shown as hours:minutes
and are the local time at the destination.
246
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FUEL STATISTICS
FLIGHT
INSTRUMENTS
The fuel statistics are calculated based on the selected starting and ending waypoints and the trip planning
inputs. Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has
already been flown.
• Fuel efficiency (EFFICIENCY) - This value is calculated by dividing the current ground speed by the
current fuel flow.
• Time of fuel endurance (TOTAL ENDUR) - This time is shown as hours:minutes. This value is obtained
by dividing the amount of fuel on board by the current fuel flow.
EIS
• Fuel on board upon reaching end of selected leg (REM FUEL) - This value is calculated by taking the
amount of fuel onboard and subtracting the fuel required to reach the end of the selected leg. AUDIO PANEL
& CNS
• Fuel endurance remaining at end of selected leg (REM ENDUR) - This value is calculated by taking the time
of fuel endurance and subtracting the estimated time enroute to the end of the selected leg.
• Fuel required for trip (FUEL REQ) - This value is calculated by multiplying the time to go by the fuel
flow.
FLIGHT
MANAGEMENT
• Total range at entered fuel flow (TOTAL RANGE) - This value is calculated by multiplying the time of fuel
endurance by the ground speed.
OTHER STATISTICS
These statistics are calculated based on the system sensor inputs or the manual trip planning inputs.
HAZARD
AVOIDANCE
• Density altitude (DENSITY ALT)
• True airspeed (TRUE AIRSPEED)
The pilot may select automatic (AUTO) or manual (MANUAL) page mode, and flight plan (FPL) or waypoint
(WPTS) mode. In automatic page mode, only the FPL, LEG, or waypoint IDs are editable (based on FPL/WPTS
selection).
Selected Flight Plan NN -
Stored Flight Plan
- CUM: Beginning to End of FPL
- NN: Beginning to End of Selected Leg
Active Flight Plan
- REM: Pres. Pos. to End of FPL
- NN: Pres. Pos. to End of Selected Leg
ADDITIONAL
FEATURES
Starting and Ending Waypoint
of Selected Flight Plan Segment
AFCS
Selected Leg(s)
00 is Active FPL
01-99 are Stored FPLs
Figure 5-100 Trip Planning Page - Flight Plan Mode
Not Available
Selected Leg(s)
APPENDICES
Selected Flight Plan
Not Available
Selected Starting and Ending Waypoints
Figure 5-101 Trip Planning Page - Waypoint Mode
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
247
SYSTEM
OVERVIEW
Selecting automatic or manual page mode:
FLIGHT
INSTRUMENTS
FLIGHT MANAGEMENT
Selecting flight plan or waypoint mode:
Select the AUTO Softkey or the MANUAL Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual
Mode’, and press the ENT Key.
Select the FPL Softkey or the WPTS Softkey; or press the MENU Key, highlight ‘Flight Plan Mode’ or ‘Waypoints
Mode’, and press the ENT Key.
Selecting a flight plan and leg for trip statistics:
EIS
1) Press the FMS Knob to activate the cursor in the flight plan number field.
2) Turn the small FMS Knob to select the desired flight plan number.
AUDIO PANEL
& CNS
3) Turn the large FMS Knob to highlight ‘CUM’ or ‘REM’. The statistics for each leg can be viewed by turning the
small FMS Knob to select the desired leg. The Inset Map also displays the selected data.
Selecting waypoints for waypoint mode:
FLIGHT
MANAGEMENT
1) Select the WPTS Softkey; or press the MENU Key, highlight ‘Waypoints Mode’, and press the ENT Key. The
cursor is positioned in the waypoint field directly below the FPL field.
2) Turn the FMS knobs to select the desired waypoint (or select from the Page Menu ‘Set WPT to Present Position’
if that is what is desired), and press the ENT Key. The cursor moves to the second waypoint field.
HAZARD
AVOIDANCE
3) Turn the FMS knobs to select the desired waypoint, and press the ENT Key. The statistics for the selected leg
are displayed.
In manual page mode, the other eight trip input data fields must be entered by the pilot, in addition to flight
plan and leg selection.
Entering manual data for trip statistics calculations:
AFCS
1) Select the MANUAL Softkey or select ‘Manual Mode’ from the Page Menu, and press the ENT Key. The cursor
may now be positioned in any field in the top right two boxes.
INDEX
APPENDICES
ADDITIONAL
FEATURES
2) Turn the FMS Knobs to move the cursor onto the DEP TIME field and enter the desired value. Press the ENT Key.
The statistics are calculated using the new value and the cursor moves to the next entry field. Repeat until all
desired values have been entered.
248
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
5.10 RAIM PREDICTION
FLIGHT
INSTRUMENTS
RAIM (Receiver Autonomous Integrity Monitoring) is a GPS receiver function that performs a consistency
check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate
a position within a specified RAIM protection limit (2.0 nm for oceanic, 2.0 nm for enroute, 1.0 nm for terminal,
and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is
available nearly 100% of the time. The RAIM prediction function also indicates whether RAIM is available at a
specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival
date and time. Because of the tighter protection limit on approaches, there may be times when RAIM is not
available. RAIM prediction must be initiated manually if there is concern over SBAS coverage at the destination
or some other reason that compromises navigation precision. If RAIM is not predicted to be available for the
final approach course, the approach does not become active. If RAIM is not available when crossing the FAF, the
missed approach procedure must be flown.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
RAIM PREDICTION Box
AFCS
RAIM Softkey
HAZARD
AVOIDANCE
- Prediction Waypoint
- Arrival Time
- Arrival Date
- RAIM Status
SBAS Softkey
(displays SBAS Selection)
(displays RAIM PREDICTION)
Figure 5-102 RAIM Prediction
ADDITIONAL
FEATURES
Predicting RAIM availability at a selected waypoint:
1) Select the AUX-GPS Status Page.
APPENDICES
2) Press the FMS Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted.
3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank
Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway
waypoints).
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
4) Enter the identifier, facility, or city name of the departure waypoint; or select a waypoint from the submenu of
waypoints and press the ENT Key to accept the waypoint entry.
249
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
5) Turn the FMS Knobs to enter an arrival time and press the ENT Key.
6) Turn the FMS Knobs to enter an arrival date and press the ENT Key.
FLIGHT
INSTRUMENTS
7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation.
Predicting RAIM availability at the aircraft present position:
1) Select the AUX-GPS Status Page.
2) Press the FMS Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted.
3) Press the MENU Key, highlight ‘Set WPT to Present Position’, and press the ENT Key.
EIS
4) Press the ENT Key to accept the waypoint entry.
5) Turn the FMS Knobs to enter an arrival time and press the ENT Key.
AUDIO PANEL
& CNS
6) Turn the FMS Knobs to enter an arrival date and press the ENT Key.
7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation.
FLIGHT
MANAGEMENT
• ‘COMPUTE RAIM?’ - RAIM has not been computed.
HAZARD
AVOIDANCE
Status of the RAIM computation for the selected waypoint, time, and date is displayed at the bottom of the
RAIM PREDICTION Box as follows:
The Satellite Based Augmentation System (SBAS) provides increased navigation accuracy when available. SBAS
can be enabled or disabled manually on the GPS Status Page.
• ‘COMPUTING AVAILABILITY’ - RAIM calculation is in progress.
• ‘RAIM AVAILABLE’ - RAIM is predicted to be available.
AFCS
• ‘RAIM NOT AVAILABLE’ - RAIM is predicted to be unavailable.
SBAS Status
ADDITIONAL
FEATURES
SBAS SELECTION Box
APPENDICES
- EGNOS Enable/Disable
- MSAS Enable/Disable
- WAAS Enable/Disable
RAIM Softkey
SBAS Softkey
(displays SBAS Selection)
INDEX
(displays RAIM PREDICTION)
Figure 5-103 SBAS Display - Active
250
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Enabling/Disabling SBAS:
1) Select the AUX-GPS Status Page.
2) Press the SBAS Softkey.
FLIGHT
INSTRUMENTS
3) Press the FMS Knob, and turn the large FMS Knob to highlight ‘EGNOS’, ‘MSAS’ or ‘WAAS’.
4) Press the ENT Key to disable SBAS. Press the ENT Key again to enable SBAS.
EIS
SBAS Status
AUDIO PANEL
& CNS
SBAS SELECTION Box
- EGNOS Enable/Disable
- MSAS Enable/Disable
- WAAS Enable/Disable
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
SBAS Softkey
(displays SBAS Selection)
RAIM Softkey
(displays RAIM PREDICTION)
Figure 5-104 SBAS Display - Disabled
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
251
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
5.11 NAVIGATING A FLIGHT PLAN
FLIGHT
INSTRUMENTS
The following discussion is an example of navigating a flight plan with the SBAS capable GPS system while the
G1000 provides vertical guidance through descents. A lateral flight plan (LNAV) would be navigated in much the
same way, but would not include vertical guidance when the final approach course is active.
NOTE: The following example flight plan is for instructional purposes only. All database information depicted
should be considered not current.
AUDIO PANEL
& CNS
1) Prior to departure, the TIFTO2 departure, the airways, and the DBRY1 arrival at KCOS are loaded. See the
Procedures section for loading departures and arrivals. Note the magenta arrow in Figure 5-105 indicating the
active departure leg.
FLIGHT
MANAGEMENT
EIS
The example is a flight plan from KMKC to KCOS filed using the TIFTO2 departure, various Victor Airways,
and the DBRY1 arrival with the transition at TBE. The flight plan includes an enroute altitude of 12,000 feet, an
LPV (WAAS) approach selected for runway 35R, and a missed approach executed at the Missed Approach Point
(MAP). A few enroute changes are demonstrated.
2) Figure 5-105 shows the aircraft on the assigned heading of 240º. ‘TERM’ (Terminal) is the current CDI flight
phase displayed on the HSI indicating 1.0 nm CDI scaling.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
After takeoff, ATC assigns a heading of 240º.
INDEX
Figure 5-105 Assigned Heading of 240º
252
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
3) ATC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. The aircraft turns to heading
290° as seen in Figure 5-106.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-106 Assigned Heading of 290º
4) Enter V4 into the flight plan.
HAZARD
AVOIDANCE
a) Press the FMS Knob to activate the cursor.
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
253
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
b) The desired entry point for V4 (TOP) must be entered. Turn the large FMS Knob to highlight the desired flight
plan insertion point (SLN) as shown in Figure 5-107. When the V4 entry point (TOP) is inserted, it is placed
immediately above the highlighted waypoint (SLN).
FLIGHT
MANAGEMENT
Figure 5-107 Begin Adding V4 to the Flight Plan
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
c) Turn the small FMS Knob to display the Waypoint Information Window. Enter the desired entry point for V4,
Topeka VOR (TOP), as shown in Figure 5-108.
INDEX
Figure 5-108 Entering V4 Entry Point
254
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
d) Press the ENT Key. TOP is inserted into the flight plan as in Figure 5-109.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Figure 5-109 TOP Inserted into the Flight Plan
FLIGHT
MANAGEMENT
e) With SLN still highlighted as in Figure 5-109, turn the small FMS Knob clockwise. The Waypoint Information
Page is displayed and the LD AIRWY Softkey is now available.
f) Select the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 5-110.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 5-110 List of Available Airways for TOP
APPENDICES
g) Turn either FMS Knob to highlight V4 in the list as seen in Figure 5-110 .
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
255
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
h) Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 5-111.
FLIGHT
MANAGEMENT
Figure 5-111 List of Available Exits for V4
i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as in
Figure 5-111.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
j) Press the ENT Key. The selected airway and exit are displayed, and the prompt “LOAD?” highlighted as in
Figure 5-112.
Figure 5-112 Ready to Load V4
INDEX
k) Press the ENT Key.
256
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
l) V4 is now loaded into the flight plan as shown in Figure 5-113.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Figure 5-113 V4 is Loaded in the Flight Plan
FLIGHT
MANAGEMENT
5) Making V4 the active leg of the flight plan.
a) Press the FMS Knob to activate the cursor.
b) Turn the large FMS Knob to highlight SLN. The TO waypoint of the leg is selected in order to activate the leg.
HAZARD
AVOIDANCE
c) Select the ACT LEG Softkey. The confirmation window is now displayed as in Figure 5-114. Note the TOP to
SLN leg is actually part of V4.
AFCS
Figure 5-114 Comfirm Active Leg
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
257
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 5-115, the magenta arrow in
the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg. Note the
phase of flight remained in Terminal (TERM) mode up to this point because a departure leg was active. Since a
leg after the departure is now active, the current CDI flight phase is ENR (Enroute) and CDI scaling has changed
to 2.0 nm.
HAZARD
AVOIDANCE
Figure 5-115 V4 Now Active Leg
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
6) The aircraft continues on heading 290º. When crosstrack distance is less than 2.0 nm, the XTK disappears from
the HSI and the CDI is positioned on the last dot indicating a 2.0 nm distance from the centerline of the next
course.
258
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 5-116.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-116 Turn on to Active Leg
8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box
as seen in Figure 5-117.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 5-117 Turn to Intercept V244
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
259
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
9) As seen in Figure 5-118, V244 is now the active flight plan leg.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Figure 5-118 V244 Now Active Leg
260
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-119.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-119 HYS to LAA Leg Active
HAZARD
AVOIDANCE
11) ATC grants clearance to proceed direct to the OPSHN intersection to begin the arrival procedure. ATC advises
to expect an altitude of 10,000 feet at OPSHN.
a) Press the FMS Knob to activate the cursor.
b) Turn the large FMS Knob to select OPSHN in the flight plan list.
c) Press the Direct-to (
) Key. The Direct-to Window is now displayed as shown in Figure 5-120.
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 5-120 Direct To OPSHN
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
261
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 5-121.
FLIGHT
MANAGEMENT
Figure 5-121 Enter VNV Altitude
e) An altitude of 10,000 feet is entered as requested by ATC.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 5-122.
Figure 5-122 Enter VNV Offset Distance
INDEX
g) Enter the offset, or distance from the waypoint at which to reach the selected altitude. In this case, three miles
prior to OPSHN is entered. In other words, the G1000 gives vertical guidance so the aircraft arrives at an
altitude of 10,000 feet three miles prior to OPSHN.
262
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
h) Press the ENT Key twice to activate the direct-to. Note, in Figure 5-123, the magenta arrow indicating the
direct-to OPSHN after the offset waypoint for OPSHN. The preceding offset waypoint indicates the offset
distance and altitude that were previously entered. The remaining waypoints in the loaded arrival procedure
have no database specified altitudes, therefore, dashes are displayed. Keep the CDI centered and maintain a
track along the magenta line to OPSHN.
Note the Direct-to waypoint is within the loaded arrival procedure, therefore, phase of flight scaling for the CDI
changes to Terminal Mode and is annunciated by displaying ‘TERM’ on the HSI.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 5-123 Direct-to Active
12) The aircraft is proceeding to OPSHN. The expected approach is the RNAV LPV approach to runway 35R, so it is
selected.
AFCS
a) Press the PROC Key to display the Procedures Window.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
263
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-124.
FLIGHT
MANAGEMENT
Figure 5-124 Procedures Window
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-125.
APPENDICES
Figure 5-125 List of Available Approaches
INDEX
d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 5-125.
264
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
e) Press the ENT Key. A list of available transitions for the selected approach is displayed as in Figure 5-126.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-126 List of Available Transitions
f) Turn either FMS Knob to select the desired transition. In this case, the Initial Approach Fix (IAF) at HABUK is
used.
g) Press the ENT Key.
HAZARD
AVOIDANCE
h) Barometric Minimums
To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’, and press the ENT Key. Turn the small FMS Knob to select the altitude, and press the ENT Key.
Or:
AFCS
To skip setting minimums, press the ENT Key.
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 5-127 Barometric Minimums Set
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
265
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
i) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen
in Figure 5-128.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Figure 5-128 Loaded Approach
266
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-129. These
altitudes are loaded from the database and are displayed as light blue text, indicating these values are
“designated” for use in computing vertical deviation guidance.
FLIGHT
INSTRUMENTS
Note: To no longer use the displayed altitude for calculating vertical deviation guidance, perform the
following:
a) Press the FMS Knob to activate the cursor.
b) Turn the small FMS Knob to highlight the desired altitude.
c) Press the CLR Key.
EIS
d) Press the FMS Knob to deactivate the cursor.
After making the altitude “non-designated”, it is displayed as white text.
AUDIO PANEL
& CNS
Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be
designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 5-129.
Vertical guidance from the FAF and on to the Missed Approach Point (MAP) is given using the WAAS GPS
altitude source, therefore, the displayed altitude values are for reference only.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
Figure 5-129 Vertical Guidance is Active to the FAF
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
267
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
14) As the aircraft approaches OPSHN, it may be desirable to adjust the speed, or steepness of the upcoming
descent. The default Flight Path Angle (FPA) is -3.0 degrees and a required vertical speed is computed to
maintain the -3.0 FPA. To change the vertical flight path, perform the following steps.
FLIGHT
INSTRUMENTS
a) Select the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure
5-130.
b) At this point, the descent vertical speed can be selected, or the FPA can be selected. Turn the large FMS Knob
to select the desired selection field, then turn the small FMS Knob to enter the desired value.
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Note the information now displayed in the ‘CURRENT VNV PROFILE’ box. Also, note the offset waypoint (orange
box) and gray circle are now displayed on the map. The gray circle marks the Top of Descent (TOD). In this
example, vertical guidance is provided at the TOD that results in a -3.0 degree FPA descent to an altitude of
10,000 feet upon reaching the offset waypoint.
Figure 5-130 Adjusting the Descent
INDEX
APPENDICES
ADDITIONAL
FEATURES
c) Press the ENT Key.
268
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
15) As seen in Figure 5-131, the aircraft is approaching TOD. Note the target vertical speed required to reach the
selected altitude. The Vertical Deviation Indicator (VDI) and the Required Vertical Speed Indicator (RVSI) are
now displayed on the PFD as shown in Figure 5-132. When the aircraft is within one minute of the TOD, it is
annunciated as shown in Figure 5-132, and an aural alert ‘Vertical track’ will be heard.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-131 Approaching Top of Descent (TOD)
HAZARD
AVOIDANCE
Target Altitude
AFCS
Vertical Deviation
Indicator (VDI)
ADDITIONAL
FEATURES
Required Vertical
Speed Indicator
(RVSI)
APPENDICES
Figure 5-132 VDI & RVSI Upon Reaching Top of Descent (TOD)
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
269
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
EIS
FLIGHT
INSTRUMENTS
16) Upon reaching TOD, a descent vertical speed is established by placing the VSI pointer in line with the RVSI as
shown in Figure 5-133.
Keep Vertical Deviation
Indicator Centered
AUDIO PANEL
& CNS
Align Actual Vertical Speed
with
Required Vertical Speed
FLIGHT
MANAGEMENT
Figure 5-133 VDI & RVSI Showing Correctly Established Descent
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
17) When the aircraft is one minute from the bottom of descent (BOD) it is annunciated as shown in Figure 5-134.
Upon reaching the offset waypoint for OPSHN, the aircraft is at 10,000 feet.
INDEX
Figure 5-134 Approaching Bottom of Descent (BOD) at OPSHN Offset Waypoint
270
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
18) The aircraft is approaching OPSHN. The upcoming turn and next heading are annunciated at the top left of the
PFD as seen in Figure 5-135. Initiate the turn and maneuver the aircraft on a track through the turn radius to
intercept the magenta line for the OPSHN to FSHER leg and center the CDI.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
Figure 5-135 Turn to intercept OPSHN to FSHER Leg
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
271
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-136. The magenta arrow
in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active.
Figure 5-136 Tracking the OPSHN to FSHER Leg
HAZARD
AVOIDANCE
20) The flight continues through the arrival procedure to PYNON (see Figure 5-137). At a point 31 nm from the
destination airport, the phase of flight scaling for the CDI changes to Terminal Mode and is annunciated by
displaying ‘TERM’ on the HSI.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
A descent to HABUK is in the next leg. Note the TOD point on the map. Annunciations for the upcoming turn
and descent, as well as the VDI and RVSI, appear on the PFD as the flight progresses.
272
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
Figure 5-137 Approaching PYNON
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
273
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
21) Upon passing PYNON the approach procedure automatically becomes active. The approach may be activated
at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final
waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating
the approach procedure (see Figure 5-138).
HAZARD
AVOIDANCE
Figure 5-138 Approach is Now Active
Note: To manually activate the approach procedure, perform the following steps:
a) Press the PROC Key.
b) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’ as shown in Figure 5-139.
ADDITIONAL
FEATURES
AFCS
c) Press the ENT Key to activate the approach.
INDEX
APPENDICES
Figure 5-139 Manually Activate Approach
274
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16.
The aircraft altitude is 9,000 feet upon reaching HABUK.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-140 Descending Turn to the Initial Approach Fix (IAF)
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
275
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the
current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is
used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to
the Glidepath Indicator (as shown in Figure 5-141) when the final approach course becomes active.
HAZARD
AVOIDANCE
Figure 5-141 Descending to the FAF
The descent continues through the FAF (CEGIX) using the Glidepath Indicator, as one would use a glideslope
indicator, to obtain an altitude “AT” 7,800 feet at the FAF. Note the altitude restriction lines over and under (At)
the altitude in the ‘ALT’ field in Figure 5-141.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
276
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
24) After crossing CEGIX, the aircraft continues following the glidepath to maintain the descent to “AT or ABOVE”
6,370 feet at the Missed Approach Point (MAP) (RW35R) as seen in Figure 5-142.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-142 Descending to the Missed Approach Point
HAZARD
AVOIDANCE
In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part
of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along the runway
centerline until the required altitude required to safely make the first turn toward the MAHP is exceeded. In
this case, if the aircraft altitude is below the specified altitude (6,368 feet) after crossing the MAP, a direct-to is
established to provide a course on runway heading until an altitude of 6,368 feet reached. After reaching 6,368
feet, a direct-to is established to the published MAHP (in this case MOGAL). If the aircraft altitude is above the
specified altitude after crossing the MAP, a direct-to is established to the published fix (MOGAL) to begin the
missed approach procedure. The altitude constraint value defaults to 400 feet AGL when there is no Course to
Altitude defined in the published procedure.
AFCS
ADDITIONAL
FEATURES
In some missed approach procedures this Course to Altitude leg may be part of the published procedure. For
example, the procedure dictates a climb to 5,500 feet, then turn left and proceed to the Missed Approach Hold
Point (MAHP). In this case, the altitude would appear in the list of waypoints as ‘5500ft’. Again, if the aircraft
altitude is lower than the prescribed altitude, a direct-to is established on a Course to Altitude leg when the
missed approach procedure is activated.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
277
SYSTEM
OVERVIEW
A direct-to is initiated to MOGAL, which is the Missed Approach Hold Point (MAHP) as seen in Figure 5-143.
The aircraft is climbing to 10,000 feet. The CDI flight phase now changes from LPV to MAPR as seen on the HSI.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
25) Upon reaching the MAP, it is decided to execute a missed approach. Automatic waypoint sequencing is
suspended past the MAP. Select the SUSP Softkey on the PFD to resume automatic waypoint sequencing
through the missed approach procedure.
FLIGHT
INSTRUMENTS
FLIGHT MANAGEMENT
INDEX
Figure 5-143 Missed Approach Active
278
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern is established at
the MAHP (MOGAL) as shown in Figure 5-144.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 5-144 Establishing the Holding Pattern
27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 5-145.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 5-145 Hold Established
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
279
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
5.12 ABNORMAL OPERATION
FLIGHT
INSTRUMENTS
This section discusses the Dead Reckoning mode of operation and the subsequent indications.
NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other
phases, an invalid GPS solution produces a “NO GPS POSITION” annunciation on the map and the G1000
stops using GPS.
EIS
While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS solution or is unable to
calculate a GPS position, the system automatically reverts to Dead Reckoning (DR) Mode. In DR Mode, the G1000
uses its last-known position combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly
unreliable and must not be used as a sole means of navigation. If while in DR Mode airspeed and/or heading data
is also lost or not available, the DR function may not be capable of accurately tracking estimated position and,
consequently, the system may display a path that is different than the actual movement of the aircraft. Estimated
position information displayed by the G1000 through DR while there is no heading and/or airspeed data available
should not be used for navigation.
HAZARD
AVOIDANCE
DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the lack of satellite measurements
needed to determine a position. Changes in wind speed and/or wind direction compound the relative inaccuracy
of DR Mode. Because of this degraded accuracy, other navigation equipment must be relied upon for position
awareness until GPS-derived position data is restored.
AFCS
DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’ superimposed in yellow over the
‘own aircraft’ symbol as shown in Figure 5-146. In addition, ‘DR’ is prominently displayed in yellow on the HSI
slightly above and to the right of the aircraft symbol on the CDI as shown in Figure 5-146. The CDI deviation
bar remains, but is removed from the display after 20 minutes in DR Mode. The autopilot will remain coupled
in DR mode as long as the deviation is available (20 min.) Lastly, but at the same time, a ‘GPS NAV LOST’ alert
message appears on the PFD. Normal navigation using GPS/SBAS source data resumes automatically once a valid
GPS solution is restored.
ADDITIONAL
FEATURES
As a result of operating in DR Mode, all GPS-derived data is computed based upon an estimated position and
is displayed as yellow text on the display to denote degraded navigation source information as shown in Figure
5-146.
INDEX
APPENDICES
Also, while the G1000 is in DR Mode, the autopilot will remain coupled to GPS for up to 20 minutes. TAWS,
Terrain-SVS, and Terrain Proximity are disabled. Additionally, the accuracy of all nearest information (airports,
airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded
accuracy.
280
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
FLIGHT MANAGEMENT
SYSTEM
OVERVIEW
Distance &
Bearing
FLIGHT
INSTRUMENTS
Dead Reckoning
Annunciaion
Wind Data
Current Track
Indicator
EIS
GPS Navigation
Lost Message
Course Deviation
Indicator
AUDIO PANEL
& CNS
Bearing Pointer/
Distance
Navigation Data Bar
Wind Data
FLIGHT
MANAGEMENT
All data except Active Leg,
TAS, and DTK are in yellow
Dead Reckoning
Annunciation
HAZARD
AVOIDANCE
Subdued Aircraft
Symbol
AFCS
Figure 5-146 Dead Reckoning Mode - GPS Derived Data Shown in Yellow
ADDITIONAL
FEATURES
NOTE: The Inset Map is removed from the PFD any time aircraft pitch is greater than +30° or less than –20°,
or when a 65° bank angle is reached.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
281
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
FLIGHT MANAGEMENT
Blank Page
282
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
SECTION 6 HAZARD AVOIDANCE
FLIGHT
INSTRUMENTS
Hazard avoidance features available for the G1000 are designed to aid situational awareness and provide advisory
information with regard to potential hazards to flight safety associated with weather, terrain, and air traffic.
Weather
• GDL 69/69A SiriusXM Weather
®
• L-3 Stormscope WX-500 Series II Weather Mapping Sensor (Optional)
Terrain Avoidance
EIS
• Terrain Proximity
• Terrain-SVS (Standard with SVS Option)
AUDIO PANEL
& CNS
• Terrain Awareness and Warning System - Class B (TAWS-B) (Optional)
Traffic
• Traffic Information Service (TIS)
• TCAD 9900BX/TAS 620 Traffic Advisory System (Optional)
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
283
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
6.1 SIRIUSXM WEATHER
FLIGHT
INSTRUMENTS
WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous
weather. Information contained within data link weather products may not accurately depict current
weather conditions.
EIS
SiriusXM Weather is provided through the GDL 69/69A, a remote-mounted data link satellite receiver. Received
graphical weather information and associated text is displayed on the Multi Function Display (MFD) and the
Primary Flight Display (PFD) Inset Map. The GDL 69A can also receive SiriusXM Satellite Radio entertainment
services. Both weather data and entertainment programming operate in the S-band frequency range to provide
continuous reception capabilities at any altitude throughout North America.
AUDIO PANEL
& CNS
Services from SiriusXM are subscription-based. For more information on specific service packages, visit www.
siriusxm.com.
ACTIVATING SERVICES
FLIGHT
MANAGEMENT
Before SiriusXM Weather and SiriusXM Satellite Radio can be used, the service must be activated. Service is
activated by providing coded IDs unique to the installed GDL 69/69A. SiriusXM Satellite Radio (audio) and
SiriusXM Weather (data) services each have coded IDs. The Data and Audio Radio IDs must be provided to
activate the weather service and entertainment subscriptions, respectively. These IDs are located on:
• The label on the back of the Data Link Receiver
HAZARD
AVOIDANCE
• The XM Information Page on the MFD (Figure 6-1)
• The XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N
190-00355-04)
Contact the installer if the Audio and Data Radio IDs cannot be located.
AFCS
SiriusXM uses the coded IDs to send an activation signal that allows the system to display weather data and/
or entertainment programming provided through the GDL 69/69A.
Activating SiriusXM Weather and SiriusXM Satellite Radio services:
ADDITIONAL
FEATURES
1) Contact SiriusXM using the customer service phone number listed on the website. Follow the instructions
provided by SiriusXM Customer Service.
2) Select the XM Page in the Auxiliary Page Group.
3) Select the INFO Softkey to display the XM Information Page.
APPENDICES
4) Verify that the desired services are activated.
5) Select the LOCK Softkey.
6) Turn the large FMS Knob to highlight ‘YES’.
INDEX
7) To complete activation, press the ENT Key.
284
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Data Radio
ID (for
SiriusXM
Weather)
Audio Radio
ID (for XM
Satellite Radio)
FLIGHT
INSTRUMENTS
EIS
Weather Products
(Available
Products for
Service Class
Indicated in
Green)
Select LOCK
Softkey to Lock
Subscription
Information
FLIGHT
MANAGEMENT
Figure 6-1 XM Information Page
AUDIO PANEL
& CNS
Select INFO
Softkey to
Display XM
Information Page
USING SIRIUSXM WEATHER PRODUCTS
HAZARD
AVOIDANCE
The principal map for viewing SiriusXM Weather information is the Weather Data Link (XM) Page in the Map
Page Group. This is the only map display capable of showing information for all available SiriusXM products.
Viewing the Weather Data Link (XM) Page:
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Weather Data Link (XM) Page.
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
285
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
NEXRAD Weather
Product Enabled Icon
FLIGHT
INSTRUMENTS
Weather
Product
Ages in
Minutes
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Cloud Tops Weather
Product Enabled Icon
Figure 6-2 Weather Data Link (XM) Page
HAZARD
AVOIDANCE
WARNING: Do not use the indicated data link weather product age to determine the age of the weather
information shown by the data link weather product. Due to time delays inherent in gathering and processing
weather data for data link transmission, the weather information shown by the data link weather product
may be significantly older than the indicated weather product age.
AFCS
For each enabled SiriusXM Weather product, the system displays a weather product icon and product age. The product age is the elapsed time (in minutes) since the weather data provider compiled the weather product.
The product age display does not indicate the age of the information contained within the weather product,
which can be significantly older than the displayed weather product age.
APPENDICES
ADDITIONAL
FEATURES
The SiriusXM Weather service broadcasts weather products at specific intervals (defined in the Broadcast
Rate column in Table 6-1). If for any reason, a product is not broadcast within the Expiration Time intervals
(see Table 6-1), the system removes the expired data from the display, and shows dashes instead of the product
age. This ensures the displayed information is consistent with what is currently being transmitted by the
SiriusXM Weather service. If more than half of the expiration time has elapsed, the color of the product age
changes to yellow. If data for a weather product is not available, the system displays ‘N/A’ next to the weather
product symbol instead of the product age.
INDEX
Table 6-1 shows the weather product symbols, the expiration times and the broadcast rates. The broadcast
rate represents the interval at which the SiriusXM Weather service transmits new signals that may or may not
contain updated weather products. It does not represent the rate at which the weather information is updated
or when the Data Link Receiver receives new data. SiriusXM and its weather data suppliers define and control
the data update intervals, which are subject to change.
286
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
Symbol
30
60
12
90
12
60
12
60
12
60
12
60
12
60
5
60
12
90
12
90
12
90
12
180
12
no product image
30
5
Temporary Flight Restrictions
(TFRs)
Terminal Aerodrome Reports
(TAFs)
no product image
60
12
no product image
60
12
INDEX
12
APPENDICES
30
ADDITIONAL
FEATURES
5
AFCS
30
SiriusXM Lightning
(XM LTNG)
Cell Movement
(CELL MOV)
SIGMETs/AIRMETs
(SIG/AIR)
Meteorological Aerodrome Report
(METARs)
City Forecast
(CITY)
Surface Analysis
(SFC)
Freezing Levels
(FRZ LVL)
Winds Aloft
(WIND)
County Warnings
(COUNTY)
Cyclone Warnings
(CYCLONE)
Icing Potential (CIP and SLD)
(ICNG)
Pilot Weather Report
(PIREPs)
Air Report
(AIREPs)
Turbulence
(TURB)
HAZARD
AVOIDANCE
7.5
FLIGHT
MANAGEMENT
30
AUDIO PANEL
& CNS
15
EIS
60
Echo Top
(ECHO TOP)
No Radar Coverage
Broadcast Rate
(Minutes)
5 (U.S.)
10 (Canada)
FLIGHT
INSTRUMENTS
Next-generation Radar
(NEXRAD)
Cloud Top
(CLD TOP)
Expiration Time
(Minutes)
SYSTEM
OVERVIEW
SiriusXM Weather Product
Table 6-1 SiriusXM Weather Product Symbols and Data Timing
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
287
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
AUDIO PANEL
& CNS
Cloud Top (CLD TOP)
+
Echo Top (ECHO TOP)
+
Flight Plan Pages
+
+
+
+
+
+
+
+
+
+
Cell Movement (CELL MOV)
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
+
FLIGHT
MANAGEMENT
+
City Forecast (CITY)
HAZARD
AVOIDANCE
METARs
County Warnings (COUNTY)
+
Cyclone Warnings (CYCLONE)
+
Icing Potential (ICNG)
+
PIREPs
+
AIREPs
+
Turbulence (TURB)
+
+
Surface Analysis (SFC)
+
Freezing Levels (FRZ LVL)
+
Winds Aloft (WIND)
AFCS
+
SiriusXM Lightning (XM LTNG)
SIGMETs/AIRMETs (SIG/AIR)
+*
No Radar Coverage
TFRs
ADDITIONAL
FEATURES
Nearest Page Group
+
AUX - Video Page
+
AUX - Trip Planning
Page
+
Weather Information
Page
Weather Data Link
(XM) Page
EIS
NEXRAD
Navigation Map Page
Weather Product
PFD Inset Map
FLIGHT
INSTRUMENTS
This table shows which SiriusXM products can be displayed (indicated with a ‘+’ symbol) on specific maps.
TAFs
+
+
+
+
+
+
+
+
+
INDEX
APPENDICES
* Winds Aloft data available inside Profile View on Navigation Map Page.
Table 6-2 SiriusXM Weather Product Display Maps
288
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
WEATHER SOFTKEYS ON THE WEATHER DATA LINK (XM) PAGE
NEXRAD ECHO TOP CLD TOP
SYSTEM
CYCLONE SFC OFF
FRZ LVL
SIG/AIR
METAR
LEGEND MORE WX CHKLIST
WIND OFF ICNG OFF TURB OFF AIREPS
PIREPS
COUNTY
LTNG
CELL MOV
FLIGHT
INSTRUMENTS
Softkeys control the display of weather information on most MFD pages and the PFD Inset Map (The figure
shows the weather product softkeys for the Weather Data Link (XM) Page). When a weather product is selected
for display, the corresponding softkey label changes to gray to indicate the product is enabled for display.
BACK
EIS
SFC Softkey label changes
to reflect current selection.
WIND/ICNG/TURB Softkey labels
change to reflect current selection.
CURRENT
12 HR
24 HR
36 HR
48 HR
LEGEND
BACK
AUDIO PANEL
& CNS
OFF
Select the BACK Softkey
to move up one level.
PREV and NEXT Softkeys cycle through Winds Aloft,
Icing, and Turbulence altitude selection softkeys.
6000
9000
12000
15000
NEXT
LEGEND
BACK
PREV
OFF
18000
21000
24000
27000
30000
33000
NEXT
LEGEND
BACK
PREV
OFF
36000
39000
42000
NEXT
LEGEND
BACK
PREV
OFF
1000
3000
6000
9000
12000
NEXT
LEGEND
BACK
PREV
OFF
18000
21000
24000
27000
30000
NEXT
LEGEND
BACK
PREV
OFF
21000
24000
27000
30000
33000
NEXT
LEGEND
BACK
PREV
OFF
39000
42000
45000
NEXT
LEGEND
BACK
15000
36000
ADDITIONAL
FEATURES
3000
AFCS
SFC
HAZARD
AVOIDANCE
OFF
FLIGHT
MANAGEMENT
PREV
Figure 6-3 Weather Data Link (XM) Page Weather Product Softkeys
APPENDICES
The setup menus for the Navigation Map Page and the Weather Data Link (XM) Page control the map range
settings above which weather products data are decluttered from the display. If a map range larger than the
weather product map range setting is selected, the weather product data is removed from the map. The menus
also provide a means in addition to the softkeys for enabling/disabling display of weather products.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
289
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Setting up and customizing the Weather Data Link (XM) Page:
1) Select the Weather Data Link (XM) Page.
FLIGHT
INSTRUMENTS
2) Press the MENU Key.
3) With ‘Weather Setup’ highlighted, press the ENT Key (Figure 6-4).
4) Turn the small FMS Knob to select ‘PRODUCT GROUP 1’ or ‘PRODUCT GROUP 2’, and press the ENT Key (Figure
6-5).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections.
EIS
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.).
7) Press the ENT Key to select an option.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
8) Press the FMS Knob or CLR Key to return to the Weather Data Link (XM) Page with the changed settings.
ADDITIONAL
FEATURES
AFCS
Figure 6-4 Weather Data Link (XM) Page Menu
Figure 6-5 Weather Data Link (XM) Page Setup Menu
Restoring default Weather Data Link (XM) Page settings:
APPENDICES
1) Select the Weather Data Link (XM) Page with the FMS Knob.
2) Press the MENU Key.
3) With Weather Setup highlighted, press the ENT Key.
4) Press the MENU Key.
INDEX
5) Highlight the desired default(s) to restore (all or for selection) and press the ENT Key.
290
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Maps other than the Weather Data Link (XM) Page use settings based on those selected for the Navigation
Map Page.
Setting up and customizing weather data for the Navigation Map Page:
FLIGHT
INSTRUMENTS
1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With Map Setup highlighted, press the ENT Key (Figure 6-6).
4) Turn the small FMS Knob to select the Weather Group and press the ENT Key (Figure 6-7).
EIS
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-8).
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
7) Press the ENT Key to select an option.
AUDIO PANEL
& CNS
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 6-6 Navigation Map Page Menu
AFCS
ADDITIONAL
FEATURES
Figure 6-7 Navigation Map Page Setup Menu
Figure 6-8 Navigation Map Page Setup Menu, Weather Group
APPENDICES
When a SiriusXM Weather product is enabled for display on the PFD Inset Map, the weather product
information box (with the product icon and product age) can be displayed inside the PFD Inset Map.
Viewing the weather product information box on the PFD Inset Map:
1) On the PFD, press the INSET Softkey.
INDEX
2) Press the WX LGND Softkey.
3) To remove the weather product information box, press the WX LGND Softkey again or deselect all active
SirisuXM Weather products on the PFD Inset Map.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
291
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Each active SiriusXM product has an associated legend which can be displayed on the Weather Data Link
(XM) Page and Navigation Map Page.
FLIGHT
INSTRUMENTS
Viewing legends for displayed weather products on the Weather Data Link (XM) Page:
1) Select the Weather Data Link (XM) Page with the FMS Knob.
2) Select the LEGEND Softkey to display the legends for the displayed weather products.
Or:
1) Press the MENU Key.
EIS
2) Select Weather Legend and press the ENT Key.
3) Turn the FMS Knob to scroll through the legends if more are available than fit in the window.
AUDIO PANEL
& CNS
4) To remove the XM Weather Legends Window, select the LEGEND Softkey, the ENT or the CLR Key, or press the
FMS Knob.
Viewing legends for displayed weather products on the Navigation Map Page:
1) Select the Navigation Map Page with the FMS Knob.
FLIGHT
MANAGEMENT
2) Select the Map Softkey.
3) Select the Legend Softkey to display the legends for the displayed weather products.
4) To remove the XM Weather Legends Window, select the LEGEND Softkey, the ENT or the CLR Key, or press the
FMS Knob.
HAZARD
AVOIDANCE
Additional information about the following can be displayed by panning over the display on the map:
• Echo Tops
• METARs
• Cell Movement
• County Warnings
• SIGMETs
• TFRs
AFCS
• AIRMETs
INDEX
APPENDICES
ADDITIONAL
FEATURES
The map panning feature is enabled by pressing the RANGE Knob. The map range is adjusted by turning the
RANGE Knob. If the map range is adjusted while panning is enabled, the map is re-centered on the Map Pointer.
292
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Additional
Information on
Selected Item
FLIGHT
INSTRUMENTS
Flash Flood
Warning
Selected with
Map Pointer
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 6-9 Panning on the Weather Data Link (XM) Page
NEXRAD
HAZARD
AVOIDANCE
NOTE: The NEXRAD weather product cannot be displayed at the same time as terrain, echo tops, turbulence,
or icing data is displayed.
AFCS
The National Weather Service (NWS) operates the WSR-88D, or NEXRAD (NEXt-generation RADar)
system, an extensive network of 156 high-resolution Doppler radar systems. The NEXRAD network provides
centralized meteorological information for the continental United States and selected overseas locations. The
maximum range of a single NEXRAD site is 250 nm. In addition to a wide array of services, the NEXRAD
network provides important information about severe weather and air traffic safety.
ADDITIONAL
FEATURES
Individual NEXRAD sites supply the network with radar images, and the images from each radar site may
arrive at the network at different rates and times. Periodically, the weather data provider compiles the available
individual site images from the network to form a composite image, and assigns a single time to indicate when
it created the image. This image becomes the NEXRAD weather product. Individual images--gathered from
each NEXRAD site--differ in age, and are always older than the displayed NEXRAD weather product age. The
data provider then sends the NEXRAD data to the SiriusXM Weather service, whose satellites transmit this
information during the next designated refresh time for the NEXRAD weather product.
APPENDICES
Because of the time required to detect, assemble, and distribute the NEXRAD weather product, the displayed
weather information contained within the product may be significantly older than the current radar synopsis
and may not depict the current weather conditions. The NEXRAD weather product should never be used as a
basis for maneuvering in, near, or around areas of hazardous weather regardless of the information it contains.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
293
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
FLIGHT
MANAGEMENT
Figure 6-10 NEXRAD Data on the Weather Data Link (XM) Page
HAZARD
AVOIDANCE
The NEXRAD weather product is available for display on the following maps:
• PFD Inset Map
• Trip Planning Page
• Navigation Map Page
• Nearest Pages
• Weather Data Link (XM) Page
• Flight Plan Pages
• Airport Information Page
• AUX - Video Page
Displaying NEXRAD weather information:
AFCS
1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the
Weather Data Link (XM) Page.
2) Select the NEXRAD Softkey.
INDEX
APPENDICES
ADDITIONAL
FEATURES
Composite data from all the NEXRAD radar sites in the United States is shown. This data is composed of
the maximum reflectivity from the individual radar sweeps. The display of the information is color-coded
to indicate the weather severity level. All weather product legends can be viewed on the Weather Data Link
(XM) Page. For the NEXRAD legend, select the LEGEND Softkey when NEXRAD is selected for display.
294
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
No Radar
Coverage
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 6-11 NEXRAD Data with Legend and Areas
with No Radar Coverage
The display of no radar coverage is always active when either NEXRAD or ECHO TOPS is selected. Areas
where NEXRAD radar coverage and Echo Tops information is not currently available or is not being collected
are indicated in a gray shade of purple.
HAZARD
AVOIDANCE
Reflectivity
Reflectivity is the amount of transmitted power returned to the radar receiver. Colors on the NEXRAD
display directly correlate to the level of detected reflectivity. Reflectivity as it relates to hazardous weather
can be very complex.
AFCS
ADDITIONAL
FEATURES
The role of radar is essentially to detect moisture in the atmosphere. Simply put, certain types of weather reflect radar better than others. The intensity of a radar reflection is not necessarily an indication of the
weather hazard level. For instance, wet hail returns a strong radar reflection, while dry hail does not. Both
wet and dry hail can be extremely hazardous.
The different NEXRAD echo intensities are measured in decibels (dB) relative to reflectivity (Z). NEXRAD
measures the radar reflectivity ratio, or the energy reflected back to the radar receiver (designated by the
letter Z). The value of Z increases as the returned signal strength increases.
APPENDICES
NEXRAD Limitations
NEXRAD radar images may have certain limitations:
• NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation
characteristics. For example, it is not possible to distinguish between wet snow, wet hail, and rain.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
INDEX
• NEXRAD base reflectivity is sampled at the minimum antenna elevation angle. An individual NEXRAD
site cannot depict high altitude storms at close ranges. It has no information about storms directly over
the site.
295
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
• When zoomed in to a range of 30 nm, each square block on the display represents an area of four square
kilometers. The intensity level reflected by each square represents the highest level of NEXRAD data
sampled within the area.
FLIGHT
INSTRUMENTS
• Any unknown precipitation type below 52ºN is displayed as rain.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Each block
covers an
Area of 4 sq.
km
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 6-12 NEXRAD Weather Product at 30 Nautical Miles
296
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
The following may cause abnormalities in displayed NEXRAD radar images:
• Ground clutter
• Strobes and spurious radar data
FLIGHT
INSTRUMENTS
• Sun strobes (when the radar antenna points directly at the sun)
• Interference from buildings or mountains, which may cause shadows
• Metallic dust from military aircraft, which can cause alterations in radar scans
NEXRAD Limitations (Canada)
EIS
• Radar coverage extends to 55ºN.
• Any precipitation displayed between 52ºN and 55ºN is displayed as mixed regardless of actual precipitation
type.
AUDIO PANEL
& CNS
No Coverage
Above 55ºN
FLIGHT
MANAGEMENT
Precipitation
Above 52ºN
Appears Mixed
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 6-13 NEXRAD Weather Product in Canada
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
297
SYSTEM
OVERVIEW
ECHO TOPS
FLIGHT
INSTRUMENTS
HAZARD AVOIDANCE
The Echo Tops weather product (Figure 6-14) shows the location, elevation, and direction of the highest
radar echo. The highest radar echo does not indicate the top of a storm or clouds; rather it indicates the
highest altitude at which precipitation is detected. Information is derived from NEXRAD data.
AUDIO PANEL
& CNS
EIS
NOTE: Echo Tops cannot be displayed at the same time as NEXRAD or Cloud Tops are selected for display.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
No Radar
Coverage
Figure 6-14 Echo Tops Weather Product
AFCS
Displaying Echo Tops information:
1) Select the Weather Data Link (XM) Page with the FMS Knob.
2) Select the ECHO TOP Softkey.
APPENDICES
ADDITIONAL
FEATURES
To display the Echo Tops legend, select the LEGEND Softkey when Echo Tops is selected for display. Since
Echo Tops and Cloud Tops use the same color scaling to represent altitude, display of these weather products
is mutually exclusive. When Echo Tops is activated, NEXRAD and Cloud Tops data are removed.
INDEX
No Radar
Coverage
Figure 6-15 Echo Tops Legend
298
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
The display of no radar coverage is always active when either the NEXRAD or Echo Tops weather products
are displayed. These areas where NEXRAD radar coverage and Echo Tops information is not currently
available or is not being collected are indicated with a gray shade of purple.
FLIGHT
INSTRUMENTS
CLOUD TOPS
NOTE: Cloud Tops and Echo Tops cannot be displayed at the same time.
The Cloud Tops weather product (Figure 6-16) depicts cloud top altitudes as determined from satellite
imagery.
EIS
AUDIO PANEL
& CNS
Cloud Tops
Information
for Area
Selected with
Map Pointer
FLIGHT
MANAGEMENT
Map Pointer
Activated to
Select Echo
Tops Data
HAZARD
AVOIDANCE
AFCS
Figure 6-16 Cloud Tops Weather Product
Displaying Cloud Tops information:
ADDITIONAL
FEATURES
1) Select the Weather Data Link (XM) Page with the FMS Knob.
2) Select the CLD TOP Softkey.
APPENDICES
To display the Cloud Tops legend, select the LEGEND Softkey when Cloud Tops is selected for display. Since Cloud Tops and Echo Tops use the same color scaling to represent altitude, display of these weather
products is mutually exclusive. When Cloud Tops is activated, the Echo Tops weather product is removed.
INDEX
Figure 6-17 Cloud Tops Legend
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
299
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
SIRIUSXM LIGHTNING
NOTE: The SiriusXM Lightning weather product and the optional Stormscope lightning information cannot
FLIGHT
INSTRUMENTS
be displayed at the same time.
AUDIO PANEL
& CNS
EIS
The SiriusXM Lightning weather product (Figure 6-18) shows the approximate location of cloud-to-ground
lightning strikes. A strike icon represents a strike that has occurred within a two-kilometer region. The exact
location of the lightning strike is not displayed.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Lightning
Strikes
Figure 6-18 SiriusXM Lightning Data
ADDITIONAL
FEATURES
AFCS
The SiriusXM Lightning weather product is available on the following maps:
• PFD Inset Map
• Nearest Pages
• Navigation Map Page
• Flight Plan Pages
• Weather Data Link (XM) Page
• AUX - Video Page
• Trip Planning Page
APPENDICES
Displaying SiriusXM Lightning information:
1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the
Weather Data Link (XM) Page.
2) Select the XM LTNG Softkey.
INDEX
To display the SiriusXM Lightning legend on the Weather Data Link (XM) Page, select the LEGEND Softkey
when SiriusXM Lightning is selected for display.
Figure 6-19 Lightning Legend
300
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
CELL MOVEMENT
FLIGHT
INSTRUMENTS
The Cell Movement weather product (Figure 6-20) shows the location and movement of storm cells as
identified by the ground-based system. Cells are represented by yellow squares, with direction of movement
indicated with short, orange arrows.
EIS
Storm Cell
Movement
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 6-20 Cell Movement Weather Product
HAZARD
AVOIDANCE
On most applicable maps, Cell Movement data is selected for display along with NEXRAD. On the Weather
Data Link (XM) Page, Cell Movement data can be selected independently. Cell Movement data can be
displayed on the following maps:
• Nearest Pages
• Navigation Map Page
• Flight Plan Pages
• Weather Data Link (XM) Page
• AUX - Video Page
AFCS
• PFD Inset Map
ADDITIONAL
FEATURES
• Trip Planning Page
Displaying Cell Movement information:
APPENDICES
1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the
Weather Data Link (XM) Page.
2) Select the NEXRAD Softkey (CEL MOV Softkey on the Weather Data Link (XM) Page). For Cell Movement to be
displayed on maps other than the Weather Data Link (XM) Page, Cell Movement must enabled in the Navigation
Map Setup Menu (see the procedure, “Setting up and customizing weather data for the Navigation Map Page”).
INDEX
To display the Cell Movement legend on the Weather Data Link (XM) Page, select the LEGEND Softkey
when Cell Movement is selected for display.
Figure 6-21 Cell Movement Legend
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
301
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
SIGMETS AND AIRMETS
FLIGHT
INSTRUMENTS
SIGMETs (SIGnificant METeorological Information) and AIRMETs (AIRmen’s METeorological Information)
are broadcast for potentially hazardous weather. A Convective SIGMET is issued for hazardous convective
weather. A localized SIGMET is a significant weather condition occurring at a localized geographical position.
EIS
Information
Window for
all SIGMETs
and AIRMETS
within Map
Pointer Area
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Convective
SIGMET
Selected with
Map Pointer
HAZARD
AVOIDANCE
Figure 6-22 SIGMET/AIRMET Data
Displaying SIGMETs and AIRMETs:
1) Select the Weather Data Link (XM) Page with the FMS Knob.
AFCS
2) Select the SIG/AIR Softkey.
3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move the Map Pointer over the icon.
4) Press the ENT key. The figure below shows a sample of SIGMET text.
INDEX
APPENDICES
ADDITIONAL
FEATURES
To display the SIGMET and AIRMET legend, select the LEGEND Softkey when SIGMETs and AIRMETs are
selected for display.
Sample SIGMET Text
SIGMET/AIRMET Legend
Figure 6-23 SIGMET/AIRMET Text and Legend
302
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
METARS AND TAFS
NOTE: Atmospheric pressure reported for METARs is given in hectopascals (hPa), except in the United
FLIGHT
INSTRUMENTS
States, where it is reported in inches of mercury (in Hg). Temperatures are reported in Celsius.
NOTE: METAR information is only displayed within the installed navigation database service area.
EIS
METARs (METeorological Aerodrome Reports) typically contain information about the temperature,
dewpoint, wind, precipitation, cloud cover, cloud heights, visibility, and barometric pressure at an airport or
observation station. They can also contain information on precipitation amounts, lightning, and other critical
data. METARs reflect hourly observations; non-routine updates include the code “SPECI” in the report. METARs are shown as colored flags at airports that provide them.
AUDIO PANEL
& CNS
Instructions
for Viewing
METAR and
TAF Text
FLIGHT
MANAGEMENT
Airport
Selected with
Map Pointer
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 6-24 METAR Flags on Weather Data Link (XM) Page
with Aiport Selected
APPENDICES
TAFs (Terminal Aerodrome Forecasts) are weather predictions for specific airports within a 24- hour period,
and may span a longer forecast period. TAFs typically include forecast wind, visibility, weather phenomena,
and sky conditions using METAR codes.
METAR and TAF text are displayed on the Weather Information Page. METAR data is displayed first in
a decoded fashion, then as raw text. TAF information is displayed only in its raw form when it is available
Displaying METAR and TAF text:
INDEX
1) On the Weather Data Link (XM) Page, select the METAR Softkey
2) Select the RANGE Knob and pan to the desired airport.
3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
303
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text is placed ahead of
the TAF text.
5) Press the FMS Knob or the CLR Key to return to the Weather Data Link (XM) Page.
FLIGHT
INSTRUMENTS
Or:
1) Select the Weather Information Page.
2) Select the WX Softkey to select the Weather Information Page.
3) Press the FMS Knob to display the cursor.
EIS
4) Using the FMS Knob, enter the desired airport and press the ENT Key.
AUDIO PANEL
& CNS
5) Scroll through the METAR and TAF text with the FMS Knob or the ENT Key. Scroll through all of the METAR
text to get to the TAF text.
FLIGHT
MANAGEMENT
Decoded (if
available)
and Raw
METAR Text
Displayed
HAZARD
AVOIDANCE
METAR Flag
AFCS
TAF
Displayed
as Raw Text
ADDITIONAL
FEATURES
Raw METAR text is also accessible while panning the map cursor over a METAR flag on any map page on
which a METAR is displayed. The METAR text is shown in a box near the METAR flag.
APPENDICES
Figure 6-25 METAR Flags on Weather Data Link (XM) Page
with Aiport Selected
In addition, METAR flags and their associated text are displayed on the Active Flight Plan Page on the MFD. METAR flags appears next to waypoints in the flight plan with an associated METAR. A METAR flag indicates
the METAR observations are available for a specific waypoint; a hollow METAR flag indicates an off-route
METAR near the waypoint is available.
Displaying raw METAR text on the Active Flight Plan Page:
INDEX
1) Select the Active Flight Plan Page on the MFD.
2) Press the FMS Knob to activate the cursor.
304
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
3) Turn the large FMS Knob to highlight the desired waypoint. The METAR text will appear in the ‘SELECTED
WAYPOINT WEATHER’ window below.
FLIGHT
INSTRUMENTS
4) When finished, press the FMS Knob to remove the cursor or press the FPL Key to exit the Active Flight Plan
Page.
To display the METAR legend on the Weather Data Link (XM) Page, select the LEGEND Softkey when
METARs are selected for display.
The METAR flag color is determined by the information in the METAR text. The METAR flag is gray when
the METAR text does not contain adequate information.
EIS
AUDIO PANEL
& CNS
Figure 6-26 METAR Legend
FLIGHT
MANAGEMENT
SURFACE ANALYSIS AND CITY FORECAST
NOTE: Surface Analysis and City Forecast data are displayed only within the installed navigation database
service area.
HAZARD
AVOIDANCE
The Surface Analysis and City Forecast weather products (Figure 6-27) are available for current and forecast
weather conditions. Forecasts are available for intervals of 12, 24, 36, and 48 hours.
AFCS
ADDITIONAL
FEATURES
APPENDICES
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
INDEX
Figure 6-27 Surface Analysis and City Forecast (12 Hour Forecast Selected)
305
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Displaying Surface Analysis and City Forecast information:
1) Select the Weather Data Link (XM) Page with the FMS Knob.
FLIGHT
INSTRUMENTS
2) Select the MORE WX Softkey.
3) Select the SFC Softkey.
4) Select the forecast time: CURRENT, 12 HR, 24 HR, 36 HR, or 48 HR. The SFC Softkey label changes to reflect
the forecast time selected.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
To display the Surface Analysis and City Forecast legend, select the LEGEND Softkey when Surface Analysis
and City Forecast are selected for display.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 6-28 Surface Analysis
and City Forecast Legend
306
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
FREEZING LEVEL
FLIGHT
INSTRUMENTS
The Freezing Level weather product (Figure 6-29) shows the color-coded contour lines for the altitude and
location at which the first isotherm is found. When no data is displayed for a given altitude, the data for that
altitude has not been received, or is out of date and has been removed from the display. New data appears at
the next update.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 6-29 Freezing Level Data
Displaying Freezing Level information:
1) Select the Weather Data Link (XM) Page with the FMS Knob.
AFCS
2) Select the MORE WX Softkey.
3) Select the FRZ LVL Softkey.
ADDITIONAL
FEATURES
To display the Freezing Level legend (Figure 6-30), select the LEGEND Softkey when Freezing Level data
is selected to be displayed.
APPENDICES
Figure 6-30 Freezing Level Legend
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
307
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
WINDS ALOFT
FLIGHT
INSTRUMENTS
The Winds Aloft weather product (Figure 6-31) shows the forecast wind speed and direction at the surface
and at selected altitudes. Altitude can be displayed in 3000-foot increments up to 42,000 feet MSL.
Displaying Winds Aloft data:
1) Select the Weather Data Link (XM) Page with the FMS Knob.
2) Select the MORE WX Softkey.
3) Select the WIND Softkey.
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Select the NEXT or PREV Softkey to cycle
through the altitude softkeys. The WIND Softkey label changes to reflect the altitude selected.
Figure 6-31 WInds Aloft Weather Product (15,000’ Selected)
APPENDICES
ADDITIONAL
FEATURES
To display the Winds Aloft legend (Figure 6-32), select the LEGEND Softkey when Winds Aloft is selected
for display.
INDEX
Figure 6-32 Winds Aloft Data with Legend
308
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Headwind and tailwind components aloft are available inside the Profile View on the Navigation Map Page (Figure 6-33). The displayed components are relative to current aircraft altitude and track, but not to aircraft
speed.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Winds Aloft Data Age
Altitude Scale
FLIGHT
MANAGEMENT
Wind Component
Velocity and Direction
Arrow
Figure 6-33 Navigation Map Page with Winds Aloft Data on
Profile View
HAZARD
AVOIDANCE
Arrows pointing to the left indicate headwind components; tailwind component arrows point to the right,
as shown in Table 6-3.
Tailwind
Symbol
Headwind/Tailwind
Component
None
None
Less than 5 knots
AFCS
Headwind
Symbol
5 knots
ADDITIONAL
FEATURES
10 knots
50 knots
APPENDICES
Table 6-3 Profile View Headwind/Tailwind Component Symbols
Showing/Hiding Profile View (containing winds aloft data)
1) Select the Navigation Map Page.
INDEX
2) Select the MAP Softkey.
3) Select the PROFILE Softkey.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
309
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Or:
1) Press the MENU Key.
FLIGHT
INSTRUMENTS
2) Turn the large FMS Knob to highlight ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on current
state) and press the ENT Key.
Winds Aloft data inside the Profile View is enabled by default when the Profile View is displayed on the
Navigation Map Page. This behavior can be changed on the Navigation Map Page.
Enabling/disabling winds aloft data display in Profile View:
EIS
1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With Map Setup highlighted, press the ENT Key (Figure 6-34).
AUDIO PANEL
& CNS
4) Turn the small FMS Knob to select the Profile Group and press the ENT Key (Figure 6-35).
5) Turn the large FMS Knob to select ‘Profile Winds’ (Figure 6-36).
6) Turn the small FMS Knob to select ‘On’ or ‘Off’.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
7) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 6-34 Navigation Map Page Menu
Figure 6-36 Navigation Map Page Setup Menu, Weather Group
INDEX
Figure 6-35 Navigation Map Page Setup Menu
310
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
COUNTY WARNINGS
FLIGHT
INSTRUMENTS
The County Warnings weather product (Figure 6-37) provides specific public awareness and protection
weather warnings from the National Weather Service (NWS). This can include information on severe
thunderstorms, tornadoes, and flood conditions.
EIS
Flood
Warning
Selected
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 6-37 County Warnings Weather Product
Displaying County Warning information:
1) Select the Weather Data Link (XM) Page with the FMS Knob.
AFCS
2) Select the MORE WX Softkey.
3) Select the COUNTY Softkey.
ADDITIONAL
FEATURES
To display the County Warnings legend (Figure 6-38), select the LEGEND Softkey when County Warnings
are selected to be displayed.
APPENDICES
Figure 6-38 County Warnings Legend
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
311
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
CYCLONE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
The Cyclone weather product (Figure 6-39) shows the current location of cyclones (hurricanes), tropical
storms, and their projected tracks.
Figure 6-39 Cyclone (Hurricane) Data with Track Information
HAZARD
AVOIDANCE
Displaying cyclone (hurricane) track information:
1) Select the Weather Data Link (XM) Page with the FMS Knob.
2) Select the MORE WX Softkey.
3) Select the CYCLONE Softkey.
ADDITIONAL
FEATURES
AFCS
To display the Cyclone legend (Figure 6-40), select the LEGEND Softkey when Cyclones are selected to
be displayed.
INDEX
APPENDICES
Figure 6-40 Cyclone Legend
312
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
ICING (CIP & SLD)
FLIGHT
INSTRUMENTS
Current Icing Product (CIP) data (Figure 6-41) shows a graphical view of the icing environment. Icing
severity is displayed in four categories: light, moderate, severe, and extreme (not specific to aircraft type). The
CIP product is not a forecast, but a presentation of the current conditions at the time of the analysis.
Supercooled Large Droplet (SLD) icing conditions are characterized by the presence of relatively large,
super cooled water droplets indicative of freezing drizzle and freezing rain aloft. SLD threat areas are depicted
as magenta dots over the CIP colors.
Displaying Icing data:
EIS
1) Select the Weather Data Link (XM) Page.
2) Select the MORE WX Softkey.
AUDIO PANEL
& CNS
3) Select the ICNG Softkey.
4) Select the desired altitude level: 1,000 feet up to 30,000 feet. Select the NEXT or PREV Softkey to cycle through
the altitude softkeys. The ICNG Softkey label changes to reflect the altitude selected.
FLIGHT
MANAGEMENT
Current
Icing
Potential
HAZARD
AVOIDANCE
SLD Threat
Area
AFCS
ADDITIONAL
FEATURES
Figure 6-41 Icing Data at 15,000 Feet
APPENDICES
To display the Icing Potential legend (Figure 6-42), select the LEGEND Softkey when Icing is selected for
display.
INDEX
Figure 6-42 Icing Potential Legend
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
313
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
TURBULENCE
FLIGHT
INSTRUMENTS
The Turbulence weather product (Figure 6-43) identifies the potential for erratic movement of high-altitude
air mass associated winds. Turbulence is classified as light, moderate, severe or extreme, at altitudes between
21,000 and 45,000 feet. Turbulence data is intended to supplement AIRMETs and SIGMETs.
Displaying Turbulence data:
1) Select the Weather Data Link (XM) Page.
2) Select the MORE WX Softkey.
EIS
3) Select the TURB Softkey.
AUDIO PANEL
& CNS
4) Select the desired altitude level: 21,000 feet up to 45,000 feet. Select the NEXT or PREV Softkey to cycle
through the altitude softkeys. The TURB Softkey label changes to reflect the altitude selected.
FLIGHT
MANAGEMENT
Light
Turbulence
AFCS
HAZARD
AVOIDANCE
Moderate
Turbulence
ADDITIONAL
FEATURES
Figure 6-43 Turbulence Data at 21,000 Feet
APPENDICES
To display the Turbulence legend (Figure 6-44), select the LEGEND Softkey when Turbulence is selected for
display.
INDEX
Figure 6-44 Turbulence Legend
314
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
PIREPS AND AIREPS
FLIGHT
INSTRUMENTS
Pilot Weather Reports (PIREPs) (Figure 6-45) provide in-flight weather observations collected from pilots. When significant weather conditions are reported or forecast, Air Traffic Control (ATC) facilities are required
to solicit PIREPs. A PIREP may contain adverse weather conditions, such as low in-flight visibility, icing
conditions, wind shear, and turbulence. PIREPs are issued as either Routine (UA) or Urgent (UUA).
Another type of PIREP is an Air Report (AIREP). AIREPs are used almost exclusively by commercial airlines.
Instructions for
Viewing Report
Text
EIS
AIREP
AUDIO PANEL
& CNS
Urgent PIREP
Selected with
Map Pointer
FLIGHT
MANAGEMENT
Routine PIREP
HAZARD
AVOIDANCE
Figure 6-45 PIREPs and AIREPs on the Weather Data Link (XM) Page
Displaying PIREP and AIREP text:
AFCS
1) Select the Weather Data Link (XM) Page.
2) Select the MORE WX Softkey.
ADDITIONAL
FEATURES
3) Select the AIREPS or PIREPS Softkey.
4) Press the RANGE Knob and pan to the desired weather report. A gray circle will appear around the weather
report when it is selected.
APPENDICES
5) Press the ENT Key. The Weather Information Page is shown with PIREP or AIREP text. The data is first displayed
in a decoded fashion, then as raw text. Note the raw text may contain additional information not found in the
decoded version.
6) Use the FMS Knob or the ENT Key to scroll through the PIREP or AIREP text.
7) Press the FMS Knob or the CLR Key to return to the Weather Data Link (XM) Page.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
315
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
EIS
Decoded Urgent
PIREP Text
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Raw PIREP Text
HAZARD
AVOIDANCE
Figure 6-46 Urgent PIREP Text Information Window on
the Weather Data Link (XM) Page
To display the PIREP or AIREP legend (Figure 6-47), select the LEGEND Softkey when PIREPs or AIREPs are selected for display.
ADDITIONAL
FEATURES
AFCS
The PIREP color is determined by the type (routine or urgent).
INDEX
APPENDICES
Figure 6-47 AIREPs & PIREPs Legend
316
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
TFRS
NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information.
FLIGHT
INSTRUMENTS
Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control.
The Federal Aviation Administration (FAA) issues Temporary Flight Restrictions (TFRs) to designate areas
where flight is restricted. TFRs are issued to restrict flight for a variety of reasons including national security,
law enforcement, fire control, natural disasters., airshows, and large sporting events. TFRs may be issued at
any time.
EIS
The age of TFR product is not shown; however, if TFR information is not available or has expired, the
system displays ‘TFR N/A’ in the upper-left corner of maps on which TFRs can be displayed.
AUDIO PANEL
& CNS
TFR Summary
Information
FLIGHT
MANAGEMENT
TFR Selected
with Map
Pointer
HAZARD
AVOIDANCE
AFCS
Figure 6-48 TFR Data on the Weather Data Link (XM) Page
Displaying TFR Data:
ADDITIONAL
FEATURES
1) Select the Weather Data Link (XM) Page or Navigation Map Page.
2) Press the RANGE Knob and pan the map pointer over a TFR to highlight it. The system displays TFR summary
information above the map.
APPENDICES
3) Press the ENT Key. The system displays a pop-up menu.
4) If necessary, turn the FMS Knob to select ‘Review Airspaces’ and press the ENT Key. The system displays the
TFR Information window.
5) Press the FMS Knob or the CLR Key to remove the TFR Information window.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
317
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Figure 6-49 Full Text for Selected TFR
EIS
The setup menus for the Navigation Map Page control the map range settings above which TFR data is
decluttered from the display. If a map range larger than the TFR product map range setting is selected, the TFR
product data is removed from the map.
AUDIO PANEL
& CNS
Maps other than the Navigation Map Page use settings based on those selected for the Navigation Map Page.
Setting up and customizing TFR data for maps on which TFR data can be displayed:
1) Select the Navigation Map Page.
FLIGHT
MANAGEMENT
2) Press the MENU Key.
3) With Map Setup highlighted, press the ENT Key (Figure 6-50).
4) Turn the small FMS Knob to select the Aviation Group and press the ENT Key (Figure 6-51).
5) Turn the large FMS Knob to scroll to the TFR product range setting (Figure 6-52).
HAZARD
AVOIDANCE
6) Turn the small FMS Knob to scroll through options (Off, range settings).
7) Press the ENT Key to select an option.
ADDITIONAL
FEATURES
AFCS
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
INDEX
APPENDICES
Figure 6-50 Navigation Map Page Menu
Figure 6-51 Navigation Map Page Setup Menu
318
Figure 6-52 Navigation Map Page Setup Menu, Aviation Group
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
6.2 STORMSCOPE LIGHTNING
FLIGHT
INSTRUMENTS
WARNING: Do not rely on information from the lightning detection system display as the sole basis for
hazardous weather avoidance. Range limitations and interference may cause the system to display inaccurate
or incomplete information. Refer to documentation from the lightning detection system manufacturer for
detailed information about the system.
NOTE: Stormscope lightning information cannot be displayed at the same time as the SiriusXM Lightning
EIS
weather product.
The following pages can display Stormscope lightning information.
• AUX - Video Page
• Nearest Pages
AUDIO PANEL
& CNS
• Stormscope Page
• Navigation Map
• AUX - Trip Planning Page
FLIGHT
MANAGEMENT
To display Stormscope data on the Navigation Map, AUX - Trip Planning Page, AUX - Video Page, or any of the
Nearest Pages, press the MAP Softkey, then press the STRMSCP Softkey. These pages can also display cell or strike
data using the yellow lightning strike symbology shown in Table 6-4.
HAZARD
AVOIDANCE
AFCS
Table 6-4 Lightning Age and Symbols
SETTING UP STORMSCOPE ON THE NAVIGATION MAP
ADDITIONAL
FEATURES
Setting up Stormscope options on the Navigation Map:
1) On the Navigation Map Page, press the MENU Key.
2) With ‘Map Setup’ selected (Figure 6-53), press the ENT Key.
APPENDICES
3) Turn the small FMS Knob to display the group selection window. Turn the small FMS Knob to select ‘Weather’),
and press the ENT Key.
4) Turn the large FMS Knob to highlight and move between the product selections.
5) When an item is highlighted, turn the small FMS Knob to select the option.
INDEX
6) Press the ENT Key.
7) Press the FMS Knob to return to the Navigation Map Page (Figure 6-55).
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
319
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
The following options are available (Figure 6-54):
• STRMSCP LTNG – Turns the display of Stormscope data on or off.
FLIGHT
INSTRUMENTS
• STRMSCP MODE – Selects the CELL or STRIKE mode of lightning activity. Cell mode identifies clusters or
cells of electrical activity. Strike mode indicates the approximate location of lightning strikes.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
• STRMSCP SMBL – Selects the range at which Stormscope data displays. Stormscope data is removed when
a map range greater than the STRMSCP SMBL value is selected.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Figure 6-53 Navigation Map Page Menu
INDEX
Figure 6-54 Map Setup Menu
320
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
CELL AND STRIKE MODE ON THE NAVIGATION MAP
FLIGHT
INSTRUMENTS
On the Navigation Map, cell mode identifies cells of lightning activity (Figure 6-55). Stormscope identifies
clusters of electrical activity that indicate cells. Strike mode indicates the approximate location of lightning
strikes.
Selecting the ‘cell’ or ‘strike’ mode on the Navigation Map:
1) Press the MENU Key.
2) With ‘Map Setup’ selected, press the ENT Key.
EIS
3) Select the ‘Weather’ group.
4) Press the ENT Key. The cursor flashes on ‘STRMSCP LTNG’.
5) Turn the large FMS Knob to select ‘STRMSCP MODE’.
AUDIO PANEL
& CNS
6) Turn the small FMS Knob to change between ‘CELL’ and ‘STRIKE’ options. When an item is selected, press the
ENT Key.
7) Press the FMS knob to return to the Navigation Map Page.
FLIGHT
MANAGEMENT
Lightning
Strikes
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Stormscope
Enabled
APPENDICES
Figure 6-55 Navigation Map Page with
Stormscope Lightning Data
If heading input is lost, strikes and/or cells must be cleared manually after the execution of each turn. This
is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
321
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Manually clearing Stormscope data on the Navigation Map:
1) Press the MENU Key.
FLIGHT
INSTRUMENTS
2) Select ‘Clear Stormscope® Lightning’.
AUDIO PANEL
& CNS
EIS
3) Press the ENT Key.
FLIGHT
MANAGEMENT
Figure 6-56 Navigation Map Page Options Menu
ZOOM RANGE ON THE NAVIGATION MAP
HAZARD
AVOIDANCE
Stormscope lightning data can be displayed up to 800 nm zoom range (in North up mode) on the Navigation
Map Page. However, in the track up mode at the 500 nm range, a portion of Stormscope lightning data
can be behind the aircraft and therefore not visible on the Navigation Map. Since the range for Stormscope
data is 400 nm diameter total (200 nm in front and 200 nm behind), the 500 nm range in North up mode
shows all the data.
At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present.
AFCS
The maximum zoom range can also be set on the Navigation Map. Note that Stormscope data above the
selected maximum zoom range is decluttered.
Selecting a Stormscope range on the Navigation Map:
ADDITIONAL
FEATURES
1) Press the MENU Key.
2) Select ‘MAP SETUP’.
3) Select the ‘Weather’ group.
4) Press the ENT Key.
APPENDICES
5) Turn the large FMS Knob to select ‘STRMSCP SMBL’.
6) Turn the small FMS Knob to select the maximum display range.
7) Press the ENT Key.
8) Press the FMS Knob to return to the Navigation Map Page.
INDEX
To change the display range on the Navigation Map Page, turn the RANGE Knob clockwise to zoom out or
counter-clockwise to zoom in.
322
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
SELECTING THE STORMSCOPE PAGE
Stormscope lightning data can be displayed at the ranges of 25 nm, 50 nm, 100 nm, and 200 nm.
FLIGHT
INSTRUMENTS
Adjusting the Stormscope Map Range:
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Stormscope Page.
3) To change the map range, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 6-57 Stormscope Page
AFCS
Changing between ‘cell’ and ‘strike’ mode on the Stormscope Page:
1) Select the Stormscope Page.
ADDITIONAL
FEATURES
2) Press the MODE Softkey. The CELL and STRIKE softkeys are displayed.
3) Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey to display ‘STRIKE’ data. ‘CELL’ or
‘STRIKE’ is displayed in the mode box in the upper left corner of the Stormscope Page.
4) Press the BACK Softkey to return to the main Stormscope page.
APPENDICES
Changing the viewing mode between 360˚ and 120˚ on the Stormscope Page:
1) Select the Stormscope Page.
2) Press the VIEW Softkey. The 360 and ARC softkeys are displayed. Press the 360 Softkey to display a 360˚
viewing area or press the ARC Softkey to display a 120˚ viewing area.
INDEX
3) Press the BACK Softkey to return to the main Stormscope page.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
323
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
6.3 TERRAIN PROXIMITY
FLIGHT
INSTRUMENTS
WARNING: Do not use Terrain Proximity information for primary terrain avoidance. Terrain Proximity is
intended only to enhance situational awareness.
NOTE: Terrain data is not displayed when the aircraft is outside of the terrain database coverage area.
AUDIO PANEL
& CNS
EIS
G1000 Terrain Proximity is a terrain awareness system that does not comply with TSO-C151b certification
standards. It increases situational awareness and aids in reducing controlled flight into terrain (CFIT). Do not
confuse Terrain Proximity with the optional Terrain Awareness and Warning System - Class B (TAWS-B). TAWS-B
is more sophisticated and robust, and it is TSO-C151b certified. Terrain Proximity does not provide warning annunciations or voice alerts. It only provides color indications on map displays when terrain and obstacles are
within a certain altitude threshold from the aircraft. Although the terrain and obstacle color map displays are the
same, TAWS-B uses more sophisticated algorithms to assess aircraft distance from terrain and obstacles.
Terrain Proximity requires the following components to operate properly:
FLIGHT
MANAGEMENT
• Valid 3-D GPS position
• Valid terrain/obstacle database
HAZARD
AVOIDANCE
Terrain Proximity displays altitudes of terrain and obstructions relative to the aircraft position and altitude with
reference to a database that may contain inaccuracies. Terrain and obstructions are shown only if they are in the
database. Terrain and obstacle information should be used as an aid to situational awareness. They should never
be used to navigate or maneuver around terrain.
Note that all obstructions may not be available in the terrain and obstacle database. No terrain and obstacle
information is shown without a valid 3-D GPS position.
ADDITIONAL
FEATURES
AFCS
The G1000 GPS receiver provides the horizontal position and altitude. GPS altitude is derived from satellite
position. GPS altitude is then converted to the height above geodetic sea level (GSL), which is the height above
mean sea level calculated geometrically. GSL altitude is used to determine terrain and obstacle proximity. GSL
altitude accuracy is affected by satellite geometry, but is not subject to variations in pressure and temperature that
normally affect pressure altitude sensors. GSL altitude does not require local altimeter settings to determine MSL
altitude. It is a widely-used MSL altitude source.
APPENDICES
Terrain and obstacle databases are referenced to MSL. Using the GPS position and altitude, the Terrain Proximity
feature portrays a 2-D picture of the surrounding terrain and obstacles relative to the position and altitude of the
aircraft. GPS position and GSL altitude are used to calculate and predict the aircraft’s flight path in relation to
the surrounding terrain and obstacles. In this way, the pilot can view predicted dangerous terrain and obstacle
conditions.
DISPLAYING TERRAIN PROXIMITY INFORMATION
INDEX
The symbols and colors in Figure 6-58 and Table 6-5 are used to represent obstacles and aircraft altitude when the Terrain Proximity Page is selected for display. Terrain Proximity uses black, yellow, and red to
represent terrain information relative to aircraft altitude. The color of each obstacle is associated with the
altitude of the aircraft.
324
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Terrain Above Aircraft Altitude
Red terrain is above
or within 100 ft below
the aircraft altitude
Aircraft Altitude
100 ft Threshold
FLIGHT
INSTRUMENTS
1000 ft
Yellow terrain is between 100 ft and 1000 ft below the aircraft altitude
Black terrain is more than 1000 ft below the aircraft altitude
EIS
Figure 6-58 Terrain Altitude/Color Correlation for Terrain Proximity
AUDIO PANEL
& CNS
Unlighted Obstacle
Lighted Obstacle
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL
Obstacle Location
FLIGHT
MANAGEMENT
Red obstacle is above or within 100 ft
below the aircraft altitude
Yellow obstacle is between 100 ft and
1000 ft below the aircraft altitude
HAZARD
AVOIDANCE
Table 6-5 Terrain Proximity Terrain/Obstacle Colors and Symbology
Terrain and obstacle information can be displayed on the following pages:
• Trip Planning Page
• Navigation Map Page
• Flight Plan Page
• Terrain Proximity Page
• AUX - Video Page
AFCS
• PFD Inset Map
Displaying terrain and obstacle information (maps other than the Terrain Proximity Page):
1) Select the MAP Softkey (for the PFD Inset Map, press the INSET Softkey).
ADDITIONAL
FEATURES
2) Select the TERRAIN Softkey to display terrain and obstacle data.
When Terrain Proximity is selected on maps other than the Terrain Proximity Page, an icon to indicate the
feature is enabled for display and a legend for Terrain Proximity colors are shown (Figure 6-62).
APPENDICES
The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling
display of terrain and obstacles. The setup menu also controls the map range settings above which terrain and
obstacle data are decluttered from the display. If a map range larger than the map range setting is selected, the
data is removed from the map.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
INDEX
Terrain data can be selected for display independently of obstacle data; however, obstacles recognized by
Terrain Proximity as yellow or red are shown when terrain is selected for display and the map range is within
the setting limit.
325
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
FLIGHT
INSTRUMENTS
Maps besides the Terrain Proximity Page use settings based on those selected for the Navigation Map Page. The maximum display ranges for obstacles on each map are dependent on the range setting made for the
Navigation Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20
nm, the highest obstacle display range settings on the other applicable maps are also adjusted proportionally.
CAUTION: Terrain and obstacle data will not be displayed when the Navigation Map range is larger than
the MAP SETUP range setting for TERRAIN DATA and OBSTACLE DATA.
Customizing terrain and obstacle display on the Navigation Map Page:
EIS
1) Select the Navigation Map Page.
2) Press the MENU Key.
AUDIO PANEL
& CNS
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-59).
4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-60).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-61).
• TERRAIN DATA – Turns the display of terrain data on or off and sets maximum range at which terrain is shown
FLIGHT
MANAGEMENT
• OBSTACLE DATA – Turns the display of obstacle data on or off and sets maximum range at which obstacles are shown
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
7) Press the ENT Key to select an option.
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
INDEX
APPENDICES
Figure 6-59 Navigation Map Page Menu
Figure 6-60 Navigation Map Page Setup Menu
326
Figure 6-61 Navigation Map Page Setup Menu, Map Group
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Additional information about obstacles can be displayed by panning over the display on the map. The map
panning feature is enabled by pressing the RANGE Knob. The map range is adjusted by turning the RANGE
Knob. If the map range is adjusted while panning is enabled, the map is re-centered on the Map Pointer.
FLIGHT
INSTRUMENTS
Additional
Information on
Obstacle Selected
with Map Pointer
Red Terrain Area
(Above or Within
100’ Below Aircraft
Altitude)
EIS
Lighted Obstacle
Selected with Map
Pointer
FLIGHT
MANAGEMENT
Red Lighted
Obstacles
(Above or Within
100’ Below Aircraft
Altitude)
AUDIO PANEL
& CNS
Yellow Terrain Area
(Between 100’ and
1000’ Below Aircraft
Altitude)
Terrain Display
Enabled Icon
Terrain Legend
HAZARD
AVOIDANCE
Figure 6-62 Terrain Information on the Navigation Map Page
TERRAIN PROXIMITY PAGE
AFCS
The Map - Terrain Proximity Page is specialized to show terrain and obstacle data in relation to the aircraft’s
current altitude, without clutter from the basemap. It is the principal map page for viewing Terrain Proximity
information. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference.
ADDITIONAL
FEATURES
Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are
available relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map range is adjustable with the RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or
arcs).
Displaying the Terrain Proximity Page:
1) Turn the large FMS Knob to select the Map Page Group.
APPENDICES
2) Turn the small FMS Knob to select the Terrain Proximity Page.
3) To change the view:
a) Press the VIEW Softkey.
b) Press the 360 or ARC Softkey to select the desired view.
INDEX
Or:
a) Press the MENU Key.
b) Select ‘View Arc’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
327
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Showing/hiding aviation information on the Terrain Proximity Page:
1) Press the MENU Key.
FLIGHT
INSTRUMENTS
2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key.
Map Orientation
Current Aircraft
GPS-derived GSL
Altitude
Red Terrain
(Above or Within
100’ Below the
Aircraft Altitude)
EIS
Map Range Rings
Black Terrain
(More than 1000’
Below the Aircraft
Altitude)
AUDIO PANEL
& CNS
Red Lighted Obstacle
(Above or Within
100’ Below Aircraft
Altitude)
Yellow Terrain
(Between 100’
and 1000’ Below
the Aircraft
Altitude)
FLIGHT
MANAGEMENT
Yellow Lighted
Obstacles (Between
100’ and 1000’ Below
Aircraft Altitude)
Terrain Legend
HAZARD
AVOIDANCE
Figure 6-63 Terrain Proximity Page
Map Orientation
Current Aircraft
GPS-derived GSL
Altitude
AFCS
Red Terrain
(Above or Within
100’ Below the
Aircraft Altitude)
APPENDICES
ADDITIONAL
FEATURES
Map Range Arc
Yellow Terrain
(Between 100’ and
1000’ Below the
Aircraft Altitude)
Black Terrain
(Terrain More
than 1000’ Below
the Aircraft
Altitude)
Red Lighted Obstacle
(Above or Within
100’ Below Aircraft
Altitude)
Terrain Legend
INDEX
Figure 6-64 Terrain Proximity Page (ARC View)
328
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
6.4 PROFILE VIEW TERRAIN
FLIGHT
INSTRUMENTS
WARNING: Do not use Profile View Terrain data for primary terrain avoidance. Profile View Terrain is intended
only to enhance situational awareness.
NOTE: Terrain data is not displayed when the aircraft is outside of the installed terrain database coverage
area.
EIS
The G1000 offers a Profile View of terrain and obstacles relative to the aircraft’s current flight path and altitude
on the Navigation Map Page of the MFD. Profile View does not provide terrain or obstacle caution or warning
annunciations or voice alerts, nor does it display potential impact points inside the Profile View. The colors
and symbols used to represent terrain and obstacles are the same as those used in Terrain Proximity discussed
previously.
AUDIO PANEL
& CNS
Accessing Profile View:
1) Select the Navigation Map Page.
FLIGHT
MANAGEMENT
2) Select the MAP Softkey.
3) Select the PROFILE Softkey to enable or disable Profile View.
Or:
1) Press the MENU Key.
HAZARD
AVOIDANCE
2) Select ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on current state) and press the ENT Key.
Enabling/Disabling Profile View Terrain on the Navigation Map (when Profile View is enabled):
1) Select the Navigation Map Page.
2) Select the MAP Softkey.
AFCS
3) Select the TERRAIN Softkey.
PROFILE VIEW DISPLAY
ADDITIONAL
FEATURES
When the Profile View is enabled, it is displayed in a window below the Navigation Map. Altitude is shown
along a vertical scale, with an aircraft icon positioned at the current altitude. Distance is represented horizontally
along the bottom of the Profile View, and increases from left (present position) to right.
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
INDEX
190-00552-05 Rev. A
APPENDICES
When the Navigation Map range is adjusted with the RANGE Knob, the horizontal distance of the Profile
View is adjusted proportionately to be 1/2 of the Navigation Map range distance down to 1 nm, at which point
Profile View is no longer available (‘PROFILE NOT AVAILABLE’ is displayed). When Navigation Map range
is adjusted to remove altitude-correlated colored terrain data (as shown in the Terrain Legend) or obstacles
from the Navigation Map, these items are also removed from the Profile View; only an outline of the terrain
will be displayed in black in the Profile View window. Refer to the Terrain Proximity, Terrain-SVS, or TAWS-B
discussions for more information about displaying terrain or obstacles on the Navigation Map Page.
329
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Profile View
Path Enabled
Navigation Map Range
EIS
Terrain Legend
AUDIO PANEL
& CNS
Altitude Scale
Profile View Length
is One Half of the
Navigation Map
Range
FLIGHT
MANAGEMENT
Distance Scale
Figure 6-65 Profile View on Navigation Map with Terrain Display Enabled
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
The Profile View is based on the current aircraft track (or heading if track is unavailable) and shows the highest
known terrain or obstacles within a predetermined width from the present aircraft position to the end of the
profile range. The width of the Profile View (Table 6-6) is determined by the phase of flight, as annunciated on
the HSI. Refer to the Flight Instruments section for more information about flight phases.
Flight Phase
Total Profile View Width
Approach
0.6 nm
Departure
0.6 nm
Terminal
2.0 nm
Enroute
4.0 nm
Oceanic
4.0 nm
APPENDICES
Table 6-6 Profile View Width Scale
PROFILE PATH
INDEX
The Profile Path displays the horizontal and lateral boundaries of the Profile View. The path is shown
as a white rectangle on the Navigation Map Page (Figure 6-65) and is only available when Profile View is
enabled. White range markers appearing inside the Profile Path rectangle match the range markers along the
distance scale inside the Profile View display window whenever the profile range is at least 4 nm (or 7.5 km
if configured for metric units).
330
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
The Profile Path rectangle may enabled or disabled, and the Navigation Map range at which the Profile Path
is removed from map display can be changed.
Customizing the Profile Path display on the Navigation Map Page:
FLIGHT
INSTRUMENTS
1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-66).
4) Turn the small FMS Knob to select the ‘Profile’ Group and press the ENT Key (Figure 6-67).
EIS
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-68).
• PROFILE PATH – Turns the display of the Profile Path on or off and sets maximum map range at which the Profile
Path is shown
AUDIO PANEL
& CNS
6) Turn the small FMS Knob to scroll through options (ON/OFF, range settings).
7) Press the ENT Key to select an option.
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 6-66 Navigation Map Page Menu
AFCS
ADDITIONAL
FEATURES
APPENDICES
Figure 6-67 Navigation Map Page Setup Menu
Figure 6-68 Navigation Map Page Setup Menu,
Profile Group
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
331
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
6.5 TERRAIN-SVS
FLIGHT
INSTRUMENTS
NOTE: Terrain data is not displayed when the aircraft is outside of the installed terrain database coverage
EIS
WARNING: Do not use Terrain-SVS information for primary terrain avoidance. Terrain-SVS is intended only
NOTE: Terrain-SVS is standard when the Synthetic Vision System (SVS) option is installed. The TAWS-B
to enhance situational awareness.
area.
AUDIO PANEL
& CNS
Terrain-SVS is a terrain awareness system available with the Synthetic Vision System (SVS). SVS functionality
is offered as an optional enhancement. The optional Terrain Awareness and Warning System - Class B (TAWS-B)
or standard Terrain-SVS is integrated within SVS to provide visual and auditory alerts to indicate the presence
of threatening terrain relevant to the projected flight path. For detailed information regarding SVS, refer to the
Additional Features section of this Pilot’s Guide.
FLIGHT
MANAGEMENT
option will take precedence over Terrain-SVS.
Terrain-SVS does not comply with TSO-C151b certification standards. It increases situational awareness and
aids in reducing controlled flight into terrain (CFIT). Do not confuse Terrain-SVS with TAWS-B. TAWS-B is more
sophisticated and robust, and it is TSO-C151b certified. Although the terrain and obstacle color map displays
are the same, TAWS-B uses more sophisticated algorithms to assess aircraft distance from terrain and obstacles.
HAZARD
AVOIDANCE
Terrain-SVS does not provide the following:
• Premature Descent Alerting (PDA)
• Excessive Descent Rate (EDR)
• Negative Climb Rate (NCR)
AFCS
• Descent to 500 Feet Callout (DFC)
Terrain-SVS requires the following components to operate properly:
• Valid 3-D GPS position
ADDITIONAL
FEATURES
• Valid terrain/airport terrain/obstacle database
APPENDICES
Terrain-SVS displays altitudes of terrain and obstructions relative to the aircraft position and altitude with
reference to a database that may contain inaccuracies. Terrain and obstructions are shown only if they are in the
database. Terrain and obstacle information should be used as an aid to situational awareness. They should never
be used to navigate or maneuver around terrain.
Note that all obstructions may not be available in the terrain and obstacle database. No terrain and obstacle
information is shown without a valid 3-D GPS position.
INDEX
The G1000 GPS receiver provides the horizontal position and altitude. GPS altitude is derived from satellite
position. GPS altitude is then converted to the height above geodetic sea level (GSL), which is the height above
mean sea level calculated geometrically. GSL altitude is used to determine terrain and obstacle proximity. GSL
altitude accuracy is affected by satellite geometry, but is not subject to variations in pressure and temperature that
332
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
normally affect pressure altitude sensors. GSL altitude does not require local altimeter settings to determine MSL
altitude. It is a widely-used MSL altitude source.
FLIGHT
INSTRUMENTS
Terrain and obstacle databases are referenced to MSL. Using the GPS position and altitude, the Terrain-SVS
feature portrays a 3-D picture of the surrounding terrain and obstacles relative to the position and altitude of the
aircraft. GPS position and GSL altitude are used to calculate and predict the aircraft’s flight path in relation to
the surrounding terrain and obstacles. In this way, the pilot can view predicted dangerous terrain and obstacle
conditions.
DISPLAYING TERRAIN-SVS INFORMATION
EIS
Terrain-SVS uses yellow (caution) and red (warning) to depict terrain and obstacles (with heights greater than
200 feet above ground level, AGL) alerts relative to aircraft altitude. Colors are adjusted automatically as the
aircraft altitude changes. The colors and symbols in Figure 6-69 and Tables 6-7 and 6-8 are used to represent
terrain, obstacles, and potential impact points.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 6-69 Terrain Altitude/Color Correlation for Terrain-SVS
Obstacle Location
AFCS
Unlighted Obstacle
Lighted Obstacle
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL
Red obstacle is above or within 100 ft
below the aircraft altitude
ADDITIONAL
FEATURES
Yellow obstacle is between 100 ft and
1000 ft below the aircraft altitude
Potential Impact
Point Symbol
Alert Type
APPENDICES
Table 6-7 Terrain-SVS Obstacle Colors and Symbology
Example Annunciation
INDEX
Warning
Caution
Table 6-8 Terrain-SVS Potential Impact Point Symbols with Alert Types
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
333
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
FLIGHT
INSTRUMENTS
Terrain-SVS information can be displayed on the following maps:
• PFD Inset Map
• Trip Planning Page
• Navigation Map Page
• Flight Plan Pages
• Terrain-SVS Page
• AUX - Video Page
Displaying terrain and obstacle information (maps other than the Terrain-SVS Page):
1) Select the MAP Softkey (for the PFD Inset Map, press the INSET Softkey).
EIS
The Navigation Map Page Setup Menu provides a means in addition to the softkeys for enabling/disabling the
display of terrain and obstacles. The setup menu also controls the map range settings above which terrain and
obstacle data are decluttered from the display. If a map range larger than the map range setting is selected, the
data is removed from the map. For terrain data, the enable/disable function applies only to the MFD, while the
range setting also affects the PFD Inset Map.
FLIGHT
MANAGEMENT
When Terrain-SVS is selected on maps other than the Terrain-SVS Page, an icon is shown to indicate that the
feature is enabled for display. A legend for Terrain-SVS terrain colors will accompany the icon on the Navigation
Map Page (Figure 6-76) and the Flight Plan Pages. The legend is always shown on the Terrain-SVS Page.
AUDIO PANEL
& CNS
2) Select the TERRAIN Softkey to display terrain and obstacle data.
Terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings
and cautions are issued are shown when terrain is selected for display and the map range is within the setting
limit.
HAZARD
AVOIDANCE
Maps besides the Terrain-SVS Page use settings based on those selected for the Navigation Map Page. The
maximum display ranges for obstacles on each map are dependent on the range setting made for the Navigation
Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm, the highest
obstacle display range settings on the other applicable maps are also adjusted proportionally.
AFCS
CAUTION: Terrain and obstacle data will not be displayed when the Navigation Map range is larger than
the MAP SETUP range setting for TERRAIN DATA and OBSTACLE DATA.
Customizing terrain and obstacle display on the Navigation Map Page:
ADDITIONAL
FEATURES
1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-70).
4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-71).
APPENDICES
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-72).
• TERRAIN DATA – Turns the display of terrain data on or off and sets maximum range at which terrain is shown
• OBSTACLE DATA – Turns the display of obstacle data on or off and sets maximum range at which obstacles are shown
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
INDEX
7) Press the ENT Key to select an option.
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
334
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
Figure 6-70 Navigation Map Page Menu
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 6-71 Navigation Map Page Setup Menu
Figure 6-72 Navigation Map Page Setup Menu, Map Group
TERRAIN-SVS PAGE
HAZARD
AVOIDANCE
The Terrain-SVS Page is specialized to show terrain, obstacle, and potential impact point data in relation
to the aircraft’s current altitude, without clutter from the basemap. It is the principal map page for viewing
terrain information. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference. If an
obstacle and the projected flight path of the aircraft intersect, the display automatically zooms in to the closest
potential point of impact on the Terrain-SVS Page.
AFCS
Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are
available relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map range is adjustable with the RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or arcs).
ADDITIONAL
FEATURES
Displaying the Terrain-SVS Page:
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Terrain-SVS Page.
APPENDICES
Changing the Terrain-SVS Page view:
1) Select the VIEW Softkey.
2) Select the 360 or ARC Softkey to choose the desired view.
Or:
INDEX
1) Press the MENU Key.
2) Select ‘View Arc’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
335
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Showing/hiding aviation information on the Terrain-SVS Page:
1) Press the MENU Key.
FLIGHT
INSTRUMENTS
2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key.
Map Orientation
Current Aircraft
GPS-derived GSL
Altitude
Red Terrain
(Above or Within
100’ Below the
Aircraft Altitude)
EIS
Map Range Rings
Black Terrain
(More than 1000’
Below the Aircraft
Altitude)
AUDIO PANEL
& CNS
Red Lighted Obstacle
(Above or Within
100’ Below Aircraft
Altitude)
Yellow Terrain
(Between 100’
and 1000’ Below
the Aircraft
Altitude)
FLIGHT
MANAGEMENT
Yellow Lighted Obstacles
(Between 100’ and 1000’
Below Aircraft Altitude)
Terrain Legend
Annunciation
Window
HAZARD
AVOIDANCE
Figure 6-73 Terrain-SVS Page
Map Orientation
Current Aircraft
GPS-derived GSL
Altitude
AFCS
Red Terrain
(Above or Within
100’ Below the
Aircraft Altitude)
Map Range Arc
ADDITIONAL
FEATURES
Yellow Terrain
(Between 100’ and
1000’ Below the
Aircraft Altitude)
APPENDICES
Black Terrain
(Terrain More
than 1000’ Below
the Aircraft
Altitude)
Terrain Legend
Red Lighted Obstacle
(Above or Within
100’ Below Aircraft
Altitude)
Annunciation
Window
INDEX
Figure 6-74 Terrain-SVS Page (ARC View)
336
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
TERRAIN-SVS ALERTS
FLIGHT
INSTRUMENTS
Alerts are issued when flight conditions meet parameters that are set within Terrain-SVS software algorithms. Terrain-SVS alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is
issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-8 shows TerrainSVS alert types with corresponding annunciations and aural messages.
When an alert is issued, annunciations appear on the PFD and MFD. The Terrain-SVS Alert Annunciation is
shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the TerrainSVS Page is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the pop-up alert:
EIS
• Press the CLR Key (returns to the currently viewed page), or
• Press the ENT Key (accesses the Terrain-SVS Page)
Alert Annunciation
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Pop-up
Alert
Figure 6-75 Terrain-SVS Alert Annunciations
AFCS
ADDITIONAL
FEATURES
APPENDICES
Terrain Display Enabled
Terrain Legend
Alert Annunciation
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
INDEX
Figure 6-76 Navigation Map Page
(After Terrain-SVS Pop-up Alert Acknowledgment)
337
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
PFD/MFD*
Alert
Annunciation
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Alert Type
MFD Pop-Up Alert (Except
Terrain-SVS Page)
Aural Message
Reduced Required Terrain Clearance
Warning (RTC)
“Warning; Terrain, Terrain”
Imminent Terrain Impact Warning (ITI)
“Warning; Terrain, Terrain”
Reduced Required Obstacle Clearance
Warning (ROC)
“Warning; Obstacle, Obstacle”
Imminent Obstacle Impact Warning (IOI)
“Warning; Obstacle, Obstacle”
Reduced Required Terrain Clearance
Caution (RTC)
“Caution; Terrain, Terrain”
Imminent Terrain Impact Caution (ITI)
“Caution; Terrain, Terrain”
Reduced Required Obstacle Clearance
Caution (ROC)
“Caution; Obstacle, Obstacle”
Imminent Obstacle Impact Caution (IOI)
“Caution; Obstacle, Obstacle”
*Annunciation shown on MFD pages when terrain display is enabled
Table 6-8 Terrain-SVS Alerts Summary
FORWARD LOOKING TERRAIN AVOIDANCE
HAZARD
AVOIDANCE
The Forward Looking Terrain Avoidance (FLTA) feature of Terrain-SVS compares the aircraft’s projected
flight path with known terrain and obstacles in their respective databases and issues four types of alerts as
either a caution or a warning:
AFCS
Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC)
alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum
clearance values in Figure 6-77. When an RTC alert is issued, a potential impact point is displayed on the
Terrain-SVS Page.
INDEX
APPENDICES
ADDITIONAL
FEATURES
Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the
aircraft is below the elevation of a terrain or obstacle cell in the aircraft’s projected path. ITI and IOI alerts are
accompanied by a potential impact point displayed on the Terrain-SVS Page. The alert is annunciated when
the projected vertical flight path is calculated to come within minimum clearance altitudes in Figure 6-77.
338
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Level (FT)
Descending (FT)
800
600
FLIGHT
INSTRUMENTS
500
400
300
200
EIS
Required
Clearance
(FT)
Required Terrain
Clearance (FT)
700
100
0
5
10
15
20
25
AUDIO PANEL
& CNS
0
30
Distance From Runway (NM)
Figure 6-77 FLTA Alert Minimum Terrain and Obstacle Clearance Values
FLIGHT
MANAGEMENT
FLTA alerts are automatically inhibited when the aircraft is less than 200 feet above the destination runway
elevation while within 0.5 nm of the approach runway or the aircraft is between runway ends. Alerts can
also be manually inhibited. Discretion should be used when inhibiting Terrain-SVS alerting, and the system
should be enabled when appropriate. When Terrain-SVS alerting is inhibited, the status annunciation ‘TER
INH’ is shown on the PFD and inside the Terrain-SVS annunciation window on the MFD (Figure 6-78).
HAZARD
AVOIDANCE
Figure 6-78 Terrain-SVS Alerting Disabled
(Terrain-SVS Inhibited) Annunciation
AFCS
Inhibiting/enabling Terrain-SVS alerting:
1) Select the Terrain-SVS Page.
2) Press the INHIBIT Softkey to inhibit or enable Terrain-SVS (choice dependent on current state).
ADDITIONAL
FEATURES
Or:
a) Press the MENU Key.
b) Select ‘Inhibit Terrain’ or ‘Enable Terrain’ (choice dependent on current state) and press the ENT Key.
APPENDICES
If Terrain-SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS
approach, a ‘LOW ALT’ annunciation may appear on the PFD next to the Altimeter if the current aircraft
altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments
Section for details.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
339
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
SYSTEM STATUS
FLIGHT
INSTRUMENTS
During power-up, Terrain-SVS conducts a self-test of its aural and visual annunciations. An aural alert is
issued at test completion.
Alert Type
PFD/MFD* Status
Annunciation
System Test in Progress
System Test Pass
EIS
Terrain System Test Fail
None
Terrain-SVS Page Center
Banner Annunciation
Aural Message
TERRAIN TEST
None
None
“Terrain System Test OK”
TERRAIN FAIL
“Terrain System Failure”
AUDIO PANEL
& CNS
*Annunciation shown on MFD pages with terrain display enabled
Table 6-9 Terrain-SVS System Test Status Annunciations
Terrain-SVS continually monitors several system-critical items such as database validity, hardware status, and
GPS status. If the terrain/obstacle database is not available, the aural message “Terrain System Failure” is
generated along with the ‘TER FAIL’ alert annunciation.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Terrain-SVS requires a 3-D GPS navigation solution along with specific vertical accuracy minimums. Should
the navigation solution become degraded or if the aircraft is out of the database coverage area, the annunciation
‘TER N/A’ is generated in the annunciation window and on the Terrain-SVS Page. The aural message “Terrain
System Not Available” is generated. When the GPS signal is re-established and the aircraft is within the
database coverage area, the aural message “Terrain System Available” is generated.
340
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Aural Message
TERRAIN DATABASE FAILURE
None
TERRAIN FAIL
“Terrain System Failure”
NO GPS POSITION
“Terrain System Not Available”
“Terrain System Available” when GPS
position availability returns
“Terrain System Not Available”
“Terrain System Available” when
sufficient GPS signal reception returns.
EIS
Terrain-SVS Page Center Banner
Annunciation
FLIGHT
INSTRUMENTS
Out of database
coverage area
None
HAZARD
AVOIDANCE
None
FLIGHT
MANAGEMENT
Excessively degraded
GPS signal
AUDIO PANEL
& CNS
PFD/MFD*
Alert Cause
Status
Annunciation
MFD Terrain or Obstacle
None
database unavailable
or invalid. System
operating with PFD
Terrain or Obstacle
databases
Terrain or Obstacle
database unavailable or
invalid, invalid software
configuration, system
audio fault
No GPS position
“Terrain System Not Available”
“Terrain System Available” when reentering database coverage area
*Annunciation shown on MFD pages with terrain display enabled
Table 6-10 Terrain-SVS Status Annunciations
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
341
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
6.6 TAWS-B
FLIGHT
INSTRUMENTS
NOTE: The data contained in the TAWS databases comes from government agencies. Garmin accurately
EIS
WARNING: Do not use TAWS information for primary terrain avoidance. TAWS is intended only to enhance
NOTE: Terrain data is not displayed when the aircraft is outside of the installed terrain database coverage
situational awareness.
processes and cross-validates the data but cannot guarantee the accuracy and completeness of the data.
area.
AUDIO PANEL
& CNS
TAWS-B (Terrain Awareness and Warning System - Class B) is used to increase situational awareness and aid in
reducing controlled flight into terrain (CFIT). TAWS provides visual and aural annunciations when terrain and
obstacles are within the given altitude threshold from the aircraft. The displayed alerts and warnings are advisory
in nature only.
FLIGHT
MANAGEMENT
TAWS-B satisfies TSO-C151b Class B requirements for certification.
TAWS-B requires the following to operate properly:
• A valid terrain/obstacle/airport terrain database
• A valid 3-D GPS position solution
HAZARD
AVOIDANCE
TAWS-B uses terrain and obstacle information supplied by government sources. Terrain information is based
on terrain elevation information in a database that may contain inaccuracies. Individual obstructions may be
shown if available in the database. The data undergoes verification by Garmin to confirm accuracy of the content,
per TSO-C151b. However, the displayed information should never be understood as being all-inclusive and data
may be inaccurate.
APPENDICES
The terrain and obstacle databases used by TAWS-B are referenced to MSL. Using the GPS position and GSL
altitude, TAWS-B displays a 2-D picture of the surrounding terrain and obstacles relative to the position and
altitude of the aircraft. Furthermore, the GPS position and GSL altitude are used to calculate and “predict” the
aircraft’s flight path in relation to the surrounding terrain and obstacles. In this manner, TAWS-B can provide
advanced alerts of predicted dangerous terrain conditions.
INDEX
ADDITIONAL
FEATURES
AFCS
TAWS-B uses information provided from the GPS receiver to provide a horizontal position and altitude. GPS
altitude is derived from satellite measurements. GPS altitude is then converted to the height above geodetic sea
level (GSL), which is the height above mean sea level (MSL) calculated geometrically. GSL altitude is used to
determine TAWS-B alerts. GSL altitude accuracy is affected by satellite geometry, but is not subject to variations
in pressure and temperature that normally affect pressure altitude sensors. GSL altitude does not require local
altimeter settings to determine MSL altitude. It is a widely-used MSL altitude source. Therefore, GSL altitude
provides a highly accurate and reliable MSL altitude source to calculate terrain and obstacle alerts.
Baro-corrected altitude (or indicated altitude) is derived by adjusting the altimeter setting for local atmospheric
conditions. The most accurate baro-corrected altitude can be achieved by frequently updating the altimeter
setting to the nearest reporting station along the flight path. However, because actual atmospheric conditions
seldom match the standard conditions defined by the International Standard Atmosphere (ISA) model (where
342
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
pressure, temperature, and lapse rates have fixed values), it is common for the baro-corrected altitude (as read
from the altimeter) to differ from the GSL altitude. This variation results in the aircraft’s GSL altitude differing
from the baro-corrected altitude.
FLIGHT
INSTRUMENTS
DISPLAYING TAWS-B DATA
TAWS-B uses yellow (caution) and red (warning) to depict terrain and obstacles (with heights greater than
200 feet above ground level, AGL) alerts relative to aircraft altitude. Colors are adjusted automatically as the
aircraft altitude changes. The colors and symbols in the figure and tables below are used to represent terrain,
obstacles, and potential impact points.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 6-79 Terrain Altitude/Color Correlation for TAWS-B
Obstacle Location
HAZARD
AVOIDANCE
Unlighted Obstacle
Lighted Obstacle
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL
Red obstacle is above or within 100 ft
below the aircraft altitude
AFCS
Yellow obstacle is between 100 ft and
1000 ft below the aircraft altitude
Table 6-11 TAWS-B Obstacle Colors and Symbology
Alert Type
ADDITIONAL
FEATURES
Potential Impact
Point Symbol
Example Annunciation
Warning
APPENDICES
Caution
Table 6-12 TAWS-B Potential Impact Point Symbols with Alert Types
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
343
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
FLIGHT
INSTRUMENTS
TAWS-B information can be displayed on the following maps:
• PFD Inset Map
• Trip Planning Page
• Navigation Map Page
• Flight Plan Pages
• TAWS-B Page
• AUX-Video Page
Displaying terrain and obstacle information (maps other than the TAWS-B Page):
1) Select the MAP Softkey (for the PFD Inset Map, press the INSET Softkey).
2) Select the TERRAIN Softkey to display terrain and obstacle data.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
When TAWS-B is selected on maps other than the TAWS-B Page, an icon is shown to indicate that the feature
is enabled for display. A legend for TAWS-B terrain colors will accompany the icon on the Navigation Map Page
(Figure 6-80) and the Flight Plan Pages. The icon is always shown on the TAWS-B Page.
Figure 6-80 TAWS-B Icon and Legend
HAZARD
AVOIDANCE
The Navigation Map Page Setup Menu provides a means in addition to the softkeys for enabling/disabling the
display of terrain and obstacles. The setup menu also controls the map range settings above which terrain and
obstacle data are decluttered from the display. If a map range larger than the map range setting is selected, the
data is removed from the map. For terrain data, the enable/disable function applies only to the MFD, while the
range setting also affects the PFD Inset Map.
AFCS
Terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings
and cautions are issued are shown when terrain is selected for display and the map range is within the setting
limit.
INDEX
APPENDICES
ADDITIONAL
FEATURES
Maps besides the TAWS-B Page use settings based on those selected for the Navigation Map Page. The
maximum display ranges for obstacles on each map are dependent on the range setting made for the Navigation
Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm, the highest
obstacle display range settings on the other applicable maps are also adjusted proportionally.
344
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
CAUTION: Terrain and obstacle data will not be displayed when the Navigation Map range is larger than
the MAP SETUP range setting for TERRAIN DATA and OBSTACLE DATA.
FLIGHT
INSTRUMENTS
Customizing terrain and obstacle display on the Navigation Map Page:
1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-81).
EIS
4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-82).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-83).
• TERRAIN DATA – Turns the display of terrain data on or off and sets maximum range at which terrain is shown
AUDIO PANEL
& CNS
• OBSTACLE DATA – Turns the display of obstacle data on or off and sets maximum range at which obstacles are shown
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings).
7) Press the ENT Key to select an option.
FLIGHT
MANAGEMENT
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
HAZARD
AVOIDANCE
AFCS
Figure 6-81 Navigation Map Page Menu
ADDITIONAL
FEATURES
APPENDICES
Figure 6-82 Navigation Map Page Setup Menu
Figure 6-83 Navigation Map Page Setup Menu, Map Group
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
345
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
TAWS-B PAGE
FLIGHT
INSTRUMENTS
The TAWS-B Page is specialized to show terrain, obstacle, and potential impact point data in relation to the
aircraft’s current altitude, without clutter from the basemap. It is the principal map page for viewing terrain
information. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference. If an obstacle
and the projected flight path of the aircraft intersect, the display automatically zooms in to the closest potential
point of impact on the TAWS-B Page.
EIS
Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are available
relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map range
is adjustable with the RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or arcs).
Displaying the TAWS-B Page:
AUDIO PANEL
& CNS
2) Turn the small FMS Knob to select the TAWS-B Page.
FLIGHT
MANAGEMENT
1) Turn the large FMS Knob to select the Map Page Group.
2) Select the 360 or ARC Softkey to select the desired view.
Changing the TAWS-B Page view:
1) Select the VIEW Softkey.
Or:
1) Press the MENU Key.
HAZARD
AVOIDANCE
2) Select ‘View ARC’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view
Showing/hiding aviation information on the TAWS-B Page:
1) Press the MENU Key.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key.
346
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Map Orientation
Current Aircraft
GPS-derived GSL
Altitude
FLIGHT
INSTRUMENTS
Red Terrain
(Above or Within
100’ Below the
Aircraft Altitude)
Map Range Rings
Black Terrain
(More than 1000’
Below the Aircraft
Altitude)
EIS
Red Lighted Obstacle
(Above or Within
100’ Below Aircraft
Altitude)
Yellow Lighted
Obstacles (Between
100’ and 1000’
Below Aircraft
Altitude)
AUDIO PANEL
& CNS
Yellow Terrain
(Between 100’
and 1000’ Below
the Aircraft
Altitude)
Terrain Legend
Annunciation
Window
FLIGHT
MANAGEMENT
Figure 6-84 TAWS-B Page
Red Terrain
(Above or Within
100’ Below the
Aircraft Altitude)
HAZARD
AVOIDANCE
Map Orientation
Current Aircraft
GPS-derived GSL
Altitude
Map Range Arc
AFCS
Yellow Terrain
(Between 100’ and
1000’ Below the
Aircraft Altitude)
ADDITIONAL
FEATURES
Black Terrain
(Terrain More
than 1000’ Below
the Aircraft
Altitude)
Terrain Legend
Red Lighted Obstacle
(Above or Within
100’ Below Aircraft
Altitude)
Annunciation
Window
APPENDICES
Figure 6-85 TAWS-B Page (ARC View)
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
347
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
TAWS-B ALERTS
FLIGHT
INSTRUMENTS
Alerts are issued when flight conditions meet parameters that are set within TAWS-B software algorithms. TAWS-B alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert
is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-13 shows
TAWS-B alert types with corresponding annunciations and aural messages.
EIS
When an alert is issued, annunciations appear on the PFD and MFD. The TAWS-B Alert Annunciation is
shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the TAWS-B
Page is not displayed at the time of the alert, a pop-up alert appears on the MFD. To acknowledge the pop-up
alert:
• Press the CLR Key (returns to the currently viewed page), or
• Press the ENT Key (accesses the TAWS-B Page)
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Alert Annunciation
Pop-up
Alert
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 6-86 TAWS-B Alert Annunciations
Terrain Display Enabled
Terrain Legend
Alert Annunciation
INDEX
Figure 6-87 Navigation Map Page
(After TAWS-B Pop-up Alert Acknowledgment)
348
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
MFD Pop-Up Alert
(Except TAWS-B Page)
Aural Message
Excessive Descent Rate Warning
(EDR)
“Pull Up”
or
*
or
Imminent Obstacle Impact
Warning (IOI)
or
*
*
*
or
“Terrain Ahead; Terrain Ahead”*
or
“Caution, Terrain; Caution, Terrain”
Reduced Required Obstacle
Clearance Caution (ROC)
or
“Obstacle Ahead; Obstacle Ahead”
or
“Caution, Obstacle; Caution, Obstacle”*
*
or
“Obstacle Ahead; Obstacle Ahead”*
or
“Caution, Obstacle; Caution, Obstacle”
ADDITIONAL
FEATURES
*
Imminent Obstacle Impact
Caution (IOI)
AFCS
“Terrain Ahead; Terrain Ahead”*
or
“Caution, Terrain; Caution, Terrain”
or
Imminent Terrain Impact
Caution (ITI)
“Too Low, Terrain”
None
None
APPENDICES
“Five-Hundred”
“Sink Rate”
*
or
“Don’t Sink”*
or
“Too Low, Terrain”
INDEX
Negative Climb Rate Caution
(NCR)
*
HAZARD
AVOIDANCE
Reduced Required Terrain
Clearance Caution (RTC)
FLIGHT
MANAGEMENT
Reduced Required Obstacle
Clearance Warning (ROC)
AUDIO PANEL
& CNS
or
“Terrain Ahead, Pull Up; Terrain Ahead, Pull
Up”*
or
“Terrain, Terrain; Pull Up, Pull Up”*
Terrain Ahead, Pull Up; Terrain Ahead, Pull
Up’*
or
“Terrain, Terrain; Pull Up, Pull Up”
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull
Up”
or
“Obstacle, Obstacle; Pull Up, Pull Up”*
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull
Up”*
or
“Obstacle, Obstacle; Pull Up, Pull Up”
EIS
*
Imminent Terrain Impact
Warning (ITI)
FLIGHT
INSTRUMENTS
Reduced Required Terrain
Clearance Warning (RTC)
Premature Descent Alert
Caution (PDA)
Altitude Callout “500”
Excessive Descent Rate Caution
(EDR)
SYSTEM
OVERVIEW
PFD/MFD† Alert
Annunciation
Alert Type
* Alerts with multiple messages are configurable at installation and are installation-dependent. Alerts for the default
configuration are indicated with asterisks.
† Annunciation shown on MFD pages when terrain display is enabled
Table 6-13 TAWS-B Alerts Summary
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
349
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
EXCESSIVE DESCENT RATE ALERT
FLIGHT
INSTRUMENTS
The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the
aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 6-88 shows the
parameters for the alert as defined by TSO-C151b.
6000
5500
5000
Height Above Terrain (Feet)
4500
EIS
4000
NK
: “SI
ion
Caut
3500
”
RATE
3000
AUDIO PANEL
& CNS
2500
2000
Warning: “PULL UP”
1500
1000
12000
11000
Descent Rate (FPM)
10000
9000
8000
7000
6000
5000
4000
3000
2000
1000
0
0
FLIGHT
MANAGEMENT
500
HAZARD
AVOIDANCE
Figure 6-88 Excessive Descent Rate Alert Criteria
FORWARD LOOKING TERRAIN AVOIDANCE
AFCS
The Forward Looking Terrain Avoidance (FLTA) feature of TAWS-B compares the aircraft’s projected flight
path with known terrain and obstacles in their respective databases and issues four types of alerts as either a
caution or a warning:
ADDITIONAL
FEATURES
Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC)
alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum
clearance values in Figure 6-89. When an RTC alert is issued, a potential impact point is displayed on the
TAWS-B Page.
INDEX
APPENDICES
Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the
aircraft is below the elevation of a terrain or obstacle cell in the aircraft’s projected path. ITI and IOI alerts
are accompanied by a potential impact point displayed on the TAWS-B Page. The alert is annunciated when
the projected vertical flight path is calculated to come within minimum clearance altitudes in Figure 6-89.
350
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Level (FT)
Descending (FT)
800
600
FLIGHT
INSTRUMENTS
500
400
300
200
EIS
Required
Clearance
(FT)
Required Terrain
Clearance (FT)
700
100
0
5
10
15
20
25
AUDIO PANEL
& CNS
0
30
Distance From Runway (NM)
Figure 6-89 FLTA Alert Minimum Terrain and Obstacle Clearance Values
FLIGHT
MANAGEMENT
FLTA alerts are automatically disabled when the aircraft is less than 200 feet above the destination runway
elevation while within 0.5 nm of the approach runway or the aircraft is between runway ends.
PREMATURE DESCENT ALERTING
HAZARD
AVOIDANCE
A Premature Descent Alert (PDA) is issued when the system detects that the aircraft is significantly
below the normal approach path to a runway (Figure 6-90).
PDA alerting begins when the aircraft is below 700 feet AGL within 15 nm of the destination airport and
ends when the aircraft is 0.5 nm from the runway threshold.
800
600
500
ADDITIONAL
FEATURES
400
300
PDA ALERTING AREA
200
100
APPENDICES
Height Above Destination (Feet)
AFCS
700
15
14
13
12
11
10
9
8
7
6
5
4
3
2
1
0
0
Distance to Destination (NM)
Figure 6-90 PDA Alerting Threshold
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
351
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
FLIGHT
INSTRUMENTS
PDA and FLTA aural and visual alerts can be manually inhibited. Discretion should be used when
inhibiting TAWS-B and the system should be enabled when appropriate. When TAWS-B is inhibited, the
alert annunciation ‘TAWS INH’ is shown on the PFD and in the TAWS-B Annunciation Window of the MFD
(Figure 6-91).
Figure 6-91 TAWS-B Alerting Disabled
(TAWS-B Inhibited) Annunciation
EIS
Inhibiting/enabling TAWS-B alerting:
1) Select the TAWS-B Page.
AUDIO PANEL
& CNS
2) Press the INHIBIT Softkey to inhibit or enable TAWS (choice dependent on current state).
Or:
a) Press the MENU Key.
FLIGHT
MANAGEMENT
b) Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current state) and press the ENT Key.
If TAWS-B alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach,
a ‘LOW ALT’ annunciation may appear on the PFD next to the Altimeter if the current aircraft altitude is at
least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments Section for
details.
HAZARD
AVOIDANCE
FIVE-HUNDRED AURAL ALERT
AFCS
The purpose of the aural alert message “Five-hundred” is to provide an advisory alert of when the aircraft
descends to within 500 feet above the terrain or runway threshold. When the aircraft is within 5 nm of an
airport, the “Five Hundred” aural alert is based on the nearest runway threshold elevation. When the aircraft
is more than 5 nm of the nearest airport, the “Five Hundred” aural alert is based on the height above terrain
as determined by the GPS-derived GSL altitude and terrain database.
NEGATIVE CLIMB RATE AFTER TAKEOFF ALERT (NCR)
ADDITIONAL
FEATURES
The Negative Climb Rate (NCR) After Takeoff alert (also referred to as “Altitude Loss After Takeoff”)
provides alerts when the system determines the aircraft is losing altitude (closing upon terrain) after takeoff. The aural message “Don’t Sink” is given for NCR alerts, accompanied by an annunciation and a pop-up terrain
alert on the display. NCR alerting is only active when departing from an airport and when the following
conditions are met:
APPENDICES
• Height above the terrain is less than 700 feet
• Distance from the departure airport is 2 nm or less
• Heading change from the departure heading is less than 110 degrees
INDEX
Figures 6-75 and 6-76 shows the NCR alerting parameters as defined by TSO-C151b.
352
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
1000
800
FLIGHT
INSTRUMENTS
Height Above Terrain (Feet)
900
700
600
“DON’T SINK”
or
“TOO LOW, TERRAIN”
500
400
300
EIS
200
100
0
20
40
60
80
100
120
140
AUDIO PANEL
& CNS
0
Altitude Loss (Feet)
Figure 6-92 Negative Climb Rate (NCR) Altitude Loss
1000
FLIGHT
MANAGEMENT
800
700
600
“DON’T SINK”
or
“TOO LOW, TERRAIN”
500
400
300
HAZARD
AVOIDANCE
Height Above Terrain (Feet)
900
200
100
AFCS
0
0
500
1000
1500
2000
2500
3000
3500
4000
4500
5000
5500
6000
6500
7000
Sink Rate (FPM)
ADDITIONAL
FEATURES
Figure 6-93 Negative Climb Rate (NCR) Sink Rate
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
353
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
SYSTEM STATUS
FLIGHT
INSTRUMENTS
During power-up, TAWS-B conducts a self-test of its aural and visual annunciations. The system test can also
be manually initiated. An aural alert is issued at test completion. TAWS-B System Testing is disabled when
ground speed exceeds 30 knots.
Alert Type
PFD/MFD* Status
Annunciation
System Test in Progress
EIS
System Test Pass
None
TAWS-B System Test Fail
TAWS-B Page
Center Banner
Annunciation
Aural Message
TAWS TEST
None
None
“TAWS System Test OK”
TAWS FAIL
“TAWS System Failure”
AUDIO PANEL
& CNS
*Annunciation shown on MFD pages when terrain display is enabled
Table 6-14 TAWS-B System Test Status Annunciations
Manually testing the TAWS-B System:
FLIGHT
MANAGEMENT
1) Select the TAWS-B Page.
2) Press the MENU Key (Figure 6-89).
AFCS
HAZARD
AVOIDANCE
3) Select ‘Test TAWS System’ and press the ENT Key to confirm the selection.
Figure 6-89 TAWS-B Page Menu
ADDITIONAL
FEATURES
TAWS-B continually monitors several system-critical items such as database validity, hardware status, and
GPS status. If the terrain/obstacle database is not available, the aural message “TAWS System Failure” is
generated along with the ‘TAWS FAIL’ alert annunciation.
INDEX
APPENDICES
TAWS-B requires a 3-D GPS navigation solution along with specific vertical accuracy minimums. Should the
navigation solution become degraded or if the aircraft is out of the database coverage area, the annunciation
‘TAWS N/A’ is generated in the annunciation window and on the TAWS-B Page. The aural message “TAWS Not
Available” is generated. When the GPS signal integrity returns and the aircraft is within the database coverage
area, the aural message “TAWS Available” is generated
354
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
Aural Message
TERRAIN DATABASE FAILURE
None
TAWS FAIL
“TAWS System Failure”
NO GPS POSITION
“TAWS Not Available”
“TAWS Available” when GPS
position availability returns
“TAWS Not Available”
“TAWS Available” when sufficient
GPS signal is received
“TAWS Not Available”
“TAWS Available” when aircraft reenters database coverage area.
EIS
TAWS-B Page Annunciation
FLIGHT
INSTRUMENTS
None
Out of database coverage
area
None
FLIGHT
MANAGEMENT
Excessively degraded GPS
signal
AUDIO PANEL
& CNS
MFD Terrain or Obstacle
database unavailable or
invalid. System operating
with PFD Terrain or Obstacle
databases
Terrain or Obstacle
database unavailable or
invalid, invalid software
configuration, TAWS audio
fault
No GPS position
PFD/MFD*
Status
Annunciation
None
SYSTEM
OVERVIEW
Alert Cause
HAZARD
AVOIDANCE
*Annunciation shown on MFD pages when terrain display is enabled
Table 6-15 TAWS-B Abnormal Status Annunciations
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
355
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
6.7 TRAFFIC INFORMATION SERVICE (TIS)
FLIGHT
INSTRUMENTS
WARNING: The Traffic Information Service (TIS) is intended for advisory use only. TIS is intended to help the
pilot locate traffic visually. It is the responsibility of the pilot to see and maneuver to avoid traffic.
NOTE: TIS is available only when the aircraft is within the service volume of a TIS-capable terminal radar
EIS
site. Aircraft without an operating transponder are invisible to both Traffic Advisory Systems (TAS) and TIS.
Aircraft without altitude reporting capability are shown without altitude separation data or climb descent
indication.
AUDIO PANEL
& CNS
NOTE: TIS is disabled if a Traffic Advisory System (TAS) is installed.
FLIGHT
MANAGEMENT
Traffic Information Service (TIS) is designed to help in detection and avoidance of other aircraft. TIS uses the
Mode S transponder for the traffic data link. TIS receives traffic information from ground stations, and is updated
every 5 seconds. The system displays up to eight traffic targets within a 7.5-nm radius, from 3000 feet below to
3500 feet above the requesting aircraft. Traffic is displayed using the symbology shown in the table below.
TIS Symbol
Description
Non-Threat Traffic
HAZARD
AVOIDANCE
Traffic Advisory (TA)
Traffic Advisory Off Scale
AFCS
Table 6-16 TIS Traffic Symbols
ADDITIONAL
FEATURES
Traffic Advisories (TA) alert the crew to intruding aircraft. When traffic meets the advisory criteria for the TA,
a solid yellow circle symbol is generated. A TA which is detected but is outside the range of the map on which
traffic is displayed are indicated with a message in the lower left corner of the map.
APPENDICES
TIS also provides a vector line showing the direction in which the traffic is moving, to the nearest 45°. Traffic
information for which TIS is unable to determine the bearing (non-bearing traffic) is displayed in the center of the
Traffic Map Page (Figure 6-94) or in a banner at the lower left corner of maps other than the Traffic Map Page on
which traffic can be displayed (Figure 6-90).
INDEX
The altitude difference between the requesting aircraft and other intruder aircraft is displayed above/below the
traffic symbol in hundreds of feet. If the other aircraft is above the requesting aircraft, the altitude separation
appears above the traffic symbol; if below, the altitude separation appears below. Altitude trend is displayed as
an up/down arrow (for vertical speeds greater than 500 fpm in either direction) to the right of the traffic symbol. Traffic symbols for aircraft without altitude reporting capability appear without altitude separation or climb/
descent information.
356
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
DISPLAYING TRAFFIC DATA
Traffic information can be displayed on the following maps (when TIS is operating):
• Nearest Pages
• Navigation Map Page
• Active Flight Plan Page
• Traffic Map Page
• AUX - Video Page
FLIGHT
INSTRUMENTS
• PFD Inset Map
• Trip Planning Page
EIS
Traffic information is also displayed on the PFD when the Synthetic Vision System (SVS) option is installed
and enabled. See the Additional Features Section for details.
Displaying traffic information (maps other than the Traffic Map Page):
AUDIO PANEL
& CNS
1) Select the MAP Softkey.
2) Select the TRAFFIC Softkey. Traffic is now displayed on the map.
When traffic is selected on maps other than the Traffic Map Page, an icon is shown to indicate the feature is
enabled for display.
FLIGHT
MANAGEMENT
Non-Threat
Traffic
HAZARD
AVOIDANCE
Traffic
Advisory
AFCS
TA Off Scale
Banner
Annunciation
Traffic System
Status Banner
Annunciations
“No Bearing”
Traffic Advisory
Banner
Annunciation
Traffic Status
Icon
ADDITIONAL
FEATURES
Figure 6-95 TIS Traffic on Navigation Map Page
Displaying traffic information (PFD Inset Map):
APPENDICES
1) Select the INSET Softkey.
2) Select the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1).
3) Select the softkey again to display the traffic-only inset (TRFC-2).
4) Select the softkey again to remove traffic data.
INDEX
The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling
display of traffic. The setup menu also controls the map range settings above which traffic data (symbols
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
357
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
and labels) are decluttered from the display. If a map range larger than the map range setting is selected, the
data is removed from the map. Maps besides the Traffic Map Page use settings based on those selected for the
Navigation Map Page.
FLIGHT
INSTRUMENTS
Customizing traffic display on the Navigation Map Page:
1) Select the Navigation Map Page.
2) Press the MENU Key.
3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-91).
EIS
4) Turn the small FMS Knob to select the ‘Traffic’ Group and press the ENT Key (Figure 6-92).
5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-93).
• TRAFFIC – Turns the display of traffic data on or off
AUDIO PANEL
& CNS
• TRAFFIC MODE – Selects the traffic mode for display; select from:
- All Traffic - Displays all traffic
- TA ONLY - Displays Traffic Alerts only
FLIGHT
MANAGEMENT
• TRAFFIC SMBL – Selects the maximum range at which traffic symbols are shown
• TRAFFIC LBL – Selects the maximum range at which traffic labels are shown (with the option to turn off)
6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.).
7) Press the ENT Key to select an option.
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings.
INDEX
APPENDICES
Figure 6-96 Navigation Map Page Menu
Figure 6-97 Navigation Map Page Setup Menu
358
Figure 6-98 Navigation Map Page Setup Menu, Traffic Group
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
TRAFFIC MAP PAGE
FLIGHT
INSTRUMENTS
The Traffic Map Page is specialized to show surrounding TIS traffic data in relation to the aircraft’s current
position and altitude, without clutter from the basemap. It is the principal map page for viewing traffic
information. Aircraft orientation on this map is always heading up unless there is no valid heading. Map range
is adjustable with the RANGE Knob from 2 to 12 nm, as indicated by the map range rings.
The traffic mode is annunciated in the upper left corner of the Traffic Map Page. When the aircraft is on the
ground, TIS automatically enters Standby Mode. Once the aircraft is airborne, TIS switches from Standby to
Operating Mode and the G1000 begins to display traffic information. Refer to the System Status discussion for
more information.
EIS
Displaying traffic on the Traffic Map Page:
1) Turn the large FMS Knob to select the Map Page Group.
AUDIO PANEL
& CNS
2) Turn the small FMS Knob to select the Traffic Map Page.
3) Confirm TIS is in Operating Mode:
Select the OPERATE Softkey to begin displaying traffic.
FLIGHT
MANAGEMENT
Or:
a) Press the MENU Key.
b) Select ‘Operate Mode’ (shown if TIS is in Standby Mode) and press the ENT Key.
Traffic Mode Annunciation
HAZARD
AVOIDANCE
Non-Threat
Traffic, 2500’
Above,
Descending
“TIS Not Available”
Voice Alert Status
AFCS
Traffic Advisory, 500’
Below, Climbing
“Non-Bearing” Traffic
(System Unable to
Determine Bearing)
Distance is 4.0 nm,
500’ Above,
Descending
Off-Scale Traffic
Advisory
400’ Below, Level
ADDITIONAL
FEATURES
Range
Marking
Rings
Traffic Status Banner
Annunciations
Figure 6-99 Traffic Map Page
APPENDICES
Non-Threat
Traffic,
Altitude Not
Reported
Select
to Mute
“TIS Not
Available”
Voice Alert
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
359
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
TIS ALERTS
When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur:
FLIGHT
INSTRUMENTS
• A single “Traffic” voice alert is generated.
• A ‘TRAFFIC’ Annunciation appears to the top left of the Attitude Indicator on the PFD, flashes for 5 seconds
and remains displayed until no TAs are detected in the area.
• The PFD Inset Map is automatically displayed with traffic.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
To reduce the number of nuisance alerts due to proximate aircraft, the “Traffic” voice alert is generated only
when the number of TAs increases. For example, when the first TA is displayed, a voice and visual annunciation
are generated. As long as a single TA remains on the display, no additional voice alerts are generated. If a second
TA appears on the display or if the number of TAs initially decreases and then subsequently increases, another
voice alert is generated.
HAZARD
AVOIDANCE
Inset Map
Displays When
TA is Detected
AFCS
Figure 6-100 Traffic Annunciation (PFD)
A “TIS Not Available” (TNA) voice alert is generated when the TIS service becomes unavailable or is out of
range. TIS may be unavailable in the radar coverage area due to the following:
ADDITIONAL
FEATURES
• Radar site TIS Mode S sensor is not operational or is out of service
• Traffic or requesting aircraft is beyond the maximum range of the TIS-capable Mode S radar site.
• Traffic or requesting aircraft is above the radar site in the cone of silence and out of range of an adjacent site.
APPENDICES
• Traffic or requesting aircraft is below radar coverage. In flat terrain, the coverage extends from about 3000
feet upward at 55 miles. Terrain and obstacles around the radar site can further decrease radar coverage in all
directions.
• Traffic does not have an operating transponder.
INDEX
The “TIS Not Available” (TNA) voice alert can be manually muted to reduce nuisance alerting. TNA muting
status is shown in the upper left corner of the Traffic Map Page.
360
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Muting the “TIS Not Available” voice alert:
1) Select the Traffic Map Page.
2) Select the TNA MUTE Softkey. The status is displayed in the upper left corner of the Traffic Map Page.
FLIGHT
INSTRUMENTS
Or:
a) Press the MENU Key.
b) Select ‘‘’Not Available” Mute On’ (shown if TNA muting is currently off) and press the ENT Key.
SYSTEM STATUS
EIS
The G1000 performs an automatic test of TIS during power-up. If TIS passes the test, TIS enters Standby
Mode (on the ground) or Operating Mode (in the air). If TIS fails the power up test, an annunciation is shown
in the center of the Traffic Map Page.
FAILED
Description
Data is not being received from the transponder*
Data is being received from the transponder, but
a failure is detected in the data stream*
FLIGHT
MANAGEMENT
DATA FAILED
AUDIO PANEL
& CNS
Traffic Map Page
Annunciation
NO DATA
The transponder has failed*
UNAVAILABLE
TIS is unavailable or out of range
HAZARD
AVOIDANCE
* Contact a service center or Garmin dealer for corrective action
Table 6-17 TIS Failure Annunciations
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
361
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
FLIGHT
INSTRUMENTS
System Test has
Failed
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Data Not
Received from
Transponder
Figure 6-101 TIS Power-up Test Failure
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
The traffic mode is annunciated in the upper left corner of the Traffic Map Page. When the aircraft is on the
ground, TIS automatically enters Standby Mode. If traffic is selected for display on another map while Standby
Mode is selected, the traffic display enabled icon is crossed out (also the case whenever TIS has failed). Once
the aircraft is airborne, TIS switches to Operating Mode and traffic information is displayed. The mode can be
changed manually using softkeys or the page menu.
Mode
Traffic Mode Annunciation
(Traffic Map Page)
TIS Operating
OPERATING
TIS Standby
STANDBY
(also shown in white in center of page)
TIS Failed*
FAIL
Traffic Display Enabled Icon
(Other Maps)
* See Table 6-19 for additional failure annunciations
INDEX
APPENDICES
Table 6-18 TIS Modes
362
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
Switching between TIS modes:
1) Select the Traffic Map Page.
FLIGHT
INSTRUMENTS
2) Select the STANDBY or OPERATE Softkey to switch between modes. The mode is displayed in the upper left
corner of the Traffic Map Page.
Or:
a) Press the MENU Key.
b) Select ‘Operate Mode’ or ‘Standby Mode’ (choice dependent on current state) and press the ENT Key.
Traffic Status Banner
Annunciation
AGE MM:SS
TRFC RMVD
Traffic is removed because it is too old for coasting (12 to 60 seconds since last message)
Traffic may exist within the selected display range, but it is not displayed
Traffic data has failed
Traffic has not been detected
The traffic service is unavailable or out of range
AFCS
TRFC FAIL
NO TRFC DATA
TRFC UNAVAIL
HAZARD
AVOIDANCE
TRFC COAST
A Traffic Advisory is outside the selected display range*
Annunciation is removed when traffic comes within the selected display range
System cannot determine bearing of Traffic Advisory**
Annunciation indicates distance in nm, altitude separation in hundreds of feet, and
altitude trend arrow (climbing/descending)
Appears if traffic data is not refreshed within 6 seconds
If after another 6 seconds data is not received, traffic is removed from the display
The quality of displayed traffic information is reduced as the age increases
The displayed data is not current (6 to 12 seconds since last message)
The quality of displayed traffic information is reduced when this message is displayed
FLIGHT
MANAGEMENT
TA X.X ± XX ↕
Description
AUDIO PANEL
& CNS
TA OFF SCALE
EIS
The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of
maps on which traffic can be displayed (Table 6-19).
*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page
ADDITIONAL
FEATURES
Table 6-19 TIS Traffic Status Annunciations
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
363
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
6.8 TCAD 9900BX/TAS 620 TRAFFIC
FLIGHT
INSTRUMENTS
NOTE: TIS is disabled when the optional TCAS 9900BX or TAS 620 systems are installed.
Refer to the TCAD 9900BX/TAS 620 Pilot’s Operating Handbook for a detailed discussion of this system. In the
following section references to TAS include both the TCAD 9900BX and TAS 620 systems.
TAS SYMBOLOGY
EIS
Traffic Advisory System (TAS) is designed to help in detection and avoidance of other aircraft. TAS uses
an on-board interrogator-processor and the Mode S transponder for the air-to-air traffic data link. Traffic is
displayed using the symbology shown in the table below.
AUDIO PANEL
& CNS
TAS Symbol
Description
Non-Threat Traffic
FLIGHT
MANAGEMENT
Proximity Advisory (PA)
Traffic Advisory (TA)
HAZARD
AVOIDANCE
Traffic Advisory Off Scale
Table 6-20 TAS Symbol Description
AFCS
A Non-threat Advisory, shown as an open white diamond, indicates that an intruding aircraft is at greater than
±1200 feet relative altitude or the distance is beyond 5 nm.
A Proximity Advisory indicates that the intruding aircraft is within ±1200 feet and is within 5 nm range, but
is still not considered a threat.
INDEX
APPENDICES
ADDITIONAL
FEATURES
A Traffic Advisory (TA) alerts the crew to a potentially hazardous intruding aircraft. Closing rate, distance,
and vertical separation meet TA criteria. A Traffic Advisory that is beyond the selected display range is indicated
by a half TA symbol at the edge of the screen at the relative bearing of the intruder.
364
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
DISPLAYING TRAFFIC DATA
Traffic information is displayed on the following maps:
• Nearest Pages
• Navigation Map Page
• Active Flight Plan Page
• Traffic Map Page
• AUX - Video Page
FLIGHT
INSTRUMENTS
• PFD Inset Map
• Trip Planning Page
EIS
Traffic information is also displayed on the PFD when the Synthetic Vision System (SVS) option is installed
and enabled. See the Additional Features Section for details.
Displaying traffic on the Traffic Map Page:
AUDIO PANEL
& CNS
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Traffic Map Page.
3) Turn the RANGE Knob clockwise to display a larger area or counter-clockwise to display a smaller area.
FLIGHT
MANAGEMENT
Operating
Mode
Altitude
Mode
Traffic Display
Range Ring
Traffic Advisory,
500’ Below,
Climbing
AFCS
“Non-Bearing”
Traffic (Bearing
Undetermined),
Distance 4.0
nm, 500’ Above,
Descending
HAZARD
AVOIDANCE
Non-Threat
Traffic, 2500’
Above,
Descending
Proximity
Traffic, 900’
Above, Level
ADDITIONAL
FEATURES
Off Scale
Traffic
Advisory, 400’
Below, Level
Non-Threat
Traffic,
Altitude Not
Reported
APPENDICES
Figure 6-102 Traffic Map Page
The Traffic Map Page shows surrounding TAS traffic data in relation to the aircraft’s current position and
altitude, without basemap clutter. Aircraft orientation is always heading up unless there is no valid heading. Map range is adjustable with the RANGE Knob from 2 to 24 nm, as indicated by the map range rings.
INDEX
The traffic mode and altitude display mode are annunciated in the upper left corner.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
365
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Displaying traffic information (maps other than the Traffic Map Page):
1) Select the MAP Softkey.
FLIGHT
INSTRUMENTS
2) Select the TRAFFIC Softkey to display traffic data.
EIS
When traffic is selected on maps other than the Traffic Map Page, a traffic icon is shown to indicate TAS is
enabled for display.
Non-Threat
Traffic
AUDIO PANEL
& CNS
Traffic
Advisory
FLIGHT
MANAGEMENT
Proximity
Traffic
TA Off Scale
Banner
Traffic Enabled
Icon
HAZARD
AVOIDANCE
Non-Bearing
Traffic Advisory
Figure 6-103 TAS Traffic on Navigation Map
Displaying traffic information (PFD Inset Map):
AFCS
1) Select the INSET Softkey.
2) Select the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1).
3) Select the softkey again to display the traffic-only inset (TRFC-2).
INDEX
APPENDICES
ADDITIONAL
FEATURES
4) Select the softkey again to remove traffic data.
366
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
ALTITUDE DISPLAY
Changing the altitude display mode:
FLIGHT
INSTRUMENTS
1) On the Traffic Page, select the ALT MODE Softkey.
2) Select one of the following Softkeys:
BELOW
•
NORMAL
•
ABOVE
•
UNREST (unrestricted)
EIS
•
3) To return to the Traffic Page, press the BACK Softkey.
AUDIO PANEL
& CNS
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select one of the following:
BELOW
•
NORMAL
•
ABOVE
•
UNREST (unrestricted)
FLIGHT
MANAGEMENT
•
HAZARD
AVOIDANCE
3) Press the ENT Softkey.
TRAFFIC MAP PAGE DISPLAY RANGE
The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the
RANGE Knob from 2 to 24 nm, as indicated by the map range rings.
AFCS
Changing the display range on the Traffic Page:
1) Turn the RANGE Knob.
2) The following range options are available:
•
2 and 6 nm
•
6 and 12 nm
•
12 and 24 nm
APPENDICES
2 nm
ADDITIONAL
FEATURES
•
The Navigation Map Page Setup Menu also controls the display of traffic. The setup menu controls the map
range settings. Traffic data symbols and labels can be decluttered from the display. If a map range larger than
the map range setting is selected, the data is removed from the map. Maps besides the Traffic Map Page use
settings based on those selected for the Navigation Map Page.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
367
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
Customizing the traffic display on the Navigation Map Page:
1) Select the Navigation Map Page.
FLIGHT
INSTRUMENTS
2) Press the MENU Key.
3) With Map Setup highlighted, press the ENT Key (Figure 6-104).
4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-105).
5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-106).
• TRAFFIC – Turns the display of traffic data on or off
EIS
• TRAFFIC MODE – Selects the traffic mode for display; select from:
- All Traffic - Displays all traffic
AUDIO PANEL
& CNS
- TA/PA - Displays Traffic Alerts and Proximity Advisories
- TA ONLY - Displays Traffic Alerts only
• TRAFFIC SMBL – Selects the maximum range at which traffic symbols are shown
• TRAFFIC LBL – Selects the maximum range at which traffic labels are shown with the option to turn off
FLIGHT
MANAGEMENT
6) Turn the small FMS Knob to scroll through options (ON/OFF, range settings, etc.).
7) Press the ENT Key to select an option.
AFCS
HAZARD
AVOIDANCE
8) Press the FMS Knob or CLR Key to return to the Navigation Map Page.
APPENDICES
ADDITIONAL
FEATURES
Figure 6-104 Navigation Map
Page Menu
INDEX
Figure 6-105 Navigation Map Page Setup Menu
368
Figure 6-106 Navigation Map Page Setup Menu,
Traffic Group
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
HAZARD AVOIDANCE
SYSTEM
OVERVIEW
TAS ALERTS
NOTE: Refer to the TCAD 9900BX/TAS 620 documentation for information on alerts generated by the TAS
FLIGHT
INSTRUMENTS
equipment.
When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur:
• A “Traffic” voice alert is generated followed by the clock position, relative altitude and range of the TA.
• A TRAFFIC Annunciation appears at the top right of the airspeed on the PFD, flashing for 5 seconds and
remaining displayed until no TAs are detected in the area.
EIS
• The PFD Inset Map is automatically displayed with TA traffic.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Inset Map
Displays When
TA is Detected
HAZARD
AVOIDANCE
Figure 6-107 Traffic Annunciation (PFD)
AFCS
TAS VOICE ALERTS
To listen to an update of Traffic Advisories select the MUTE Softkey twice. If no Traffic Advisories (TAs) are
in effect, a “No Advisories” statement is heard. ADDITIONAL
FEATURES
Muting the TAS voice alert in progress:
1) Select the Traffic Map Page.
2) Select the MUTE Softkey while the voice alert is playing. Subsequent voice alerts will be heard.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Corvalis/Corvalis TT
369
SYSTEM
OVERVIEW
HAZARD AVOIDANCE
SYSTEM STATUS
FLIGHT
INSTRUMENTS
NOTE: Refer to the TCAD 9900BX/TAS 620 documentation for information on the operating mode.
The traffic mode is annunciated in the upper left corner of the Traffic Map Page.
Traffic Mode Annunciation
(Traffic Map Page)
Mode
OPERATING
TAS Operating
EIS
Traffic Display Enabled Icon
(Other Maps)
FAIL
TAS Failed*
AUDIO PANEL
& CNS
* See Table 6-22 for additional failure annunciations
Table 6-21 TAS Modes
If the unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page.
FLIGHT
MANAGEMENT
Traffic Map Page
Annunciation
NO DATA
DATA FAILED
HAZARD
AVOIDANCE
FAILED
Description
Data is not being received from the TAS unit
Data is being received from the TAS unit, but the
unit is self-reporting a failure
Incorrect data format received from the TAS unit
Table 6-22 TAS Failure Annunciations
AFCS
The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of
maps on which traffic can be displayed.
ADDITIONAL
FEATURES
TA OFF SCALE
APPENDICES
Traffic Status Banner
Annunciation
TA X.X ± XX ↕
TRFC FAIL
INDEX
NO TRFC DATA
Description
A Traffic Advisory is outside the selected display
range*
Annunciation is removed when traffic comes within
the selected display range
System cannot determine bearing of Traffic
Advisory**
Annunciation indicates distance in nm, altitude
separation in hundreds of feet, and altitude trend
arrow (climbing/descending)
TAS unit has failed (unit is self-reporting a failure or
sending incorrectly formatted data)
Data is not being received from the TAS unit
*Shown as symbol on Traffic Map Page
**Shown in center of Traffic Map Page
Table 6-23 TAS Traffic Status Annunciations
370
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
FLIGHT
INSTRUMENTS
NOTE: The approved Aircraft Flight Manual (AFM) always supersedes the information in this Pilot’s Guide.
NOTE: A failure of the primary (#1) GIA 63/63W Integrated Avionics Unit (IAU) results in loss of the flight
director. Any IAU failure results in loss of the autopilot and manual electric trim.
• GSA 81 AFCS Servos (2)
• GDU 1042/1044/1044B Multi-Function Display
(MFD)
• GTA 82 Pitch Trim Adapter (1)
AUDIO PANEL
& CNS
• GDU 1040/1044B Primary Flight Display (PFD)
EIS
The GFC 700 is a digital Automatic Flight Control System (AFCS), fully integrated within the System avionics
architecture. The System Overview section provides a block diagram to support this system description.
GFC 700 AFCS functionality in the Cessna Corvalis aircraft is distributed across the following Line Replaceable
Units (LRUs):
• GSM 85 Servo Mounts (2)
• GIA 63/63W Integrated Avionics Units (2)
FLIGHT
MANAGEMENT
The GFC 700 AFCS can be divided into these main operating functions:
• Flight Director (FD) — Flight director operation takes place within the primary (#1) IAU. Flight director
commands are displayed on the PFD. The flight director provides:
– Command Bars showing pitch/roll guidance
HAZARD
AVOIDANCE
– Pitch/roll mode selection and processing
– Autopilot communication
AFCS
• Autopilot (AP) — Autopilot operation occurs within the pitch and roll servos and the pitch trim adapter
and provides servo monitoring and automatic flight control in response to flight director steering commands,
AHRS attitude and rate information, and airspeed.
• Manual Electric Trim (MET) — The pitch trim adapter provides manual electric trim capability when the
autopilot is not engaged.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
371
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
7.1 AFCS CONTROLS
FLIGHT
INSTRUMENTS
The following dedicated AFCS keys are located on the bezel of the MFD:
1
2
3
4
5
EIS
6
AUDIO PANEL
& CNS
7
8
AP Key
HDG Key
NAV Key
APR Key
VS Key
FLC Key
FD Key
Engages/disengages the autopilot
Selects/deselects Heading Select Mode
Selects/deselects Navigation Mode
Selects/deselects Approach Mode
Selects/deselects Vertical Speed Mode
Selects/deselects Flight Level Change Mode
Activates/deactivates the flight director only
ALT Key
Pressing once turns on the flight director in the default pitch and roll modes. Pressing again deactivates the flight director and removes the Command Bars. If the autopilot is engaged, the key is disabled.
Selects/deselects Altitude Hold Mode
VNV Key (GDU
1044/1044B only)
10 BC Key (GDU 1044B
only)
11 NOSE UP/
NOSE DN Keys
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
9
Selects/deselects Vertical Path Tracking Mode for Vertical Navigation flight
control
Selects/deselects Backcourse Mode
Control the mode reference in Pitch Hold, Vertical Speed, and Flight Level
Change modes
1
7
2
8
3
9
4
10
5
APPENDICES
11
6
INDEX
Figure 7-1 Dedicated MFD AFCS Controls (GDU 1044B Shown)
372
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
The following AFCS controls are located in the cockpit separately from the PFD and MFD:
AP DISC Switch
(Autopilot Disconnect)
Disengages the autopilot and interrupts pitch trim operation
FLIGHT
INSTRUMENTS
The AP DISC Switch is located on the control stick.
This switch may be used to acknowledge an autopilot disconnect alert and
mute the associated aural tone.
EIS
While pressed, allows manual control of the aircraft while the autopilot is
CWS Button
(Control Wheel Steering) engaged and synchronizes the flight director’s Command Bars with the
current aircraft pitch (if not in Glideslope Mode) and roll (if in Roll Hold
Mode)
AUDIO PANEL
& CNS
Upon release of the CWS Button, the flight director may establish new
reference points, depending on the current pitch and roll modes. CWS
operation details are discussed in the flight director modes section.
The CWS Button is located on the control stick.
GA Switch (Go Around)
Disengages the autopilot and selects flight director Go Around Mode
FLIGHT
MANAGEMENT
If an approach procedure is loaded, this switch also activates the missed
approach when the selected navigation source is GPS or when the navigation
source is VOR/LOC and a valid frequency has been tuned.
The GA Switch is located on the throttle.
Used to command manual electric trim
(Manual Electric Trim)
This composite switch is split into left and right sides. The left switch is
the ARM contact and the right switch controls the DN (forward) and UP
(rearward) contacts. The MET ARM Switch can be used to disengage the
autopilot and to acknowledge an autopilot disconnect alert and mute the
associated aural tone.
HAZARD
AVOIDANCE
MET Switch
AFCS
ADDITIONAL
FEATURES
Manual trim commands are generated only when both sides of the switch
are operated simultaneously. If either side of the switch is active separately for
more than three seconds, MET function is disabled and ‘PTRM’ is displayed
as the AFCS Status Annunciation on the PFD. The function remains disabled
until both sides of the switch are inactivated.
The trim switch is located on the control stick; push up/down for MET.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
373
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
7.2 FLIGHT DIRECTOR OPERATION
FLIGHT
INSTRUMENTS
The flight director function provides pitch and roll commands to the AFCS and displays them on the PFD. With the flight director activated, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (+20°/-15°) and roll (22°) angles, vertical acceleration, and roll rate are limited to
values established during AFCS certification. The flight director also provides commands to the autopilot.
ACTIVATING THE FLIGHT DIRECTOR
EIS
An initial press of a key listed in Table 7-1 (when the flight director is not active) activates the flight director
in the listed modes. The flight director may be turned off and the Command Bars removed from the display by
pressing the FD Key again. The FD Key is disabled when the autopilot is engaged.
AUDIO PANEL
& CNS
Control Pressed
ALT Key
VS Key
FLC Key
VNV Key
Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Takeoff (on ground)
Go Around (in air)
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
NAV Key
Navigation**
BC Key (GDU 1044B
only)
Backcourse***
APR Key
Approach**
HDG Key
Heading Select
FLIGHT
MANAGEMENT
FD Key
AP Key
CWS Button
AFCS
HAZARD
AVOIDANCE
GA Switch
ADDITIONAL
FEATURES
Modes Selected
ROL
ROL
ROL
TO
GA
ROL
ROL
ROL
ROL
GPS
VOR
LOC
BC
GPS
VOR
LOC
HDG
Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Takeoff (on ground)
TO
Go Around (in air)
GA
Altitude Hold
ALT
Vertical Speed
VS
Flight Level Change
FLC
Vertical Path Tracking* VPTH
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
APPENDICES
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS
course before NAV or APR Key press activates flight director.
***The selected navigation receiver must have a valid LOC signal before BC Key press
activates flight director.
INDEX
Table 7-1 Flight Director Activation
374
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
AFCS STATUS BOX
Lateral Modes
Active
Vertical Modes
Active
Mode
Reference
Armed
EIS
Armed
Autopilot
Status
FLIGHT
INSTRUMENTS
Flight director mode annunciations are displayed on the PFD when the flight director is active. Autopilot status is displayed in the center of the AFCS Status Box. Lateral flight director modes are displayed on the left
and vertical on the right. Armed modes are displayed in white and active in green.
AFCS Status Box
AUDIO PANEL
& CNS
Selected
Altitude
FLIGHT
MANAGEMENT
Command
Bars
HAZARD
AVOIDANCE
AFCS
Figure 7-2 PFD AFCS Display
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
375
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
COMMAND BARS
FLIGHT
INSTRUMENTS
Upon activation of the flight director, Command Bars are displayed on the PFD as a single magenta cue. The
Command Bars move together vertically to indicate pitch commands, and bank left or right to indicate roll
commands. The Command Bars do not override the aircraft symbol.
If the attitude information sent to the flight director becomes invalid or unavailable, the Command Bars are
removed from the display. The flight director Command Bars also disappear if the pitch exceeds +30˚/-20˚ or
bank exceeds 65˚.
EIS
Command Bars
AUDIO PANEL
& CNS
Aircraft Symbol
Figure 7-3 Command Bars
FLIGHT
MANAGEMENT
FLIGHT DIRECTOR MODES
Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise
specified, all mode keys are alternate action (i.e., press on, press off). In the absence of specific mode selection,
the flight director reverts to the default pitch and/or roll modes(s).
HAZARD
AVOIDANCE
Armed modes are annunciated in white and active in green in the AFCS Status Box. Under normal operation
when the control for the active flight director mode is pressed, the flight director reverts to the default modes(s)
for the axis(es). Automatic transition from armed to active mode is indicated by the white armed mode
annunciation moving to the green active mode field and flashing for 10 seconds.
ADDITIONAL
FEATURES
AFCS
If the information required to compute a flight director mode becomes invalid or unavailable, the flight
director automatically reverts to the default mode for that axis. A flashing yellow mode annunciation and
annunciator light indicate loss of sensor (ADC) or navigation data (VOR, LOC, GPS, SBAS) required to compute
commands. When such a loss occurs, the system automatically begins to roll the wings level (enters Roll Hold
Mode) or maintain the pitch angle (enters Pitch Hold Mode), depending on the affected axis. The flashing
annunciation stops when the affected mode key is pressed or another mode for the axis is selected. If after 10
seconds no action is taken, the flashing annunciation stops.
APPENDICES
Figure 7-4 Loss of VOR Signal
INDEX
The flight director is automatically disabled if the attitude information required to compute the default flight
director modes becomes invalid or unavailable.
376
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
7.3 VERTICAL MODES
Description
Pitch Hold
Flight Level Change
VNV Target Altitude Capture
Glideslope
1 kt
ADDITIONAL
FEATURES
Go Around
100 fpm
AFCS
Glidepath***
0.5°
HAZARD
AVOIDANCE
Vertical Path Tracking
Holds aircraft pitch attitude; may
be used to climb/descend to the (default)
PIT
-15° to +20°
Selected Altitude
Captures the Selected Altitude
*
ALTS
Holds current Altitude Reference ALT Key ALT nnnnn ft
Holds aircraft vertical speed; may
-2000 to
be used to climb/descend to the
VS Key VS nnnn fpm
+1500 fpm
Selected Altitude
80 to 200 kts
Holds aircraft airspeed while
(350)
aircraft is climbing/descending to FLC Key FLC nnn kt
80 to 210 kts
the Selected Altitude
(400)
Captures and tracks descent legs
VNV
VPTH
of an active vertical profile
Key
Captures the Vertical Navigation
**
ALTV
(VNV) Target Altitude
Captures and tracks the SBAS
GP
glidepath on approach
APR
Key
Captures and tracks the ILS
GS
glideslope on approach
Disengages the autopilot and
GA
commands a constant pitch angle
GA
7°
Switch
and wings level
Reference
Change
Increment
FLIGHT
MANAGEMENT
Vertical Speed
Reference
Range
AUDIO PANEL
& CNS
Selected Altitude Capture
Altitude Hold
Control Annunciation
EIS
Vertical Mode
FLIGHT
INSTRUMENTS
Table 7-2 lists the vertical modes with their corresponding controls and annunciations. The mode reference is
displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes. The NOSE UP/NOSE DN Keys can be used to change the vertical mode reference while operating under Pitch
Hold, Vertical Speed, or Flight Level Change Mode. Increments of change and acceptable ranges of values for
each of these references using the NOSE UP/NOSE DN Keys are also listed in the table.
APPENDICES
* ALTS is armed automatically when PIT, VS, FLC, or GA is active, and under VPTH when the Selected Altitude is to be captured
instead of the VNV Target Altitude.
** ALTV is armed automatically under VPTH when the VNV Target Altitude is to be captured instead of the Selected Altitude.
***GP is available in installations with GIA 63W IAUs when SBAS is available.
Table 7-2 Flight Director Vertical Modes
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
377
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
PITCH HOLD MODE (PIT)
FLIGHT
INSTRUMENTS
When the flight director is activated (the FD Key is pressed), Pitch Hold Mode is selected by default. Pitch
Hold Mode is indicated as the active pitch mode by the green annunciation ‘PIT’. This mode may be used for
climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is
automatically armed when Pitch Hold Mode is activated.
EIS
In Pitch Hold Mode, the flight director maintains a constant pitch attitude, the pitch reference. The pitch
reference is set to the aircraft pitch attitude at the moment of mode selection. If the aircraft pitch attitude
exceeds the flight director pitch command limitations, the flight director commands a pitch angle equal to the
nose-up/down limit.
CHANGING THE PITCH REFERENCE
AUDIO PANEL
& CNS
When operating in Pitch Hold Mode, the pitch reference can be adjusted by:
• Using the NOSE UP/NOSE DN Keys
• By pressing the CWS Button, hand-flying the aircraft to establish a new pitch reference, then releasing the
CWS Button
FLIGHT
MANAGEMENT
Pitch Hold
Mode Active
Selected Altitude
Capture Mode Armed
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Selected
Altitude
Command Bars Maintain
Desired Pitch Reference
INDEX
APPENDICES
Figure 7-5 Pitch Hold Mode
378
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
SELECTED ALTITUDE CAPTURE MODE (ALTS)
Selected Altitude Capture Mode is automatically armed with activation of the following modes:
• Go Around
• Vertical Speed
• Vertical Path Tracking (if the Selected Altitude is to
be captured instead of the VNV Target Altitude)
• Flight Level Change
FLIGHT
INSTRUMENTS
• Pitch Hold
EIS
The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 7-5 for example). The ALT Knob is used to set the Selected Altitude (shown above the Altimeter) until Selected Altitude Capture
Mode becomes active.
AUDIO PANEL
& CNS
As the aircraft nears the Selected Altitude, the flight director automatically transitions to Selected Altitude
Capture Mode with Altitude Hold Mode armed (Figure 7-6). This automatic transition is indicated by the green
‘ALTS’ annunciation flashing for up to 10 seconds and the appearance of the white ‘ALT” annunciation. The
Selected Altitude is shown as the Altitude Reference beside the ‘ALTS’ annunciation.
FLIGHT
MANAGEMENT
At 50 feet from the Selected Altitude, the flight director automatically transitions from Selected Altitude
Capture to Altitude Hold Mode and holds the Selected Altitude (shown as the Altitude Reference). As Altitude
Hold Mode becomes active, the white ‘ALT’ annunciation moves to the active pitch mode field and flashes green
for 10 seconds to indicate the automatic transition.
Altitude Reference
(in this case, equal to
Selected Altitude)
HAZARD
AVOIDANCE
Flash up to 10 sec, Indicating Automatic Transition
Figure 7-6 Automatic Mode Transitions During Altitude Capture
AFCS
CHANGING THE SELECTED ALTITUDE
ADDITIONAL
FEATURES
NOTE: Pressing the CWS Button while in Selected Altitude Capture Mode does not cancel the mode.
Use of the ALT Knob to change the Selected Altitude while Selected Altitude Capture Mode is active causes
the flight director to revert to Pitch Hold Mode with Selected Altitude Capture Mode armed for the new
Selected Altitude.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
379
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
ALTITUDE HOLD MODE (ALT)
FLIGHT
INSTRUMENTS
Altitude Hold Mode can be activated by pressing the ALT Key; the flight director maintains the current aircraft
altitude (to the nearest 10 feet) as the Altitude Reference. The flight director’s Altitude Reference, shown in the
AFCS Status Box, is independent of the Selected Altitude, displayed above the Altimeter. Altitude Hold Mode
active is indicated by a green ‘ALT’ annunciation in the AFCS Status Box.
Altitude Hold Mode is automatically armed when the flight director is in Selected Altitude Capture Mode (see
Figure 7-6). Selected Altitude Capture Mode automatically transitions to Altitude Hold Mode when the altitude
error is less than 50 feet. In this case, the Selected Altitude becomes the flight director’s Altitude Reference.
EIS
CHANGING THE ALTITUDE REFERENCE
NOTE: Turning the ALT Knob while in Altitude Hold Mode changes the Selected Altitude, but not the flight
AUDIO PANEL
& CNS
director’s Altitude Reference, and does not cancel the mode.
With the CWS Button depressed, the aircraft can be hand-flown to a new Altitude Reference. When the
CWS Button is released at the desired altitude, the new altitude is established as the Altitude Reference.
FLIGHT
MANAGEMENT
Altitude Hold
Mode Active
Altitude
Reference
HAZARD
AVOIDANCE
Selected
Altitude
ADDITIONAL
FEATURES
AFCS
Selected
Altitude
Bug
Command Bars Hold Pitch Attitude
to Maintain Altitude Reference
INDEX
APPENDICES
Figure 7-7 Altitude Hold Mode
380
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
VERTICAL SPEED MODE (VS)
FLIGHT
INSTRUMENTS
Vertical Speed Mode is activated by pressing the VS Key. The annunciation ‘VS’ appears in the active pitch
mode field, along with the Vertical Speed Reference to the right; the Vertical Speed Reference is also displayed
above or below the Vertical Speed Indicator, depending on whether the aircraft is climbing or descending. In Vertical Speed Mode, the flight director acquires and maintains a Vertical Speed Reference as it climbs or
descends to the Selected Altitude (shown above the Altimeter). Current aircraft vertical speed becomes the
Vertical Speed Reference at the moment of Vertical Speed Mode engagement. A Vertical Speed Reference Bug
corresponding to the Vertical Speed Reference is shown on the indicator.
EIS
CHANGING THE VERTICAL SPEED REFERENCE
The Vertical Speed Reference (shown both in the AFCS Status Box and above/below the Vertical Speed
Indicator) may be changed:
AUDIO PANEL
& CNS
• Using the NOSE UP/NOSE DN Keys
• By pressing the CWS Button, hand-flying the aircraft to a new Vertical Speed Reference, then releasing the
CWS Button
FLIGHT
MANAGEMENT
NOTE: If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed.
To adjust the Altitude Reference in this case, the CWS Button must be pressed again after the Selected
Altitude is reached..
Vertical Speed
Reference
Selected Altitude
Capture Mode
Armed
Vertical
Speed
Reference
AFCS
Selected
Altitude
HAZARD
AVOIDANCE
Vertical Speed
Mode Active
ADDITIONAL
FEATURES
Vertical
Speed
Reference
Bug
APPENDICES
Command Bars Indicate Climb to
Attain Vertical Speed Reference
Figure 7-8 Vertical Speed Mode
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
381
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
FLIGHT LEVEL CHANGE MODE (FLC)
FLIGHT
INSTRUMENTS
Flight Level Change Mode is selected by pressing the FLC Key. This mode acquires and maintains the
Airspeed Reference while climbing or descending to the Selected Altitude (shown above the Altimeter). When
Flight Level Change Mode is active, the flight director continuously monitors Selected Altitude, airspeed, and
altitude.
EIS
NOTE: The Selected Altitude should be set before engaging Flight Level Change Mode.
The Airspeed Reference is set to the current airspeed upon mode activation. Flight Level Change Mode
is indicated by an ‘FLC’ annunciation beside the Airspeed Reference in the AFCS Status Box. The Airspeed
Reference is also displayed directly above the Airspeed Indicator, along with a bug corresponding to the
Airspeed Reference along the tape.
AUDIO PANEL
& CNS
Engine power must be adjusted to allow the autopilot to fly the aircraft at a pitch attitude corresponding to the desired flight profile (climb or descent) while maintaining the Airspeed Reference. The flight director
maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not
allow the aircraft to climb or descend away from the Selected Altitude.
FLIGHT
MANAGEMENT
CHANGING THE AIRSPEED REFERENCE
The Airspeed Reference (shown in both the AFCS Status Box and above the Airspeed Indicator) may be
adjusted by:
• Using the NOSE UP/NOSE DN Keys
HAZARD
AVOIDANCE
• Pressing the CWS Button, hand-flying the aircraft to a new airspeed, then releasing the CWS Button to
establish the new Airspeed Reference
NOTE: If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
To adjust the Altitude Reference in this case, the CWS Button must be pressed again after the Selected
Altitude is reached.
382
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
Airspeed
Reference
SYSTEM
OVERVIEW
Flight Level Change
Mode Active
Selected Altitude
Capture Mode
Armed
FLIGHT
INSTRUMENTS
Airspeed
Reference
Selected
Altitude
EIS
AUDIO PANEL
& CNS
Airspeed
Reference
Bug
FLIGHT
MANAGEMENT
Command Bars Indicate Climb
to Attain Selected Altitude
Figure 7-9 Flight Level Change Mode
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
383
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
VERTICAL NAVIGATION MODES (VPTH, ALTV)
FLIGHT
INSTRUMENTS
NOTE: VNV is disabled when parallel track or dead reckoning mode is active.
NOTE: The Selected Altitude takes precedence over any other vertical constraints.
Vertical Navigation (VNV) flight control is available for enroute/terminal cruise and descent operations any
time that VNV flight planning is available. Refer to the Flight Management Section for more information on
VNV flight plans. Conditions for availability include, but are not limited to:
EIS
• The selected navigation source is GPS.
• A VNV flight plan (with at least one altitude-constrained waypoint) or vertical direct-to is active.
AUDIO PANEL
& CNS
• VNV is enabled (VNV ENBL Softkey pressed on the MFD).
• Crosstrack error is valid and within certain limits.
• Desired/actual track are valid or track angle error is within certain limits.
FLIGHT
MANAGEMENT
• The VNV Target Altitude of the active waypoint is no more than 250 ft above the current aircraft altitude.
HAZARD
AVOIDANCE
The flight director may be armed for VNV at any time, but no target altitudes are captured during a climb. The Command Bars provide vertical profile guidance based on specified altitudes (entered manually or loaded
from the database) at waypoints in the active flight plan or vertical direct-to. The appropriate VNV flight control
modes are sequenced by the flight director to follow the path defined by the vertical profile. Upon reaching
the last waypoint in the VNV flight plan, the flight director transitions to Altitude Hold Mode and cancels any
armed VNV modes.
VERTICAL PATH TRACKING MODE (VPTH)
NOTE: If another pitch mode key is pressed while Vertical Path Tracking Mode is selected, Vertical Path
AFCS
Tracking Mode reverts to armed.
NOTE: Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode. The
ADDITIONAL
FEATURES
autopilot guides the aircraft back to the descent path upon release of the CWS Button.
INDEX
APPENDICES
When a vertical profile (VNV flight plan) is active and the VNV Key is pressed, Vertical Path Tracking
Mode is armed in preparation for descent path capture. ‘VPTH’ (or ‘/V’ when Glidepath or Glideslope Mode
is concurrently armed) is annunciated in white in addition to previously armed modes. If applicable, the
appropriate altitude capture mode is armed for capture of the next VNV Target Altitude (ALTV) or the Selected
Altitude (ALTS), whichever is greater.
Figure 7-10 Vertical Path Tracking Armed Annunciations
384
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
Prior to descent path interception, the Selected Altitude must be set below the current aircraft altitude
by at least 75 feet. For the flight director to transition from Altitude Hold to Vertical Path Tracking Mode,
acknowledgment is required within 5 minutes of descent path interception by:
FLIGHT
INSTRUMENTS
• Pressing the VNV Key
• Adjusting the Selected Altitude
If acknowledgment is not received within 1 minute of descent path interception, the white ‘VPTH’
annunciation starts to flash. Flashing continues until acknowledged or the descent path is intercepted. If
the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the
descent is not captured.
EIS
In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the Navigation Status Box
and the “Vertical track” voice message, VNV indications (VNV Target Altitude, vertical deviation, and vertical
speed required) appear on the PFD in magenta (Figure 7-11).
AUDIO PANEL
& CNS
Altitude Hold
Mode Active
Vertical Path Tracking
Armed, (Flashing Indicates
Acknowledgment Required)
FLIGHT
MANAGEMENT
Selected
Altitude Below
VNV Target
VNV Target
Altitude
HAZARD
AVOIDANCE
Vertical
Deviation
Indicator
Terminal
Phase
of Flight
ADDITIONAL
FEATURES
GPS is
Selected
Navigation
Source
AFCS
Required
Vertical
Speed Bug
Figure 7-11 Vertical Path Capture
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
385
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
When a descent leg is captured (i.e., vertical deviation becomes valid), Vertical Path Tracking becomes
active and tracks the descent profile (Figure 7-12). An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as
appropriate.
FLIGHT
INSTRUMENTS
Vertical Path
Tracking Active
VNV Target Altitude
Capture Armed
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
VNV Target
Altitude
HAZARD
AVOIDANCE
GPS is
Selected
Navigation
Source
Terminal
Phase of
Flight
Required
Vertical
Speed
Indication
Command Bars Indicate Descent to
Maintain Required Vertical Speed
Vertical
Deviation
Indicator
Figure 7-12 Vertical Path Tracking Mode
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
If the Altimeter’s barometric setting is adjusted while Vertical Path Tracking is active, the flight director
increases/decreases the descent rate by up to 500 fpm to re-establish the aircraft on the descent path (without
commanding a climb). Adjusting the altimeter barometric setting creates discontinuities in VNV vertical
deviation, moving the descent path. For large adjustments, it may take several minutes for the aircraft to reestablish on the descent path. If the change is made while nearing a waypoint with a VNV Target Altitude,
the aircraft may not re-establish on the descent path in time to meet the vertical constraint.
386
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
Automatic Reversion to Pitch Hold Mode
Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to
revert to Pitch Hold Mode:
FLIGHT
INSTRUMENTS
• Vertical deviation exceeds 200 feet during an overspeed condition.
• Vertical deviation experiences a discontinuity that both exceeds 200 feet in magnitude and results in the
vertical deviation exceeding 200 feet in magnitude. Such discontinuities are usually caused by flight plan
changes that affect the vertical profile.
• Vertical deviation becomes invalid (the Vertical Deviation Indicator is removed from the PFD).
EIS
• A display enters Reversionary Mode (this does not apply to an active vertical direct-to).
Unless VNV is disabled, Vertical Path Tracking Mode and the appropriate altitude capture mode become
armed following the reversion to Pitch Hold Mode to allow for possible profile recapture.
AUDIO PANEL
& CNS
Non-Path Descents
FLIGHT
MANAGEMENT
Pitch Hold, Vertical Speed, and Flight Level Change modes can also be used to fly non-path descents
while VNV flight control is selected. If the VS or FLC Key is pressed while Vertical Path Tracking Mode is
selected, Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to
allow profile re-capture.
Figure 7-13 Flight Level Change VNV Non-Path Descent
HAZARD
AVOIDANCE
To prevent immediate profile re-capture, the following must be satisfied:
• At least 10 seconds have passed since the non-path transition was initiated
• Vertical deviation from the profile has exceeded 250 feet, but is now less than 200 feet
AFCS
Pressing the VNV Key twice re-arms Vertical Path Tracking for immediate profile re-capture.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
387
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
VNV TARGET ALTITUDE CAPTURE MODE (ALTV)
NOTE: Armed VNV Target Altitude and Selected Altitude capture modes are mutually exclusive. However,
FLIGHT
INSTRUMENTS
Selected Altitude Capture Mode is armed implicitly (not annunciated) whenever VNV Target Altitude Capture
Mode is armed.
EIS
VNV Target Altitude Capture is analogous to Selected Altitude Capture Mode and is armed automatically
after the VNV Key is pressed and the next VNV Target Altitude is to be intercepted before the Selected
Altitude. The annunciation ‘ALTV’ indicates that the VNV Target Altitude is to be captured. VNV Target
Altitudes are shown in the active flight plan or vertical direct-to, and can be entered manually or loaded
from a database (see the GPS Navigation Section for details). At the same time as “TOD within 1 minute”
is annunciated in the Navigation Status Box, the active VNV Target Altitude is displayed above the Vertical
Speed Indicator (see Figure 7-11).
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
As the aircraft nears the VNV Target Altitude, the flight director automatically transitions to VNV Target
Altitude Capture Mode with Altitude Hold Mode armed. This automatic transition is indicated by the green
‘ALTV’ annunciation flashing for up to 10 seconds and the appearance of the white ‘ALT” annunciation. The
VNV Target Altitude is shown as the Altitude Reference beside the ‘ALTV’ annunciation and remains displayed
above the Vertical Speed Indicator. The Required Vertical Speed Indication (RVSI) is removed once VNV
Target Altitude Capture Mode becomes active.
HAZARD
AVOIDANCE
At 50 feet from the VNV Target Altitude, the flight director automatically transitions from VNV Target
Altitude Capture to Altitude Hold Mode and tracks the level leg. As Altitude Hold Mode becomes active, the
white ‘ALT’ annunciation moves to the active vertical mode field and flashes green for 10 seconds to indicate
the automatic transition. The flight director automatically arms Vertical Path Tracking, allowing upcoming
descent legs to be captured and subsequently tracked.
AFCS
Altitude Reference (in
this case, equal to VNV
Altitude Target)
ADDITIONAL
FEATURES
Flash up to 10 sec, Indicating Automatic Transition
Figure 7-14 Automatic Mode Transitions During Altitude Capture
APPENDICES
Changing the VNV Target Altitude
NOTE: Pressing the CWS Button while in VNV Target Altitude Capture Mode does not cancel the mode.
INDEX
Changing the current VNV Target Altitude while VNV Target Altitude Capture Mode is active causes the
flight director to revert to Pitch Hold Mode. Vertical Path Tracking and the appropriate altitude capture
mode are armed in preparation to capture the new VNV Target Altitude or the Selected Altitude, depending
on which altitude is to be intercepted first.
VNV target altitudes can be changed while editing the active flight plan (see the Flight Management
Section for details).
388
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
GLIDEPATH MODE (GP) (SBAS ONLY)
NOTE: Pressing the CWS Button while Glidepath Mode is active does not cancel the mode. The autopilot
FLIGHT
INSTRUMENTS
guides the aircraft back to the glidepath upon release of the CWS Button.
Glidepath Mode is available only in installations with GIA 63W IAUs when SBAS is available. Glidepath
Mode is used to track the SBAS-based glidepath. When Glidepath Mode is armed, ‘GP’ is annunciated in white
in the AFCS Status Box.
Selecting Glidepath Mode:
EIS
1) Ensure a GPS approach with vertical guidance (LPV, LNAV/VNAV, LNAV+V) is loaded into the active flight plan.
The active waypoint must be part of the flight plan (cannot be a direct-to a waypoint not in the flight plan).
2) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources).
AUDIO PANEL
& CNS
3) Press the APR Key.
NOTE: Some RNAV (GPS) approaches provide a vertical descent angle as an aid in flying a stabilized
FLIGHT
MANAGEMENT
approach. These approaches are NOT considered Approaches with Vertical Guidance (APV). Approaches
that are annunciated on the HSI as LNAV or LNAV+V are considered Nonprecision Approaches (NPA) and
are flown to an MDA even though vertical glidepath (GP) information may be provided.
WARNING: When flying an LNAV approach (with vertical descent angle) with the autopilot coupled, the
aircraft will not level off at the MDA even if the MDA is set in the altitude preselect.
HAZARD
AVOIDANCE
Upon reaching the glidepath, the flight director transitions to Glidepath Mode and begins to capture and
track the glidepath.
Figure 7-15 Glidepath Mode Armed
AFCS
Once the following conditions have been met, the glidepath can be captured:
• The active waypoint is at or after the final approach fix (FAF).
• Vertical deviation is valid.
ADDITIONAL
FEATURES
• The CDI is at less than full scale deviation
• Automatic sequencing of waypoints has not been suspended (no ‘SUSP’ annunciation on the HSI)
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
389
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
Glidepath
Mode Active
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
GPS Approach
Mode Active
HAZARD
AVOIDANCE
GPS is Selected
Navigation
Source
LNAV
Approach
Active
Command Bars Indicate
Descent on Glidepath
Glidepath
Indicator
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 7-16 Glidepath Mode
390
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
GLIDESLOPE MODE (GS)
NOTE: Pressing the CWS Button while Glideslope Mode is active does not cancel the mode. The autopilot
FLIGHT
INSTRUMENTS
guides the aircraft back to the glideslope upon release of the CWS Button.
Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope. When Glideslope
Mode is armed (annunciated as ‘GS’ in white), LOC Approach Mode is armed as the lateral flight director
mode.
Selecting Glideslope Mode:
EIS
1) Ensure a valid localizer frequency is tuned.
2) Ensure that LOC is the selected navigation source (use the CDI Softkey to cycle through navigation sources).
AUDIO PANEL
& CNS
3) Press the APR Key.
Or:
1) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources).
2) Ensure a LOC/ILS approach is loaded into the active flight plan.
FLIGHT
MANAGEMENT
3) Ensure the corresponding LOC frequency is tuned.
4) Press the APR Key.
HAZARD
AVOIDANCE
Figure 7-17 Glideslope Mode Armed
Once LOC is the navigation source, the localizer and glideslope can be captured. Upon reaching the glideslope,
the flight director transitions to Glideslope Mode and begins to intercept and track the glideslope.
Active ILS
Frequency Tuned
Approach
Mode Active
Glideslope
Mode Active
AFCS
ADDITIONAL
FEATURES
APPENDICES
Command Bars Indicate Descent
on Localizer/Glideslope Path
Figure 7-18 Glideslope Mode
190-00552-05 Rev. A
INDEX
NAV2 (localizer) is Selected
Navigation Source
Glideslope
Indicator
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
391
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
GO AROUND MODE (GA)
FLIGHT
INSTRUMENTS
Pushing the GA Switch engages the flight director in a wings-level, pitch-up attitude, allowing the execution
of a missed approach or a go around. This mode is a coupled pitch and roll mode and is annunciated as ‘GA’
in both the active pitch and roll mode fields. Go Around Mode disengages the autopilot and arms Selected
Altitude Capture Mode automatically. Subsequent autopilot engagement is allowed. Attempts to modify the
aircraft attitude (i.e., with the CWS Button or NOSE UP/NOSE DN Keys) result in reversion to Pitch and Roll
Hold modes.
EIS
Go Around Mode Active
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Autopilot Disconnect Annunciation
Flashes Yellow 5 sec
Command Bars Indicate Climb
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 7-19 Go Around Mode
392
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
7.4 LATERAL MODES
Lateral Mode
Description
Roll Hold
ROL
22°
HDG
Key
HDG
22°
GPS
22°
22° Capture
10° Track
22° Capture
10° Track
Navigation, GPS
Navigation, VOR Enroute Capture/Track
Navigation, LOC Capture/Track
(No Glideslope)
Captures and tracks the
selected navigation source
(GPS, VOR, LOC)
Backcourse
LOC
BC Key
(GDU
1044B
only)
Approach, GPS
BC
GPS
Approach, VOR Capture/Track
Captures and tracks the
selected navigation source APR Key
(GPS, VOR, LOC)
GA
Switch
LOC
GA
22°
22° Capture
10° Track
22° Capture
10° Track
Wings Level
ADDITIONAL
FEATURES
Disengages the autopilot
and commands a constant
pitch angle and wings level
VAPP
22° Capture
10° Track
AFCS
Approach, LOC Capture/Track
(Glideslope Mode automatically armed)
Go Around
VOR
HAZARD
AVOIDANCE
Captures and tracks
a localizer signal for
backcourse approaches
NAV
Key
FLIGHT
MANAGEMENT
(default)
AUDIO PANEL
& CNS
Heading Select
Maximum Roll
Command Limit
EIS
Holds the current aircraft
roll attitude or rolls the
wings level, depending
on the commanded bank
angle
Captures and tracks the
Selected Heading
Control Annunciation
FLIGHT
INSTRUMENTS
The GFC 700 offers the lateral modes listed in Table 7-3. Refer to the vertical modes section for information
regarding Go Around Mode:
The GFC 700 may generate a lower bank angle than the maximum roll command limit in degrees indicated in the
table above by the amount needed to produce a turn rate equal to or less than standard rate.
Table 7-3 Lateral Modes
APPENDICES
The CWS Button does not change lateral references for Heading Select, Navigation, Backcourse, or Approach
modes. The autopilot guides the aircraft back to the Selected Heading/Course upon release of the CWS
Button.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
393
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
ROLL HOLD MODE (ROL)
NOTE: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls the wings
FLIGHT
INSTRUMENTS
level.
EIS
Figure 7-20 Roll Hold Mode Annunciation
AUDIO PANEL
& CNS
Bank Angle
Flight Director Response
< 6°
Rolls wings level
6° to 22° Maintains current aircraft roll attitude
> 22°
Limits bank to 22°
FLIGHT
MANAGEMENT
When the flight director is activated, Roll Hold Mode is selected by default. This mode is annunciated as
‘ROL’ in the AFCS Status Box. The current aircraft bank angle is held, subject to the bank angle conditions listed
in Table 7-4.
Table 7-4 Roll Hold Mode Responses
CHANGING THE ROLL REFERENCE
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
The roll reference can be changed by pressing the CWS Button, establishing the desired bank angle, then
releasing the CWS Button.
394
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
HEADING SELECT MODE (HDG)
FLIGHT
INSTRUMENTS
Heading Select Mode is activated by pressing the HDG Key. Heading Select Mode acquires and maintains
the Selected Heading. The Selected Heading is shown by a light blue bug on the HSI and in the box to the
upper left of the HSI.
CHANGING THE SELECTED HEADING
NOTE: Pressing the HDG Knob synchronize the Selected Heading to the current heading.
EIS
The Selected Heading is adjusted using the HDG Knob. Pressing the CWS Button and hand-flying the
aircraft does not change the Selected Heading. The autopilot guides the aircraft back to the Selected Heading
upon release of the CWS Button.
Heading Select
Mode Active
AUDIO PANEL
& CNS
Turns are commanded in the same direction as Selected Heading Bug movement, even if the Bug is turned
more than 180° from the present heading (e.g., a 270° turn to the right). However, Selected Heading changes
of more than 340° at a time result in turn reversals.
Pitch Mode
Active
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
Selected
Heading
Bug
ADDITIONAL
FEATURES
Selected
Heading
Command Bars Track
Selected Heading
APPENDICES
Figure 7-21 Heading Select Mode
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
395
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
NAVIGATION MODES (GPS, VOR, LOC,)
NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the
FLIGHT
INSTRUMENTS
flight director to enter Navigation Mode.
NOTE: When intercepting a flight plan leg, the flight director gives commands to capture the active leg at
approximately a 45° angle to the track between the waypoints defining the active leg. The flight director
does not give commands fly to the starting waypoint of the active leg.
AUDIO PANEL
& CNS
EIS
Pressing the NAV Key selects Navigation Mode. Navigation Mode acquires and tracks the selected navigation
source (GPS, VOR, LOC). The flight director follows GPS roll steering commands when GPS is the selected
navigation source. When the navigation source is VOR or LOC, the flight director creates roll steering commands
from the Selected Course and deviation. Navigation Mode can also be used to fly non-precision GPS and LOC
approaches where glideslope capture is not required.
FLIGHT
MANAGEMENT
If the Course Deviation Indicator (CDI) shows greater than one dot when the NAV Key is pressed, the selected
mode is armed. If the CDI is less than one dot, Navigation Mode is automatically captured when the NAV Key
is pressed. The armed annunciation appears in white to the left of the active roll mode.
Figure 7-22 GPS Navigation Mode Armed
HAZARD
AVOIDANCE
When the CDI has automatically switched from GPS to LOC during a LOC/ILS approach, GPS Navigation
Mode remains active, providing GPS steering guidance until the localizer signal is captured. LOC Navigation
Mode is armed when the automatic navigation source switch takes place. If the APR Key is pressed prior to the
automatic navigation source switch, LOC Navigation Mode is armed.
AFCS
LOC Navigation Mode automatically reverts to Backcourse Mode if the localizer front course is greater
than 105° from the aircraft heading. Refer to the discussion (in this section) on Backcourse Mode for more
information on this topic.
If Navigation Mode is active and either of the following occur, the flight director reverts to Roll Hold Mode
(wings rolled level):
ADDITIONAL
FEATURES
• Different VOR tuned while in VOR Navigation Mode (VOR Navigation Mode reverts to armed)
• Navigation source manually switched (with the CDI Softkey)
INDEX
APPENDICES
• During a LOC/ILS approach, the FAF is crossed while in GPS Navigation Mode after the automatic navigation
source switch from GPS to LOC
396
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
CHANGING THE SELECTED COURSE
GPS Navigation
Mode Active
Pitch Mode
Active
FLIGHT
INSTRUMENTS
The Selected Course is controlled using the CRS Knob (while in VOR, LOC, or OBS Mode). Pressing the
CWS Button and hand-flying the aircraft does not change the Selected Course while in Navigation Mode. The autopilot guides the aircraft back to the Selected Course (or GPS flight plan) when the CWS Button is
released.
Selected Altitude
Capture Mode
Armed
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Selected
Course
Command Bars Indicate Left
Turn to Track GPS Course and Climb
to Intercept Selected Altitude
HAZARD
AVOIDANCE
GPS is Selected
Navigation
Source
Figure 7-23 Navigation Mode
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
397
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
APPROACH MODES (GPS, VAPP, LOC)
NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the
FLIGHT
INSTRUMENTS
flight director to enter Approach Mode.
EIS
Approach Mode is activated when the APR Key is pressed. Approach Mode acquires and tracks the
selected navigation source (GPS, VOR, or LOC), depending on loaded approach. This mode uses the selected
navigation receiver deviation and desired course inputs to fly the approach. Pressing the APR Key when
the CDI is greater than one dot arms the selected approach mode (annunciated in white to the left of the
active lateral mode). If the CDI is less than one dot, the LOC is automatically captured when the APR Key
is pressed.
VOR Approach Mode (VAPP) provides greater sensitivity for signal tracking than VOR Navigation Mode .
AUDIO PANEL
& CNS
Selecting VOR Approach Mode:
1) Ensure a valid VOR frequency is tuned.
2) Ensure that VOR is the selected navigation source (use the CDI Softkey to cycle through navigation sources if
necessary).
FLIGHT
MANAGEMENT
3) Press the APR Key.
When GPS Approach Mode is armed, Glidepath Mode is also armed.
Selecting GPS Approach Mode:
HAZARD
AVOIDANCE
1) Ensure a GPS approach is loaded into the active flight plan. The active waypoint must be part of the flight plan
(cannot be a direct-to a waypoint not in the flight plan).
2) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if
necessary).
AFCS
3) Press the APR Key.
INDEX
APPENDICES
ADDITIONAL
FEATURES
Figure 7-24 Navigation/Approach Mode Armed
398
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
LOC Approach Mode allows the autopilot to fly a LOC/ILS approach with a glideslope. When LOC Approach
Mode is armed, Glideslope Mode is also armed automatically. LOC captures are inhibited if the difference
between aircraft heading and localizer course exceeds 105°.
FLIGHT
INSTRUMENTS
Selecting LOC Approach Mode:
1) Ensure a valid localizer frequency is tuned.
2) Ensure that LOC is the selected navigation source (use the CDI Softkey to cycle through navigation sources if
necessary).
3) Press the APR Key.
EIS
Or:
1) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if
necessary).
AUDIO PANEL
& CNS
2) Ensure a LOC/ILS approach is loaded into the active flight plan.
3) Ensure the corresponding LOC frequency is tuned.
4) Press the APR Key.
FLIGHT
MANAGEMENT
If the following occurs, the flight director reverts to Roll Hold Mode (wings rolled level):
• Approach Mode is active and a Vectors-To-Final is activated
• Approach Mode is active and Navigation source is manually switched
HAZARD
AVOIDANCE
• During a LOC/ILS approach, GPS Navigation Mode is active and the FAF is crossed after the automatic
navigation source switch from GPS to LOC
CHANGING THE SELECTED COURSE
AFCS
The Selected Course is controlled using the CRS Knob (while in VOR, LOC, or OBS Mode). Pressing the
CWS Button and hand-flying the aircraft does not change the Selected Course while in Approach Mode. The autopilot guides the aircraft back to the Selected Course (or GPS flight plan) when the CWS Button is
released.
INTERCEPTING AND FLYING A DME ARC
ADDITIONAL
FEATURES
APPENDICES
The AFCS will intercept and track a DME arc that is part of the active flight plan provided that GPS
Navigation Mode is engaged, GPS is the active navigation source on the CDI, and the DME arc segment is
the active flight plan leg. It is important to note that automatic navigation of DME arcs is based on GPS. Thus, even if the APR key is pressed and LOC or VOR Approach Mode is armed prior to reaching the Initial
Approach Fix (IAF), Approach Mode will not activate until the arc segment is completed.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
If the pilot decides to intercept the arc at a location other than the published IAF (i.e. ATC provides vectors
to intercept the arc) and subsequently selects Heading Mode or Roll Mode, the AFCS will not automatically
intercept or track the arc unless the pilot activates the arc leg of the flight plan and arms GPS Navigation
Mode. The AFCS will not intercept and fly a DME arc before reaching an IAF that defines the beginning of the
arc segment. Likewise, if at any point while established on the DME arc the pilot deselects GPS Navigation
Mode, the AFCS will no longer track the arc.
399
SYSTEM
OVERVIEW
BACKCOURSE MODE (BC)
FLIGHT
INSTRUMENTS
Backcourse Mode captures and tracks a localizer signal in the backcourse direction. The mode may be
selected by pressing the BC Key (GDU 1044B only). Backcourse Mode is armed if the CDI is greater than one
dot when the mode is selected. If the CDI is less than one dot, the Backcourse Mode is automatically captured
when the BC Key is pressed. The flight director creates roll steering commands from the Selected Course and
deviation when in Backcourse Mode. The annunciation ‘BC’ in the AFCS Status Box indicates Backcourse Mode
(Figure 7-26).
EIS
AUTOMATIC FLIGHT CONTROL SYSTEM
LOC Navigation Mode automatically (i.e., without pressing the BC key) reverts to Backcourse Mode if the
localizer front course is greater than 105° from the aircraft heading. Refer to the previous discussion (in this
section) on Navigation Modes for more information on LOC Navigation Mode.
AUDIO PANEL
& CNS
NOTE: When making a backcourse approach, set the Selected Course to the localizer front course.
Pitch Hold
Mode Active
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Backcourse
Mode Active
ADDITIONAL
FEATURES
LOC2 is Selected Navigation Source
Command Bars Hold Pitch Attitude
Figure 7-25 Backcourse Mode
APPENDICES
CHANGING THE SELECTED COURSE
INDEX
The Selected Course is controlled using the CRS Knob. Pressing the CWS Button and hand-flying the
aircraft does not reset any reference data while in Backcourse Mode. The autopilot guides the aircraft back to
the Selected Course when the CWS Button is released.
400
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
7.5 AUTOPILOT OPERATION
NOTE: Refer to the AFM for specific instructions regarding emergency procedures.
FLIGHT
INSTRUMENTS
The autopilot operates flight control surface servos to provide automatic flight control. Pitch and roll commands
are provided to the servos, based on the active flight director modes. The autopilot uses pitch and roll rates to
stabilize the aircraft attitude during upsets and flight director maneuvers. Flight director commands are rate- and
attitude-limited, combined with pitch and roll damper control, and sent to the pitch and roll servo motors.
EIS
Pitch autotrim provides trim commands to the pitch trim servo to relieve any sustained effort required by the
pitch servo. The pitch servo measures the output effort (torque) and provides this signal to the pitch trim servo.
The pitch trim servo commands the motor to reduce the average pitch servo effort.
AUDIO PANEL
& CNS
When the autopilot is not engaged, the pitch trim servo may be used to provide manual electric trim (MET). This allows the aircraft to be trimmed using a control wheel switch rather than the trim wheel. Manual trim
commands are generated with the MET Switch. Trim speeds are scheduled with airspeed to provide more
consistent response.
FLIGHT
MANAGEMENT
Servo motor control limits the maximum servo speed and torque. The servo mounts are equipped with slipclutches set to certain values. This allows the servos to be overridden in case of an emergency.
ENGAGING THE AUTOPILOT
NOTE: Autopilot engagement/disengagement is not equivalent to servo engagement/disengagement. Use
HAZARD
AVOIDANCE
the CWS Button to disengage the pitch and roll servos while the autopilot remains active.
When the AP Key is pressed, the autopilot and flight director (if not already engaged) are activated. Engagement
is indicated by a green ‘AP’ annunciation in the center of the AFCS Status Box. The flight director engages in
Pitch and Roll Hold modes when initially activated.
AFCS
Autopilot
Engaged
ADDITIONAL
FEATURES
Figure 7-26 Autopilot and Yaw Damper Engaged
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
401
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
CONTROL WHEEL STEERING
FLIGHT
INSTRUMENTS
During autopilot operation, the aircraft may be hand-flown without disengaging the autopilot. Pressing and
holding the CWS Button disengages the pitch and roll servos from the flight control surfaces and allows the
aircraft to be hand-flown. At the same time, the flight director is synchronized to the aircraft attitude during
the maneuver. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white for the duration of CWS
maneuvers.
In most scenarios, releasing the CWS Button reengages the autopilot with a new reference. Refer to the flight
director modes section for CWS behavior in each mode.
EIS
Control Wheel Steering
AUDIO PANEL
& CNS
Figure 7-27 CWS Annunciation
DISENGAGING THE AUTOPILOT
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
The autopilot is manually disengaged by pushing the AP DISC Switch, GA Switch or the AP Key on the
MFD. Manual disengagement is indicated by a five-second flashing yellow ‘AP’ annunciation and a twosecond autopilot disconnect aural alert. After manual disengagement, the autopilot disconnect aural alert
may be cancelled by pushing the AP DISC or MET Switch (AP DISC Switch also cancels the flashing ‘AP’
annunciation).
Figure 7-28 Manual Autopilot Disengagement
AFCS
Automatic autopilot disengagement is indicated by a flashing red ‘AP’ annunciation and by the autopilot
disconnect aural alert, which continue until acknowledged by pushing the AP DISC or MET Switch.
Automatic disengagement occurs due to:
• System failure
• Inability to compute default flight director modes (FD also disengages automatically)
ADDITIONAL
FEATURES
• Invalid sensor data
INDEX
APPENDICES
Figure 7-29 Automatic Autopilot Disengagement
402
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
7.6 EXAMPLE PROCEDURES
FLIGHT
INSTRUMENTS
NOTE: The following example flight plan and diagrams (not to be used for navigation) in this section are
for instructional purposes only and should be considered not current. Numbered portions of accompanying
diagrams correspond to numbered procedure steps.
EIS
This section provides a scenario-based set of procedures showing various GFC 700 AFCS modes used during a
flight. In this scenario, the aircraft departs Charles B. Wheeler Downtown Airport (KMKC), enroute to Colorado
Springs Airport (KCOS). After departure, the aircraft climbs to 12,000 ft and airway V4 is intercepted, following
ATC vectors.
0
33
30
3
27
30
27
24
24
21
30
24
27
15
27
HAZARD
AVOIDANCE
12
21
18
15
18
9
24
21
12
6
Lamar
VOR
(LAA)
Topeka
VOR
(TOP)
12
Hays
VOR
(HYS)
9
V 244
Salina
VOR
(SLN)
9
3
V4
18
V 244
9
6
0
33
15
6
KCOS
KMKC
30
6
3
3
FLIGHT
MANAGEMENT
33
0
33
0
AUDIO PANEL
& CNS
Airway V4 is flown to Salina VOR (SLN) using VOR navigation, then airway V244 is flown using GPS Navigation. The ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach
is executed.
12
21
15
18
Figure 7-30 Flight Plan Overview
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
403
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
DEPARTURE
Climbing to the Selected Altitude and flying an assigned heading:
FLIGHT
INSTRUMENTS
1) Before takeoff, set the Selected Altitude to 12,000 feet using the ALT Knob.
2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or
Flight Level Change Mode may be used).
EIS
a) Press the VS Key to activate Vertical Speed Mode.
AUDIO PANEL
& CNS
The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP/
NOSE DN Keys or pushing the CWS Button while hand-flying the aircraft to establish a new Vertical Speed
Reference.
FLIGHT
MANAGEMENT
b) Press the AP Key to engage the autopilot in a climb using Vertical Speed Mode.
3) Use the HDG Knob to set the Selected Heading, complying with ATC vectors to intercept Airway V4.
HAZARD
AVOIDANCE
Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb. The autopilot
follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading.
AFCS
4) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode,
indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.
At 50 feet from the Selected Altitude, the green ‘ALT’ annunciation flashes for up to 10 seconds; the autopilot
transitions to Altitude Hold Mode and levels the aircraft.
INDEX
APPENDICES
ADDITIONAL
FEATURES
404
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
HD
GM
od
e
EIS
3
AUDIO PANEL
& CNS
Selected Altitude of 12,000 MSL
ALT Mode
4
1
2
VS
FLIGHT
MANAGEMENT
KMKC
e
Mod
Figure 7-31 Departure
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
405
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
INTERCEPTING A VOR RADIAL
FLIGHT
INSTRUMENTS
During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina
VOR (SLN) should now be intercepted. Since the enroute flight plan waypoints correspond to VORs, flight
director Navigation Mode using either VOR or GPS as the navigation source may be used. In this scenario, VOR
Navigation Mode is used for navigation to the first VOR waypoint in the flight plan.
Intercepting a VOR radial:
1) Arm VOR Navigation Mode:
EIS
a) Tune the VOR frequency.
b) Press the CDI Softkey to set the navigation source to VOR.
AUDIO PANEL
& CNS
c) Use the CRS Knob to set the Selected Course to 255°. Note that at this point, the flight director is still in
Heading Select Mode and the autopilot continues to fly 290°.
FLIGHT
MANAGEMENT
d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of
the active lateral mode.
HAZARD
AVOIDANCE
2) As the aircraft nears the Selected Course, the flight director transitions from Heading Select to VOR Navigation
Mode and the ‘VOR’ annunciation flashes green. The autopilot begins turning to intercept the Selected
Course.
3) The autopilot continues the turn until the aircraft is established on the Selected Course.
0
3
Hd
29 g
0o
30
AFCS
33
V4
6
27
3
Salina
VOR
(SLN)
24
ADDITIONAL
FEATURES
9
o
255
NA
V
Mo
de
2
HD
G
12
M
od
e,
VO
R
Ar
m
15
21
18
APPENDICES
VO
R
ed
1
INDEX
Figure 7-32 Intercepting a VOR Radial
406
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
FLYING A FLIGHT PLAN/GPS COURSE
NOTE: Changing the navigation source cancels Navigation Mode and causes the flight director to revert
FLIGHT
INSTRUMENTS
back to Roll Hold Mode (wings rolled level).
As the aircraft closes on Salina VOR, GPS is used to navigate the next leg, airway V244. The aircraft is
currently tracking inbound on Airway V4.
Flying a GPS flight plan:
EIS
1) Transition from VOR to GPS Navigation Mode:
a) Press the CDI Softkey until GPS is the selected navigation source.
AUDIO PANEL
& CNS
b) Press the NAV Key to activate GPS Navigation Mode. The autopilot guides the aircraft along the active flight
plan leg.
2) Following the flight plan, the autopilot continues to steer the aircraft under GPS guidance.
33
3
30
0
V4
6
3
FLIGHT
MANAGEMENT
0
33
e
1
d
AV Mo
VOR N
o
075
30
e
V Mod
PS NA
6
27
G
24
27
12
21
18
12
15
24
9
Hays
VOR
(HYS)
Salina
VOR
(SLN)
V 244
HAZARD
AVOIDANCE
o
076
2
9
o
260
15
AFCS
21
18
Figure 7-33 Transition to GPS Flight Plan
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
407
SYSTEM
OVERVIEW
DESCENT
FLIGHT
INSTRUMENTS
AUTOMATIC FLIGHT CONTROL SYSTEM
• Flight Level Change descent – Flight Level Change Mode can be used to descend to the Selected Altitude at a
constant airspeed. This descent method does not account for flight plan waypoint altitude constraints.
While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS. Three methods are presented for descent:
• Vertical Path Tracking descent – Vertical Path Tracking Mode is used to follow the vertical descent path
defined in the GPS flight plan. Altitude constraints correspond to waypoints in the flight plan. Before VNV
flight control can provide vertical profile guidance, a VNV flight plan must be entered and enabled.
EIS
• Non-path descent in a VNV scenario – A VNV flight plan is entered and enabled, however Pitch Hold, Vertical
Speed, or Flight Level Change Mode can be used to descend to the VNV Target Altitude prior to reaching the
planned TOD. Flight Level Change Mode is used in the example.
AUDIO PANEL
& CNS
Flight Level Change descent:
1) Select Flight Level Change Mode:
a) Using the ALT Knob, set the Selected Altitude to 10,000 feet.
FLIGHT
MANAGEMENT
b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the
Airspeed Reference, which defaults to the current aircraft airspeed. Selected Altitude Capture Mode is armed
automatically.
HAZARD
AVOIDANCE
2) Use the NOSE UP/NOSE DN Keys or push the CWS Button while hand-flying the aircraft to adjust the
commanded airspeed while maintaining the same power, or reduce power to allow descent in Flight Level
Change Mode while the autopilot maintains the current airspeed.
AFCS
3) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode,
indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.
ADDITIONAL
FEATURES
The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the
autopilot transitions to Altitude Hold Mode and levels the aircraft.
1
Cruise Altitude of 12,000 MSL
APPENDICES
ALT Mode
2
FLC
Mod
e
3
Selected Altitude of 10,000 MSL
ALT Mode
INDEX
Figure 7-34 FLC Descent
408
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
Vertical Path Tracking descent to VNV Target Altitude:
1) Select coupled VNV:
a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears.
FLIGHT
INSTRUMENTS
b) Using the ALT Knob, set the Selected Altitude 75 feet below the flight plan’s VNV Target Altitude of 10,000
feet.
EIS
If the Selected Altitude is not at least 75 feet below the VNV Target Altitude, the flight director captures the
Selected Altitude rather than the VNV Target Altitude once Vertical Path Tracking Mode becomes active (ALTS is
armed rather than ALTV).
•
Press the VNV Key
•
Turn the ALT Knob to adjust the Selected Altitude
AUDIO PANEL
& CNS
c) If Vertical Path Tracking Mode is armed more than 5 minutes prior to descent path capture, acknowledgment is
required for the flight director to transition from Altitude Hold to Vertical Path Tracking Mode. To proceed with
descent path capture if the white ‘VPTH’ annunciation begins flashing, do one of the following
FLIGHT
MANAGEMENT
If the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the
descent is not captured.
2) When the top of descent (TOD) is reached, the flight director transitions to Vertical Path Tracking Mode and
begins the descent to the VNV Target Altitude. Intention to capture the VNV Target Altitude is indicated by the
white ‘ALTV’ annunciation.
HAZARD
AVOIDANCE
3) As the aircraft nears the VNV Target Altitude, the flight director transitions to VNV Target Altitude Capture Mode,
indicated by the green ‘ALTV’ annunciation flashing for up to 10 seconds.
AFCS
1
ALT Mode
TOD
ADDITIONAL
FEATURES
The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the VNV Target Altitude;
the autopilot transitions to Altitude Hold Mode and levels the aircraft at the vertical waypoint.
Cruise Altitude of 12,000 MSL
VPT
APPENDICES
2
HM
ode
3
VNAV Target Altitude of 10,000 MSL
BOD
ALT Mode
3 nm
INDEX
Selected Altitude (set below VNAV Target Altitude)
OPSHN
Figure 7-35 VPTH Descent
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
409
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
Non-path descent using Flight Level Change Mode:
1) Using Flight Level Change Mode, command a non-path descent to an intermediate altitude above the next VNV
flight plan altitude.:
FLIGHT
INSTRUMENTS
a) Using the ALT Knob, set the Selected Altitude below the current aircraft altitude to an altitude (in this case,
9,400 feet) at which to level off between VNV flight plan altitudes.
EIS
b) Press the FLC Key before the planned TOD during an altitude hold while VPTH is armed. The Airspeed Reference
defaults to the current aircraft airspeed. Vertical Path Tracking and Selected Altitude Capture Mode are armed
automatically.
AUDIO PANEL
& CNS
HAZARD
AVOIDANCE
3) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode,
indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.
FLIGHT
MANAGEMENT
2) Reduce power to allow descent in Flight Level Change Mode. The autopilot maintains the Airspeed Reference.
The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the
autopilot transitions to Altitude Hold Mode and levels the aircraft. After leveling off, reset selected altitude at
or below 9,000 ft.
AFCS
4) When the next TOD is reached, Vertical Path Tracking becomes active (may require acknowledgment to allow
descent path capture).
ADDITIONAL
FEATURES
5) As the aircraft nears the VNV Target Altitude, the flight director transitions to VNV Target Altitude Capture Mode,
indicated by the green ‘ALTV’ annunciation flashing for up to 10 seconds.
The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the VNV Target Altitude;
the autopilot transitions to Altitude Hold Mode and levels the aircraft at the vertical waypoint.
INDEX
APPENDICES
410
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
VP
TH
M
od
e
ALT Mode
1
FL
C
Selected Altitude of 9,400 MSL
VNAV Target Altitude of 10,000 MSL
Pla
nn
M
od
e
AUDIO PANEL
& CNS
Planned
TOD
2
BOD
3
ed
De
sce
nt
ALT Mode
Pa
th
TOD
VP
TH
FLIGHT
MANAGEMENT
4
Mo
de
VNAV Target Altitude of 9,000 MSL
5
BOD
ALT Mode
Selected Altitude
OPSHN
HABUK
HAZARD
AVOIDANCE
3 nm
Figure 7-36 Non-path Descent
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
411
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
APPROACH
Flying an ILS approach:
FLIGHT
INSTRUMENTS
1) Transition from GPS Navigation Mode to Heading Select Mode.
a) Select the Runway 35L ILS approach for KCOS and select ‘VECTORS’ for the transition. Load and activate the
approach into the flight plan.
b) Use the HDG Knob to set the Selected Heading after getting vectors from ATC.
c) Press the HDG Key. The autopilot turns the aircraft to the desired heading.
EIS
d) Use Heading Select Mode to comply with ATC vectors as requested.
AUDIO PANEL
& CNS
2) Arm LOC Approach and Glideslope modes.
a) Ensure the appropriate localizer frequency is tuned.
FLIGHT
MANAGEMENT
b) Press the APR Key when cleared for approach to arm Approach and Glideslope modes. ‘LOC’ and ‘GS’ appear
in white as armed mode annunciations.
c) The navigation source automatically switches to LOC. After this switch occurs, the localizer signal can be captured
and the flight director determine when to begin the turn to intercept the final approach course. The flight director
now provides guidance to the missed approach point.
HAZARD
AVOIDANCE
3) There are two options available at this point, as the autopilot flies the ILS approach:
• Push the AP DISC Switch at the decision height and land the aircraft.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
• Use the GA Switch to execute a missed approach.
412
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
KCOS
FLIGHT
INSTRUMENTS
LOC APR/
GS Mode
3
PETEY
2
HD
G
od
M
e
PYNON
1
EIS
AUDIO PANEL
& CNS
GPS NAV Mode
FLIGHT
MANAGEMENT
Figure 7-37 ILS Approach to KCOS
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
413
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE: Support for SBAS precision approaches is available only in installations with GIA 63W IAUs when
SBAS is available.
FLIGHT
INSTRUMENTS
Flying a RNAV GPS approach with vertical guidance:
1) Arm flight director modes for a RNAV GPS approach with vertical guidance:
a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source).
b) Select the Runway 35R LPV approach for KCOS. Load and activate the approach into the flight plan.
EIS
2) Press the APR Key once clearance for approach has been received. GPS Approach Mode is activated and
Glidepath Mode is armed.
AUDIO PANEL
& CNS
3) Once the glidepath is captured, Glidepath Mode becomes active. The flight director now provides guidance to
the missed approach point.
FLIGHT
MANAGEMENT
4) There are two options available at this point, as the autopilot flies the approach:
• Push the AP DISC Switch at the Decision height and land the aircraft.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
• Use the GA Switch to execute a missed approach.
414
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
KCOS
4
FLIGHT
INSTRUMENTS
3
GPS APR/
GP Mode
CEGIX
EIS
2
FALUR
HABUK
AUDIO PANEL
& CNS
PYNON
1
FLIGHT
MANAGEMENT
GPS NAV Mode
HAZARD
AVOIDANCE
Figure 7-38 LPV Approach to KCOS
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
415
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
GO AROUND/MISSED APPROACH
NOTE: As a result of calculations performed by the system while flying the holding pattern, the display may
FLIGHT
INSTRUMENTS
re-size automatically and the aircraft may not precisely track the holding pattern as depicted on the PFD and
MFD.
Flying a missed approach:
EIS
1) Push the GA Switch at the Decision height and apply go-around power to execute a missed approach. The
flight director Command Bars establish a nose-up climb to follow. If flying an ILS or LOC approach the CDI also
switches to GPS as the navigation source.
Note that when the GA Switch is pushed, the missed approach is activated and the autopilot disconnects,
indicated by the ‘AP’ annunciation flashing yellow for 5 seconds and the autopilot disconnect aural alert.
AUDIO PANEL
& CNS
Flashes 5 sec
2) Start the climb to the prescribed altitude in the published Missed Approach Procedure (in this case, 10,000 ft).
FLIGHT
MANAGEMENT
a) Press the AP Key to re-engage the autopilot.
HAZARD
AVOIDANCE
b) Press the NAV Key to have the autopilot fly to the hold.
3) Use the ALT Knob to set a Selected Altitude to hold.
To hold the current airspeed during the climb, press the FLC Key.
ADDITIONAL
FEATURES
AFCS
As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode,
indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds.
APPENDICES
The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the
autopilot transitions to Altitude Hold Mode and levels the aircraft.
INDEX
4) The autopilot flies the holding pattern after the missed approach is activated. Annunciations are displayed in
the Navigation Status Box, above the AFCS Status Box.
416
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
4
AUDIO PANEL
& CNS
MOGAL
FLIGHT
MANAGEMENT
GPS NAV Mode
3
GA Mode
KCOS
HAZARD
AVOIDANCE
2
1
AFCS
Figure 7-39 Go Around/Missed Approach
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
417
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
7.7 AFCS ANNUNCIATIONS AND ALERTS
FLIGHT
INSTRUMENTS
AFCS STATUS ALERTS
The annunciations in Table 7-5 (listed in order of increasing priority) can appear on the PFD above the
Airspeed and Attitude indicators. Only one annunciation occurs at a time, and messages are prioritized by
criticality.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
AFCS Status
Annunciation
Figure 7-40 AFCS Status Annunciation
HAZARD
AVOIDANCE
Alert Condition
Aileron Mistrim Right
Aileron Mistrim Left
Elevator Mistrim Down
AFCS
Elevator Mistrim Up
ADDITIONAL
FEATURES
Pitch Trim Failure
Description
Roll servo providing sustained force in the indicated direction
Pitch servo providing sustained force in the indicated direction
If AP engaged, take control of the aircraft and disengage AP
Roll Failure
Roll axis control failure; AP inoperative
Pitch Failure
Pitch axis control failure; AP inoperative
System Failure
APPENDICES
Annunciation
Preflight Test
AP and MET are unavailable; FD may still be available
Performing preflight system test; aural alert sounds at completion
Do not press the AP DISC Switch during servo power-up and preflight system tests
as this may cause the preflight system test to fail or never to start (if servos fail
their power-up tests). Power must be cycled to the servos to remedy the situation.
INDEX
Preflight system test failed; aural alert sounds at failure
Table 7-5 AFCS Status Alerts
418
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM
SYSTEM
OVERVIEW
OVERSPEED PROTECTION
NOTE: Overspeed protection is not active in Altitude Hold, Glideslope or Glidepath modes.
FLIGHT
INSTRUMENTS
While Pitch Hold, Vertical Speed, Flight Level Change, Vertical Path Tracking, or an altitude capture mode is
active, airspeed is monitored by the flight director. Pitch commands are not changed until overspeed protection
becomes active. Overspeed protection is provided in situations where the flight director cannot acquire and
maintain the mode reference for the selected vertical mode without exceeding the certified maximum autopilot
airspeed.
EIS
When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box above the Airspeed
Indicator, flashing a yellow ‘MAXSPD’ annunciation. Engine power should be reduced and/or the pitch reference
adjusted to slow the aircraft. The annunciation disappears when the overspeed condition is resolved.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Airspeed
Indicator
HAZARD
AVOIDANCE
Figure 7-41 Overspeed Annunciation
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
419
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
AUTOMATIC FLIGHT CONTROL SYSTEM
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Blank Page
420
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
SECTION 8 ADDITIONAL FEATURES
FLIGHT
INSTRUMENTS
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may be necessary to carry another
source of charts on-board the aircraft.
Additional features of the G1000 include the following:
• Synthetic Vision System (SVS)(Optional)
• SafeTaxi® diagrams
EIS
• ChartView and FliteCharts® electronic charts (Optional)
• AOPA or AC-U-KWIK Airport Directory
AUDIO PANEL
& CNS
• SiriusXM Satellite Radio entertainment (Optional)
• Scheduler
• Electronic Checklists (Optional)
FLIGHT
MANAGEMENT
• Flight Data Logging
• Auxiliary Video (Optional)
HAZARD
AVOIDANCE
The optional Synthetic Vision System (SVS) provides a three-dimensional forward view of terrain features on
the PFD. SVS imagery shows the pilot’s view of relevant features in relation to the aircraft attitude, as well as the
flight path pertaining to the active flight plan.
SafeTaxi diagrams provide detailed taxiway, runway, and ramp information at more than 700 airports in the
United States. By decreasing range on an airport that has a SafeTaxi diagram available, a close up view of the
airport layout can be seen.
AFCS
The optional ChartView and FliteCharts provide on-board electronic terminal procedures charts. Electronic
charts offer the convenience of rapid access to essential information. Either ChartView or FliteCharts may be
configured in the system, but not both.
The AOPA and AC-U-KWIK Airport Directories offer detailed information for a selected airport, such as available
services, hours of operation, and lodging options.
ADDITIONAL
FEATURES
The optional SiriusXM Satellite Radio entertainment audio feature of the GDL 69A Data Link Receiver handles
more than 170 channels of music, news, and sports. SiriusXM Satellite Radio offers more entertainment choices
and longer range coverage than commercial broadcast stations.
APPENDICES
The Scheduler feature can be used to enter and display short term or long term reminder messages such as
Switch fuel tanks, Change oil, or Altimeter-Transponder Check in the Messages Window on the PFD.
Optional checklists help to quickly find the proper procedure on the ground or during flight.
The Flight Data Logging feature automatically stores critical flight and engine data on an SD data card.
Approximately 1,000 flight hours can be recorded for each 1GB of available space on the card.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
The G1000 system provides a control and display interface to an optional auxiliary video system. The system
can display video for up to two inputs.
421
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
8.1 SYNTHETIC VISION SYSTEM (SVS) (OPTIONAL)
FLIGHT
INSTRUMENTS
WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance.
SVS is intended as an aid to situational awareness only and may not provide either the accuracy or reliability
upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic.
AUDIO PANEL
& CNS
EIS
The optional Synthetic Vision System (SVS) is a visual enhancement to the G1000 Integrated Flight Deck. SVS
depicts a forward-looking attitude display of the topography immediately in front of the aircraft. The field of
view is 30 degrees to the left and 35 degrees to the right. SVS information is shown on the Primary Flight Display
(PFD), or on the Multifunction Display (MFD) in Reversionary Mode (Figure 8‑90). The depicted imagery is
derived from the aircraft attitude, heading, GPS three-dimensional position, and a nine arc-second database of
terrain, obstacles, and other relevant features. The terrain data resolution of nine arc-seconds, meaning that
the terrain elevation contours are stored in squares measuring nine arc-seconds on each side, is required for the
operation of SVS. Loss of any of the required data, including temporary loss of the GPS signal, will cause SVS to
be disabled until the required data is restored.
FLIGHT
MANAGEMENT
The SVS terrain display shows land contours (colors are consistent with those of the topographical map display),
large water features, towers, and other obstacles over 200’ AGL that are included in the obstacle database. Cultural
features on the ground such as roads, highways, railroad tracks, cities, and state boundaries are not displayed
even if those features are found on the MFD map. The terrain display also includes a north–south east–west grid
with lines oriented with true north and spaced at one arc-minute intervals to assist in orientation relative to the
terrain.
HAZARD
AVOIDANCE
The optional Terrain Awareness and Warning System (TAWS) or standard Terrain-SVS is integrated within
SVS to provide visual and auditory alerts to indicate the presence of terrain and obstacle threats relevant to the
projected flight path. Terrain alerts are displayed in red and yellow shading on the PFD.
AFCS
The terrain display is intended for situational awareness only. It may not provide the accuracy or fidelity on
which to base decisions and plan maneuvers to avoid terrain or obstacles. Navigation must not be predicated
solely upon the use of the Terrain–SVS or TAWS terrain or obstacle data displayed by the SVS.
• Pathways
• Airport Signs
• Flight Path Marker
• Runway Display
• Horizon Heading Marks
• Terrain Alerting
• Traffic Display
• Obstacle Alerting
INDEX
APPENDICES
ADDITIONAL
FEATURES
The following SVS enhancements appear on the PFD:
422
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 8-1 Synthetic Vision Imagery
SVS OPERATION
HAZARD
AVOIDANCE
SVS is activated from the PFD using the softkeys located along the bottom edge of the display. Selecting the
softkeys turns the related function on or off. When SVS is enabled, the pitch scale increments are reduced to
10 degrees up and 7.5 degrees down.
AFCS
SVS functions are displayed on three levels of softkeys. The PFD Softkey leads into the PFD function Softkeys,
including synthetic vision. Selecting the SYN VIS Softkey displays the SVS feature softkeys. The softkeys are
labeled PATHWAY, SYN TERR, HRZN HDG, and APTSIGNS. The BACK Softkey returns to the previous
level of softkeys. Synthetic Terrain must be active before any other SVS feature may be activated.
ADDITIONAL
FEATURES
HRZN HDG, APTSIGNS, and PATHWAY Softkeys are only available when the SYN TERR Softkey is
activated (gray with black characters). After activating the SYN TERR Softkey, the HRZN HDG, APTSIGNS,
and PATHWAY softkeys may be activated in any combination to display desired features. When system power
is cycled, the last selected state (on or off) of the SYN TERR, HRZN HDG, APTSIGNS, and PATHWAY
softkeys is remembered by the system.
APPENDICES
• PATHWAY Softkey enables display of rectangular boxes that represent course guidance.
• SYN TERR Softkey enables synthetic terrain depiction.
• HRZN HDG Softkey enables horizon heading marks and digits.
• APTSIGNS Softkey enables airport signposts.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
423
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLIGHT
INSTRUMENTS
PFD
SYN VIS
BACK
Pressing the BACK Softkey
returns to the top-level softkeys.
BACK
EIS
PATHWAY SYN TERR HRZN HDG APTSIGNS
AUDIO PANEL
& CNS
Pressing the BACK Softkey returns to the previous level of softkeys.
Figure 8-2 SVS Softkeys
Activating and deactivating SVS:
FLIGHT
MANAGEMENT
1) Select the PFD Softkey.
2) Select the SYN VIS Softkey.
3) Select the SYN TERR Softkey. The SVS display will cycle on or off with the SYN TERR Softkey.
HAZARD
AVOIDANCE
Activating and deactivating Pathways:
1) Select the PFD Softkey.
2) Select the SYN VIS Softkey.
3) Select the PATHWAY Softkey. The Pathway feature will cycle on or off with the PATHWAY Softkey.
AFCS
Activating and deactivating Horizon Headings:
1) Select the PFD Softkey.
2) Select the SYN VIS Softkey.
ADDITIONAL
FEATURES
3) Select the HRZN HDG Softkey. The horizon heading display will cycle on or off with the HRZN HDG Softkey.
Activating and deactivating Airport Signs:
1) Select the PFD Softkey.
APPENDICES
2) Select the SYN VIS Softkey.
INDEX
3) Select the APTSIGNS Softkey. Display of airport signs will cycle on or off with the APTSIGNS Softkey.
424
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
SVS FEATURES
FLIGHT
INSTRUMENTS
Selected
Altitude
Airport
Runway
Pathways
Color
Matches CDI
Indicating
NAV Source
Flight
Path
Marker
Airplane
Symbol
EIS
Zero
Pitch Line
(ZPL) with
Compass
Heading
Marks
AUDIO PANEL
& CNS
Synthetic
Terrain
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
SVS
Softkeys
Figure 8-3 SVS on the Primary Flight Display
NOTE: Pathways and terrain features are not a substitute for standard course and altitude deviation
information provided by the altimeter, CDI, and VDI.
AFCS
PATHWAYS
ADDITIONAL
FEATURES
Pathways provide a three-dimensional perspective view of the selected route of flight shown as colored
rectangular boxes representing the horizontal and vertical flight path of the active flight plan. The box
size represents 700 feet wide by 200 feet tall during enroute, oceanic, and terminal flight phases. During
an approach, the box width is 700 feet or one half full scale deviation on the HSI, whichever is less. The
height is 200 feet or one half full scale deviation on the VDI, whichever is less. The altitude at which the
pathway boxes are displayed is determined by the higher of either the selected altitude or the VNAV altitude
programmed for the active leg in the flight plan (Figure 8-4).
APPENDICES
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
The color of the rectangular boxes may be magenta, green, or white depending on the route of flight and
navigation source selected. The active GPS or GPS overlay flight plan leg is represented by magenta boxes
that correspond to the Magenta CDI. A localizer course is represented by green boxes that correspond to a
green CDI. An inactive leg of an active flight plan is represented by white boxes corresponding to a white line
drawn on the Inset map or MFD map indicating an inactive leg.
425
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLIGHT
INSTRUMENTS
Selected
Altitude
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Programmed
Altitudes
HAZARD
AVOIDANCE
Figure 8-4 Programmed and Selected Altitude
AFCS
Pathways provide supplemental glidepath information on an active ILS, LPV, LNAV/VNAV, and some LNAV
approaches. Pathways are intended as an aid to situational awareness and should not be used independent
of the CDI, VDI, glide path indicator, and glide slope indicator. They are removed from the display when
the selected navigation information is not available. Pathways are not displayed beyond the active leg when
leg sequencing is suspended and are not displayed on any portion of the flight plan leg that would lead to
intercepting a leg in the wrong direction.
Departure and Enroute
APPENDICES
ADDITIONAL
FEATURES
Prior to intercepting an active flight plan leg, pathways are displayed as a series of boxes with pointers at
each corner that point in the direction of the active waypoint. Pathways are not displayed for the first leg
of the flight plan if that segment is a Heading-to-Altitude leg. The first segment displaying pathways is the
first active GPS leg or active leg with a GPS overlay. If this leg of the flight plan route is outside the SVS
field of view, pathways will not be visible until the aircraft has turned toward this leg. While approaching
the center of the active leg and prescribed altitude, the number of pathway boxes decreases to a minimum
of four.
INDEX
Pathways are displayed along the flight plan route at the highest of either the selected altitude or the
programmed altitude for the leg. Climb profiles cannot be displayed due to the variables associated with
aircraft performance. Flight plan legs requiring a climb are indicated by pathways displayed at a level above
the aircraft at the altitude selected or programmed.
426
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Descent and Approach
FLIGHT
INSTRUMENTS
Pathways are shown descending only for a programmed descent (Figures 8-5, 8-6). When the flight plan
includes programmed descent segments, pathways are displayed along the descent path provided that the
selected altitude is lower than the programmed altitude.
EIS
During a Vectors-to-Final (VTF) approach transition, pathways are displayed along the final approach
course inbound to the Missed Approach Point (MAP). Pathways are shown level at the selected altitude
or at the next programmed crossing altitude, whichever is higher, up to the point along the final approach
course where the altitude intercepts the extended vertical descent path, glidepath, or glideslope. From
the vertical path descent, glidepath, or glideslope intercept point, the pathways are shown inbound to the
Missed Approach Point (MAP) along the published lateral and vertical descent path. AUDIO PANEL
& CNS
During an ILS approach, the initial approach segment is displayed in magenta at the segment altitudes
if GPS is selected as the navigation source on the CDI. When switching to localizer inbound with LOC
selected as the navigation source on the CDI, pathways are displayed in green along the localizer and glide
slope.
FLIGHT
MANAGEMENT
VOR, LOC BC, and ADF approach segments that are approved to be flown using GPS are displayed in
magenta boxes. Segments that are flown using other than GPS or ILS, such as heading legs or VOR final
approach courses are not displayed.
Selected Altitude
set for Enroute
Selected Altitude
set for Departure
HAZARD
AVOIDANCE
Climbs NOT
displayed
by pathway
Non-programmed descents NOT displayed by pathway
TOD
AFCS
Selected Altitude
for Step Down
Programmed descent
displayed by pathway
ADDITIONAL
FEATURES
APPENDICES
Selected Altitude or Programmed Altitude
(whichever is higher)
Figure 8-5 SVS Pathways, Enroute and Descent
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
427
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
Missed Approach
FLIGHT
INSTRUMENTS
Upon activating the missed approach, pathways lead to the Missed Approach Holding Point (MAHP) and
are displayed as a level path at the published altitude for the MAHP, or the selected altitude, whichever is
the highest. If the initial missed approach leg is a Course-to-Altitude (CA) leg, the pathways boxes will
be displayed level at the altitude published for the MAHP. If the initial missed approach leg is defined by
a course using other than GPS, pathways are not displayed for that segment. In this case, the pathways
displayed for the next leg may be outside the field of view and will be visible when the aircraft has turned
in the direction of that leg.
AUDIO PANEL
& CNS
EIS
Pathways are displayed along each segment including the path required to track course reversals that are
part of a procedure, such as holding patterns. Pathways boxes will not indicate a turn to a MAHP unless a
defined geographical waypoint exists between the MAP and MAHP.
FAF
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Descent displayed
by pathway
Selected Altitude
or Programmed Altitude
(whichever is higher)
MAP Climbs NOT displayed
by pathway
Turn Segment
NOT displayed
by pathway
APPENDICES
ADDITIONAL
FEATURES
AFCS
MAHP
INDEX
Figure 8-6 SVS Pathways, Approach, Missed Approach, and Holding
428
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
FLIGHT PATH MARKER
FLIGHT
INSTRUMENTS
The Flight Path Marker (FPM), also known as a Velocity Vector, is displayed on the PFD at groundspeeds
above 30 knots. The FPM depicts the approximate projected path of the aircraft accounting for wind speed
and direction relative to the three-dimensional terrain display.
The FPM is always available when the Synthetic Terrain feature is in operation. The FPM represents the
direction of the flight path as it relates to the terrain and obstacles on the display, while the airplane symbol
represents the aircraft heading.
EIS
The FPM works in conjunction with the Pathways feature to assist the pilot in maintaining desired altitudes
and direction when navigating a flight plan. When on course and altitude the FPM is aligned inside the
pathway boxes as shown (Figure 8-7).
AUDIO PANEL
& CNS
The FPM may also be used to identify a possible conflict with the aircraft flight path and distant terrain or
obstacles. Displayed terrain or obstacles in the aircraft’s flight path extending above the FPM could indicate
a potential conflict, even before an alert is issued by TAWS. However, decisions regarding terrain and/or
obstacle avoidance should not be made using only the FPM.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Flight Path
Marker
(FPM)
AFCS
Wind
Vector
ADDITIONAL
FEATURES
APPENDICES
Figure 8-7 Flight Path Marker and Pathways
ZERO PITCH LINE
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
The Zero Pitch Line is drawn completely across the display and represents the horizon when the terrain
horizon is difficult to distinguish from other terrain being displayed. It may not align with the terrain
horizon, particularly when the terrain is mountainous or when the aircraft is flown at high altitudes.
429
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
HORIZON HEADING
FLIGHT
INSTRUMENTS
The Horizon Heading is synchronized with the HSI and shows approximately 60 degrees of compass
heading in 30‑degree increments on the Zero Pitch Line. Horizon Heading tick marks and digits appearing
on the zero pitch line are not visible behind either the airspeed or altitude display. Horizon Heading is used
for general heading awareness, and is activated and deactivated by selecting the HRZN HDG Softkey.
TRAFFIC
WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on the SVS display or may appear as a
EIS
partial symbol.
AUDIO PANEL
& CNS
Traffic symbols are displayed in their approximate locations as determined by the related traffic systems. Traffic symbols are displayed in three dimensions, appearing larger as they are getting closer, and smaller
when they are further away. Traffic within 250 feet laterally of the aircraft will not be displayed on the SVS
display. Traffic symbols and coloring are consistent with that used for traffic displayed in the Inset map or
MFD traffic page. If the traffic altitude is unknown, the traffic will not be displayed on the SVS display. For
more details refer to the traffic system discussion in the Hazard Avoidance section.
FLIGHT
MANAGEMENT
AIRPORT SIGNS
HAZARD
AVOIDANCE
Airport Signs provide a visual representation of airport location and identification on the synthetic terrain
display. When activated, the signs appear on the display when the aircraft is approximately 15 nm from
an airport and disappear at approximately 4.5 nm. Airport signs are shown without the identifier until
the aircraft is approximately eight nautical miles from the airport. Airport signs are not shown behind the
airspeed or altitude display. Airport signs are activated and deactivated by selecting the APTSIGNS Softkey.
ADDITIONAL
FEATURES
AFCS
Traffic
Airport
Sign
without
Identifier
(Between
8 nm and
15 nm)
INDEX
APPENDICES
Airport
Sign with
Identifier
(Between
4.5 nm and
8 nm)
Figure 8-8 Airport Signs
430
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
RUNWAYS
WARNING: Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft
FLIGHT
INSTRUMENTS
to the runway or for maintaining the proper approach path angle during landing.
NOTE: Not all airports have runways with endpoint data in the database, therefore, these runways are not
displayed.
EIS
Runway data provides improved awareness of runway location with respect to the surrounding terrain. All
runway thresholds are depicted at their respective elevations as defined in the database. In some situations, where threshold elevations differ significantly, crossing runways may appear to be layered. As runways are
displayed, those within 45 degrees of the aircraft heading are displayed in white. Other runways will be gray
in color. When an approach for a specific runway is active, that runway will appear brighter and be outlined
with a white box, regardless of the runway orientation as related to aircraft heading. As the aircraft gets closer
to the runway, more detail such as runway numbers and centerlines will be displayed.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Runway
Selected for
Approach
Other
Runway
on Airport
AFCS
ADDITIONAL
FEATURES
APPENDICES
Figure 8-9 Airport Runways
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
431
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
TERRAIN-SVS AND TAWS ALERTING
FLIGHT
INSTRUMENTS
Terrain alerting on the synthetic terrain display is triggered by Forward-looking Terrain Avoidance (FLTA)
alerts, and corresponds to the red and yellow X symbols on the Inset Map and MFD map displays. For more
detailed information regarding Terrain-SVS and TAWS, refer to the Hazard Avoidance Section.
EIS
In some instances, a terrain or obstacle alert may be issued with no conflict shading displayed on the
synthetic terrain. In these cases, the conflict is outside the SVS field of view to the left or right of the
aircraft.
AUDIO PANEL
& CNS
TERRAIN
Annunciation
FLIGHT
MANAGEMENT
Terrain
Caution
HAZARD
AVOIDANCE
Potential
Impact
Points
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 8-10 Terrain Alert
432
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
Obstacles are represented on the synthetic terrain display by standard two-dimensional tower symbols found
on the Inset map and MFD maps and charts. Obstacle symbols appear in the perspective view with relative
height above terrain and distance from the aircraft. Unlike the Inset map and MFD moving map display,
obstacles on the synthetic terrain display do not change colors to warn of potential conflict with the aircraft’s
flight path until the obstacle is associated with an actual FLTA alert. Obstacles greater than 1000 feet below the
aircraft altitude are not shown. Obstacles are shown behind the airspeed and altitude displays.
EIS
TERRAIN
Annunciation
AUDIO PANEL
& CNS
Obstacle
Warning
FLIGHT
MANAGEMENT
Potential
Impact
Point
HAZARD
AVOIDANCE
Figure 8-11 Obstacle
AFCS
FIELD OF VIEW
The PFD field of view can be represented on the MFD Navigation Map Page. Two dashed lines forming a
V‑shape in front of the aircraft symbol on the map, represent the forward viewing area shown on the PFD.
ADDITIONAL
FEATURES
Configuring field of view:
1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU.
2) Turn the large FMS Knob to highlight Map Setup and press the ENT Key.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
433
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
AUDIO PANEL
& CNS
Field of
View
FLIGHT
MANAGEMENT
Navigation Map Page OPTIONS Menu
Map Setup Menu, Map Group, Field of View Option
Figure 8-12 Option Menus
3) Turn the FMS Knob to select the Map Group and press the ENT Key.
HAZARD
AVOIDANCE
4) Turn the large FMS Knob to scroll through the Map Group options to FIELD OF VIEW.
5) Turn the small FMS Knob to select On or Off.
6) Press the FMS Knob to return to the Navigation Map Page.
AFCS
The following figure compares the PFD forward looking depiction with the MFD plan view and FIELD OF
VIEW turned on.
APPENDICES
ADDITIONAL
FEATURES
Lines
Depict
PFD Field
of View
SVS View on the PFD
Field of View on the MFD
INDEX
Figure 8-13 PFD and MFD Field of View Comparison
434
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
8.2 SAFETAXI
FLIGHT
INSTRUMENTS
SafeTaxi is an enhanced feature that gives greater map detail when viewing airports at close range. The
maximum map ranges for enhanced detail are pilot configurable. When viewing at ranges close enough to
show the airport detail, the map reveals taxiways with identifying letters/numbers, airport Hot Spots, and airport
landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at
lower map ranges. When the MFD display is within the SafeTaxi ranges, the airplane symbol on the airport
provides enhanced position awareness.
EIS
Designated Hot Spots are recognized at airports with many intersecting taxiways and runways, and/or complex
ramp areas. Airport Hot Spots are outlined to caution pilots of areas on an airport surface where positional
awareness confusion or runway incursions happen most often. Hot Spots are defined with a magenta circle or
outline around the region of possible confusion.
• VOR Information Page
• Inset Map (PFD)
• User Waypoint Information Page
• Weather Datalink Page
• Trip Planning Page
• Airport Information Page
• Nearest Pages
• Intersection Information Page
• Active and Stored Flight Plan Pages
FLIGHT
MANAGEMENT
• Navigation Map Page
AUDIO PANEL
& CNS
Any map page that displays the navigation view can also show the SafeTaxi airport layout within the maximum
configured range. The following is a list of pages where the SafeTaxi feature can be seen:
HAZARD
AVOIDANCE
• NDB Information Page
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
435
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLIGHT
INSTRUMENTS
During ground operations the aircraft’s position is displayed in reference to taxiways, runways, and airport
features. In the example shown, the aircraft is on taxiway Bravo approaching the High Alert Intersection boundary
on KSFO airport. Airport Hot Spots are outlined in magenta. When panning over the airport, features such as
runway holding lines and taxiways are shown at the cursor.
EIS
Aircraft
Position
AUDIO PANEL
& CNS
Taxiway
Identification
FLIGHT
MANAGEMENT
Airport Hot
Spot Outline
HAZARD
AVOIDANCE
Airport
Features
DCLTR Softkey
Removes Taxiway
Markings
Figure 8-14 SafeTaxi Depiction on the Navigation Map Page
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
The DCLTR Softkey (declutter) label advances to DCLTR-1, DCLTR -2, and DCLTR-3 each time the softkey is
selected for easy recognition of decluttering level. Selecting the DCLTR Softkey removes the taxiway markings
and airport feature labels. Selecting the DCLTR-1 Softkey removes VOR station ID, the VOR symbol, and
intersection names if within the airport plan view. Selecting the DCLTR-2 Softkey removes the airport runway
layout, unless the airport in view is part of an active route structure. Selecting the DCLTR-3 Softkey cycles back
to the original map detail. Refer to Map Declutter Levels in the Flight Management Section.
436
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Configuring SafeTaxi range:
1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU.
2) Turn the large FMS Knob to highlight the Map Setup Menu Option and press the ENT Key.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Figure 8-15 Navigation Map PAGE MENU, Map Setup Option
3) Turn the FMS Knob to select the Aviation Group and press the ENT Key.
4) Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI.
FLIGHT
MANAGEMENT
5) Turn the small FMS Knob to display the range of distances.
6) Turn either FMS Knob to select the desired distance for maximum SafeTaxi display range.
7) Press the ENT Key to complete the selection.
HAZARD
AVOIDANCE
8) Press the FMS Knob to return to the Navigation Map Page.
AFCS
SAFETAXI
Option
ADDITIONAL
FEATURES
SafeTaxi
Range
Options
APPENDICES
INDEX
Figure 8-16 MAP SETUP Menu, Aviation Group, SAFETAXI Range Options
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
437
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
SAFETAXI CYCLE NUMBER AND REVISION
FLIGHT
INSTRUMENTS
SafeTaxi database is revised every 56 days. SafeTaxi is always available for use after the expiration date. When turning on the system, the Power-up Page indicates whether the databases are current, out of date, or
not available.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
SafeTaxi Database
Figure 8-17 Power-up Page, SafeTaxi Database
HAZARD
AVOIDANCE
Power-up Page Display
Definition
Normal operation. SafeTaxi database is valid and within current cycle.
SafeTaxi database has expired.
AFCS
Database card contains no SafeTaxi data.
Table 8-1 SafeTaxi Annunciation Definitions
ADDITIONAL
FEATURES
The SafeTaxi Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found
on the AUX - System Status page, as seen in Figure 8-18.
INDEX
APPENDICES
Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed
information by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is
shown.
438
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
The SafeTaxi database cycle number shown in the figure, 12S1, is deciphered as follows:
12 – Indicates the year 2012
S – Indicates the data is for SafeTaxi
FLIGHT
INSTRUMENTS
1 – Indicates the first issue of the SafeTaxi database for the year
The SafeTaxi EFFECTIVE date 13–JAN–12 is the beginning date for the current database cycle. SafeTaxi
EXPIRES date 10–MAR–12 is the revision date for the next database cycle.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
SafeTaxi Data
HAZARD
AVOIDANCE
Figure 8-18 AUX – System Status Page, SafeTaxi Current Information
AFCS
ADDITIONAL
FEATURES
SafeTaxi information appears in blue and yellow text. The EFFECTIVE date appears in blue when data is
current and in yellow when the current date is before the effective date. The EXPIRES date appears in blue
when data is current and in yellow when expired (Figures 8‑18 and 8-19). NOT AVAILABLE appears in blue
in the REGION field if SafeTaxi data is not available on the database card (Figure 8‑19). An expired SafeTaxi
database is not disabled and will continue to function indefinitely.
APPENDICES
Select the MFD1 DB Softkey a second time. The softkey label will change to PFD1 DB. The DATABASE
window will now be displaying database information for PFD1. As before, scroll through the listed information
by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is shown.
Refer to Updating Garmin Databases in Appendix B for instructions on revising the SafeTaxi database.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
439
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Figure 8-19 illustrates possible SafeTaxi database conditions that may appear on the AUX - System Status
Page. The EFFECTIVE date is the beginning date for this database cycle. If the present date is before the
effective date, the EFFECTIVE date appears in yellow and the EXPIRES date appears in blue. The EXPIRES date
is the revision date for the next database cycle. NOT AVAILABLE indicates that SafeTaxi is not available on the
database card or no database card is inserted.
FLIGHT
MANAGEMENT
Current Date is before Effective Date
SafeTaxi Database has Expired
SafeTaxi Database Not Installed
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Figure 8-19 AUX – System Status Page, SafeTaxi Database Status
440
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
8.3 CHARTVIEW (OPTIONAL)
FLIGHT
INSTRUMENTS
ChartView resembles the paper version of Jeppesen terminal procedures charts. The charts are displayed in full
color with high-resolution. The MFD depiction shows the aircraft position on the moving map in the planview
of approach charts and on airport diagrams. Airport Hot Spots are outlined in magenta.
The geo-referenced aircraft position is indicated by an aircraft symbol displayed on the chart when the current
position is within the boundaries of the chart. Inset boxes (Figure 8-20) are not considered within the chart
boundaries. Therefore, when the aircraft symbol reaches a chart boundary line, or inset box, the aircraft symbol
is removed from the display.
EIS
Figure 8-20 shows examples of off-scale areas, indicated by the grey shading. Note, the grey shading is for
illustrative purposes only and will not appear on the published chart or MFD display. These off-scale areas
appear on the chart to convey supplemental information. However, the depicted geographical position of this
information, as it relates to the chart planview, is not the actual geographic position. Therefore, when the aircraft
symbol appears within one of these areas, the aircraft position indicated is relative to the chart planview, not to
the off-scale area.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Off-Scale
Area
Off-Scale
Areas
AFCS
ADDITIONAL
FEATURES
Figure 8-20 Sample Chart Indicating Off-Scale Areas
APPENDICES
NOTE: Do not maneuver the aircraft based solely upon the geo-referenced aircraft symbol.
The ChartView database subscription is available from Jeppesen, Inc. Available data includes:
• Arrivals (STAR)
• Airport Diagrams
• Departure Procedures (DP)
• NOTAMs
INDEX
• Approaches
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
441
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
CHARTVIEW SOFTKEYS
FLIGHT
INSTRUMENTS
ChartView functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest
Airports Page, or Flight Plan Page, selecting the SHW CHRT Softkey displays the available terminal chart and
advances to the chart selection level of softkeys: CHRT OPT, CHRT, INFO-1, DP, STAR, APR, WX, NOTAM,
and GO BACK. The chart selection softkeys shown below appear on the Airport Information Page.
Selecting the GO BACK Softkey reverts to the top level softkeys and previous page.
Selecting the CHRT OPT Softkey advances to the next level of softkeys: ALL, HEADER, PLAN, PROFILE,
MINIMUMS, FIT WDTH, FULL SCN, and BACK.
EIS
While viewing the CHRT OPT Softkeys, after 45 seconds of softkey inactivity, the system reverts to the chart
selection softkeys.
AUDIO PANEL
& CNS
SHW CHRT
CHRT
INFO-1
DP
FLIGHT
MANAGEMENT
CHRT OPT
STAR
APR
WX
NOTAM
GO BACK
Pressing the GO BACK Softkey returns
to the top-level softkeys and previous page.
HAZARD
AVOIDANCE
ALL
HEADER
PLAN
PROFILE
MINIMUMS FIT WDTH FULL SCN
BACK
Pressing the BACK Softkey returns
to the Chart Selection Softkeys.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 8-21 ChartView SHW CHRT, Chart Selection, and Chart Option Softkeys
442
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
TERMINAL PROCEDURES CHARTS
Selecting Terminal Procedures Charts:
FLIGHT
INSTRUMENTS
While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, select the SHW CHRT
Softkey.
Or:
1) Press the MENU Key to display the PAGE MENU.
2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart.
EIS
3) Press the ENT Key to display the chart.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Navigation Map Page OPTIONS Menu
Waypoint Airport Information Page OPTIONS Menu
Figure 8-22 Option Menus
AFCS
When no terminal procedure chart is available for the nearest airport or the selected airport, the banner
CHART NOT AVAILABLE appears on the screen. The CHART NOT AVAILABLE banner does not refer to
the Jeppesen subscription, but rather the availability of a particular airport chart selection or procedure for a
selected airport.
ADDITIONAL
FEATURES
Figure 8-23 Chart Not Available Banner
APPENDICES
If there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner
UNABLE TO DISPLAY CHART is then displayed.
INDEX
Figure 8-24 Unable To Display Chart Banner
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
443
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
When a chart is not available by selecting the SHW CHRT Softkey or selecting a Page Menu Option, charts
may be obtained for other airports from the WPT Pages or Flight Plan Pages.
FLIGHT
INSTRUMENTS
If a chart is available for the destination airport, or the airport selected in the active flight plan, the chart
appears on the screen. When no flight plan is active, or when not flying to a direct-to destination, selecting the
SHW CHRT Softkey displays the chart for the nearest airport, if available.
The chart shown is one associated with the WPT – Airport Information page. Usually this is the airport runway
diagram. Where no runway diagram exists, but Take Off Minimums or Alternate Minimums are available, that
page appears. If Airport Information pages are unavailable, the Approach Chart for the airport is shown.
EIS
Selecting a chart:
1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, select the SHW CHRT
Softkey. The airport diagram or approach chart is displayed on the Airport Information Page.
AUDIO PANEL
& CNS
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to select either the Airport Identifier Box or the Approach Box. (Select the APR Softkey
if the Approach Box is not currently shown).
FLIGHT
MANAGEMENT
4) Turn the small and large FMS Knob to enter the desired airport identifier.
5) Press the ENT Key to complete the airport selection.
6) Turn the large FMS Knob to select the Approach Box.
7) Turn the small FMS Knob to show the approach chart selection choices.
HAZARD
AVOIDANCE
8) Turn either FMS Knob to scroll through the available charts.
9) Press the ENT Key to complete the chart selection.
ADDITIONAL
FEATURES
AFCS
Chart Scale
Select Desired
Approach Chart
From Menu
INDEX
APPENDICES
Scroll Through
Chart With
the Joystick
Figure 8-25 Approach Information Page, Chart Selection
444
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
While the APPROACH Box is selected using the FMS Knob, the G1000 softkeys are blank. Once the desired
chart is selected, the chart scale can be changed and the chart page can be scrolled using the Joystick. Pressing
the Joystick centers the chart on the screen.
FLIGHT
INSTRUMENTS
The aircraft symbol is shown on the chart only if the chart is to scale and the aircraft position is within
the boundaries of the chart. The aircraft symbol is not displayed when the Aircraft Not Shown Icon appears
(Figure 8‑29). If the Chart Scale Box displays a banner NOT TO SCALE, the aircraft symbol is not shown. The
Aircraft Not Shown Icon may appear at certain times, even if the chart is displayed to scale.
EIS
Selecting the CHRT Softkey switches between the ChartView diagram and the associated map in the WPT
page group. In the example shown, the CHRT Softkey switches between the DeKalb Peachtree (KPDK) Airport
Diagram and the navigation map on the WPT – Airport Information page.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Select CHRT Softkey
to Switch Between
ChartView and WPT Airport Information Page
APPENDICES
INDEX
Figure 8-26 CHRT Softkey, Airport Information Page
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
445
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
Selecting the INFO-1 or INFO-2 Softkey returns to the airport diagram when the view is on a different chart. If the displayed chart is the airport diagram, the INFO-1 or INFO-2 Softkey has no effect.
FLIGHT
INSTRUMENTS
The aircraft position is shown in magenta on the ChartView diagrams when the location of the aircraft is
within the chart boundaries. In the example shown, the aircraft is taxiing on Taxiway Alpha on the Charlotte,
NC (KCLT) airport.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Another source for additional airport information is from the INFO Box above the chart for certain airports. This information source is not related to the INFO-1 or INFO-2 Softkey. When the INFO Box is selected using
the FMS Knob, the G1000 softkeys are blank. The Charlotte, NC airport has five additional charts offering
information; the Airport Diagram, Take-off Minimums, Class B Airspace, Airline Parking Gate Coordinates, and
Airline Parking Gate Location. (The numbers in parentheses after the chart name are Jeppesen designators.)
AFCS
HAZARD
AVOIDANCE
Aircraft
Current
Position
INDEX
APPENDICES
ADDITIONAL
FEATURES
Figure 8-27 Airport Information Page, INFO View, Full Screen Width
446
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
In the example shown in Figure 8-27, the Class B Chart is selected. Pressing the ENT Key displays the
Charlotte Class B Airspace Chart (Figure 8-28).
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 8-28 Airport Information Page, Class B Chart Selected from INFO View
HAZARD
AVOIDANCE
Selecting the DP Softkey displays the Departure Procedure Chart if available.
Chart Not
To Scale
AFCS
ADDITIONAL
FEATURES
APPENDICES
Aircraft Not
Shown Icon
INDEX
Figure 8-29 Departure Information Page
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
447
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
Selecting the STAR Softkey displays the Standard Terminal Arrival Chart if available.
FLIGHT
INSTRUMENTS
Chart Not
To Scale
AUDIO PANEL
& CNS
EIS
Change Range
and Scroll
Through the
Chart With the
Joystick
FLIGHT
MANAGEMENT
Aircraft Not
Shown Icon
Figure 8-30 Arrival Information Page
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Selecting the APR Softkey displays the approach chart for the airport if available.
Figure 8-31 Approach Information Page
448
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Selecting the WX Softkey shows the airport weather frequency information, and includes weather data such
as METAR and TAF from the XM Data Link Receiver, when available. Weather information is available only
when an XM Data Link Receiver is installed and the SiriusXM Weather subscription is current.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
WX Info
When
Available
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 8-32 Weather Information Page
NOTE: A subdued softkey label indicates the function is disabled.
AFCS
NOTE: Only NOTAMs applicable to specific information conveyed on the displayed Jeppesen chart are
available when the NOTAM Softkey is selected. There may be other NOTAMs available pertaining to the
flight that may not be displayed. Contact Jeppesen for more information regarding Jeppesen databasepublished NOTAMs.
ADDITIONAL
FEATURES
Recent NOTAMS applicable to the current ChartView cycle are included in the ChartView database. Selecting
the NOTAM Softkey shows the local NOTAM information for selected airports, when available. When NOTAMS
are not available, the NOTAM Softkey label appears subdued and is disabled as shown in Figure 8-32. The
NOTAM Softkey may appear on the Airport Information Page and all of the chart page selections.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
449
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLIGHT
MANAGEMENT
NOTAM
Softkey
Appears for
Selected
Airports
Figure 8-33 NOTAM Softkey Highlighted
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Local
NOTAM on
This Airport
NOTAM
Softkey
Selected
Figure 8-34 Airport Information Page, Local NOTAMs
INDEX
Selecting the NOTAM Softkey again removes the NOTAMS information.
Selecting the GO BACK Softkey reverts to the previous page (Navigation Map Page, Nearest Pages, or Flight
Plan Page).
450
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
CHART OPTIONS
Selecting the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-21).
Selecting the ALL Softkey shows the complete approach chart on the screen.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Complete
Chart
Shown
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 8-35 Approach Information Page, ALL View
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
451
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLIGHT
INSTRUMENTS
Selecting the HEADER Softkey shows the header view (approach chart briefing strip) on the screen.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Approach
Chart
Briefing Strip
Figure 8-36 Approach Information Page, Header View
AFCS
HAZARD
AVOIDANCE
Selecting the PLAN Softkey shows the approach chart two dimensional plan view.
INDEX
APPENDICES
ADDITIONAL
FEATURES
Approach
Chart Plan
View
Figure 8-37 Approach Information Page, Plan View
452
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Selecting the PROFILE Softkey displays the approach chart descent profile strip.
FLIGHT
INSTRUMENTS
EIS
Approach
Chart Descent
Profile Strip
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 8-38 Approach Information Page, Profile View, Full Screen Width
HAZARD
AVOIDANCE
Selecting the MINIMUMS Softkey displays the minimum descent altitude/visibility strip at the bottom of the
approach chart.
AFCS
ADDITIONAL
FEATURES
Minimum
Descent
Altitude/
Visibility Strip
APPENDICES
INDEX
Figure 8-39 Approach Information Page, Minimums View, Full Screen Width
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
453
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
If the chart scale has been adjusted to view a small area of the chart, selecting the FIT WIDTH Softkey
changes the chart size to fit the available screen width.
Select FIT WDTH
Softkey to Show
Full Chart Width
INDEX
APPENDICES
Figure 8-40 Airport Information Page, FIT WDTH Softkey Selected
454
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Selecting the FULL SCN Softkey alternates between removing and replacing the data window to the right.
Selecting Additional Information:
FLIGHT
INSTRUMENTS
1) While viewing the Airport Taxi Diagram, select the FULL SCN Softkey to display the information windows
(AIRPORT, INFO).
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the AIRPORT, INFO, RUNWAYS, or FREQUENCIES Box (INFO Box shown).
4) Turn the small FMS Knob to select the INFO Box choices. If multiple choices are available, scroll to the desired
choice with the large FMS Knob and press the ENT Key to complete the selection.
EIS
5) Press the FMS Knob again to deactivate the cursor.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Available
Information
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Select FULL SCN
Softkey to Switch
Between Full
Screen and Chart
With Info Window
APPENDICES
Figure 8-41 Airport Information Page, Full Screen and Info Window
INDEX
Selecting the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
455
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
The full screen view can also be selected by using the page menu option.
Selecting full screen On or Off:
FLIGHT
INSTRUMENTS
1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key.
3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
4) Turn the small FMS Knob to choose between the On and Off Full Screen Options.
Chart Setup Option
Full Screen On/Off Selection
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Figure 8-42 Page Menus
456
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
DAY/NIGHT VIEW
FLIGHT
INSTRUMENTS
ChartView can be displayed on a white or black background for day or night viewing. The Day View offers
a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark
environment. When the CHART SETUP Box is selected the G1000 softkeys are blank.
Selecting Day, Night, or Automatic View:
1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Figure 8-43 Waypoint Information Page, OPTIONS Menu
3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑44).
4) Turn the small FMS Knob to choose between Day, Auto, and Night Options.
AFCS
5) If Auto Mode is selected, turn the large FMS Knob to select the percentage field. Use the small FMS Knob to
change the percentage value. The percentage value is the day/night crossover point based on the percentage of
backlighting intensity. For example, if the value is set to 15%, the day/night display changes when the display
backlight reaches 15% of full brightness.
ADDITIONAL
FEATURES
The display must be changed in order for the new setting to become active. This may be accomplished by
selecting another page or changing the display range.
6) Press the FMS Knob when finished to remove the Chart Setup Menu.
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
457
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Figure 8-44 Arrival Information Page, Day View
INDEX
Figure 8-45 Arrival Information Page, Night View
458
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
CHARTVIEW CYCLE NUMBER AND EXPIRATION DATE
FLIGHT
INSTRUMENTS
ChartView database is revised every 14 days. Charts are still viewable during a period that extends from the
cycle expiration date to the disables date. ChartView is disabled 70 days after the expiration date and is no
longer available for viewing. When turning on the system, the Power-up Page displays the current status of the
ChartView database. See the table below for the various ChartView Power-up Page displays and the definition
of each.
EIS
AUDIO PANEL
& CNS
ChartView Database
FLIGHT
MANAGEMENT
Figure 8-46 Power-up Page, ChartView Database
Definition
Blank Line. system is not configured for ChartView. Contact a Garminauthorized service center for configuration.
System is configured for ChartView but no chart database is installed.
Contact Jeppesen for a ChartView database.
Normal operation. ChartView database is valid and within current
cycle.
ChartView database is within 1 week after expiration date. A new cycle
is available for update.
ChartView database is beyond 1 week after expiration date, but still
within the 70 day viewing period.
ChartView database has timed out. Database is beyond 70 days after
expiration date. ChartView database is no longer available for viewing.
System time is not available. GPS satellite data is unknown or the
system has not yet locked onto satellites. Check database cycle number
for effectivity.
System is verifying chart database when new cycle is installed for the
first time.
After verifying, chart database is found to be corrupt. ChartView is not
available.
HAZARD
AVOIDANCE
Power-up Page Display
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Table 8-2 ChartView Power-up Page Annunciations and Definitions
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
459
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLIGHT
INSTRUMENTS
The ChartView time critical information can also be found on the AUX - System Status page. The database
CYCLE number, EXPIRES, and DISABLES dates of the ChartView subscription appear in either blue or yellow
text. When the ChartView EXPIRES date is reached, ChartView becomes inoperative 70 days later. This is
shown as the DISABLES date. When the DISABLES date is reached, charts are no longer available for viewing. The SHW CHRT Softkey label then appears subdued and is disabled until a revised issue of ChartView is
installed.
NOTE: A subdued softkey label indicates the function is disabled.
EIS
Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed
information by turning the FMS Knob or pressing the ENT Key until the ChartView database information is
shown.
AUDIO PANEL
& CNS
The ChartView database cycle number shown in the figure, 1203, is deciphered as follows:
12 – Indicates the year 2012
03 – Indicates the third issue of the ChartView database for the year
FLIGHT
MANAGEMENT
The EXPIRES date 17–FEB–12 is the date that this database should be replaced with the next issue.
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
The DISABLES date 28–APR–12 is the date that this database becomes inoperative.
APPENDICES
ChartView
Data
Figure 8-47 AUX – System Status Page, ChartView Current and Available
INDEX
The ChartView database is provided directly from Jeppesen. Refer to Updating Jeppesen Databases in
Appendix B for instructions on revising the ChartView database.
460
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Other possible AUX - System Status page conditions are shown in Figure 8-48. The EXPIRES date, in yellow,
is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database
cycle is no longer viewable. CYCLE NOT AVAILABLE in blue, indicates no ChartView data is available on the
database card or no database card is inserted.
FLIGHT
INSTRUMENTS
EIS
ChartView Database is Disabled
AUDIO PANEL
& CNS
ChartView has Expired, but is not Disabled
ChartView Database is Not Available
FLIGHT
MANAGEMENT
Figure 8-48 AUX – System Status Page, ChartView Database Status
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
461
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
8.4 FLITECHARTS
FLIGHT
INSTRUMENTS
FliteCharts resemble the paper version of AeroNav Services terminal procedures charts. The charts are
displayed with high-resolution and in color for applicable charts. FliteCharts database subscription is available
from Garmin. Available data includes:
• Arrivals (STAR)
• Approaches
• Departure Procedures (DP)
• Airport Diagrams
EIS
FLITECHARTS SOFTKEYS
AUDIO PANEL
& CNS
FliteCharts functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest
Airports Page, or Flight Plan Page, selecting the SHW CHRT Softkey displays the available terminal chart and
advances to the chart selection level of softkeys: CHRT OPT, CHRT, INFO-1, DP, STAR, APR, WX, and
GO BACK. The chart selection softkeys appear on the Airport Information Page.
Selecting the GO BACK Softkey reverts to the top level softkeys and previous page.
FLIGHT
MANAGEMENT
Selecting the CHRT OPT Softkey displays the available terminal chart and advances to the next level of
softkeys: ALL, FIT WDTH, FULL SCN, and BACK.
While viewing the CHRT OPT Softkeys, after 45 seconds of softkey inactivity, the system reverts to the chart
selection softkeys.
NOTAMs are not available with FliteCharts. The NOTAM Softkey label appears subdued and is disabled.
HAZARD
AVOIDANCE
SHW CHRT
AFCS
CHRT OPT
CHRT
INFO-1
DP
STAR
APR
WX
GO BACK
Presssing the GO BACK Softkey returns
to the top-level softkeys and previous page.
ADDITIONAL
FEATURES
ALL
FIT WDTH
FULL SCN
BACK
Pressing the BACK Softkey returns
to the Chart Selection Softkeys.
INDEX
APPENDICES
Figure 8-49 FliteCharts SHW CHRT, Chart Selection, and Chart Option Softkeys
462
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
TERMINAL PROCEDURES CHARTS
Selecting Terminal Procedures Charts:
FLIGHT
INSTRUMENTS
While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, select the SHW CHRT
Softkey.
Or:
1) Press the MENU Key to display the PAGE MENU.
2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart.
EIS
3) Press the ENT Key to display the chart.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Navigation Map Page OPTIONS Menu
Waypoint Airport Information Page OPTIONS Menu
Figure 8-50 Option Menus
AFCS
When no terminal procedure chart is available, the banner CHART NOT AVAILABLE appears on the screen. The CHART NOT AVAILABLE banner does not refer to the FliteCharts subscription, but rather the availability
of a particular airport chart selection or procedure for a selected airport.
ADDITIONAL
FEATURES
Figure 8-51 Chart Not Available Banner
APPENDICES
If there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner
UNABLE TO DISPLAY CHART is then displayed.
INDEX
Figure 8-52 Unable To Display Chart Banner
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
463
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
When a chart is not available by selecting the SHW CHRT Softkey or selecting a Page Menu Option, charts
may be obtained for other airports from the WPT Pages or Flight Plan Pages.
FLIGHT
INSTRUMENTS
If a chart is available for the destination airport, or the airport selected in the active flight plan, the chart
appears on the screen. When no flight plan is active, or when not flying to a direct-to destination, selecting the
SHW CHRT Softkey displays the chart for the nearest airport, if available.
The chart shown is one associated with the WPT – Airport Information page. Usually this is the airport runway
diagram. Where no runway diagram exists, but Take Off Minimums or Alternate Minimums are available, that
page appears. If Airport Information pages are unavailable, the Approach Chart for the airport is shown.
EIS
Selecting a chart:
1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, select the SHW CHRT
Softkey. The airport diagram or approach chart is displayed on the Airport Information Page.
AUDIO PANEL
& CNS
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to select either the Airport Identifier Box or the Approach Box. (Select the APR Softkey
if the Approach Box is not currently shown).
FLIGHT
MANAGEMENT
4) Turn the small and large FMS Knob to enter the desired airport identifier.
5) Press the ENT Key to complete the airport selection.
6) Turn the large FMS Knob to select the Approach Box.
7) Turn the small FMS Knob to show the approach chart selection choices.
HAZARD
AVOIDANCE
8) Turn either FMS Knob to scroll through the available charts.
9) Press the ENT Key to complete the chart selection.
AFCS
Chart Not
To Scale
ADDITIONAL
FEATURES
Select Desired
Approach
Chart from
Menu
APPENDICES
Pan Chart
With the
Joystick
INDEX
Aircraft Not
Shown Icon
Figure 8-53 Approach Information Page, Chart Selection
464
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
While the APPROACH Box is selected using the FMS Knob, the G1000 softkeys are blank. Once the desired
chart is selected, the chart scale can be changed and the chart can be panned using the Joystick. Pressing the
Joystick centers the chart on the screen.
FLIGHT
INSTRUMENTS
The aircraft symbol is not shown on FliteCharts. The Chart Scale Box displays a banner NOT TO SCALE, and
the Aircraft Not Shown Icon is displayed in the lower right corner of the screen.
Selecting the CHRT Softkey alternates between the FliteCharts diagram and the associated map in the WPT
page group. In the example shown, the CHRT Softkey switches between the Charlotte, NC (KCLT) Airport
Diagram and the navigation map on the WPT – Airport Information page.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
Select CHRT Softkey
to Switch Between
FliteCharts and
Navigation Map Page
ADDITIONAL
FEATURES
APPENDICES
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
Figure 8-54 CHRT Softkey, Airport Information Page
465
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
Selecting the INFO-1 or INFO-2 Softkey returns to the airport diagram when the view is on a different chart. If the displayed chart is the airport diagram, the INFO-1 or INFO-2 Softkey has no effect.
EIS
FLIGHT
INSTRUMENTS
Another source for additional airport information is from the INFO Box above the chart (Figure 8-53) or to
the right of the chart (Figure 8-55) for certain airports. This information source is not related to the INFO1 or INFO-2 Softkey. When the INFO Box is selected using the FMS Knob, the G1000 softkeys are blank. The Charlotte, NC airport has three additional charts offering information; the Airport Diagram, Alternate
Minimums, and Take-off Minimums.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Info Box
Selected
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 8-55 Airport Information Page, INFO View with Airport Information
466
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
In the example shown in Figure 8-55, TAKE OFF MINIMUMS is selected. Pressing the ENT Key displays the
Take-off Minimums and Departure Procedures Chart (Figure 8-56).
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 8-56 Airport Information Page, TAKE OFF MINIMUMS Selected from INFO View
HAZARD
AVOIDANCE
Selecting the DP Softkey displays the Departure Procedure Chart if available.
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 8-57 Departure Information Page
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
467
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Selecting the STAR Softkey displays the Standard Terminal Arrival Chart if available.
Figure 8-58 Arrival Information Page
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Selecting the APR Softkey displays the approach chart for the airport if available.
INDEX
Figure 8-59 Approach Information Page
468
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Selecting the WX Softkey shows the airport weather frequency information, when available, and includes
weather data such as METAR and TAF from the XM Data Link Receiver. Weather information is available only
when an XM Data Link Receiver is installed and the SiriusXM Weather subscription is current.
FLIGHT
INSTRUMENTS
Selecting Additional Information:
1) While viewing the Airport Taxi Diagram, select the WX Softkey to display the information windows (AIRPORT,
INFO).
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the INFO Box.
EIS
4) Turn the small FMS Knob to select the INFO Box choices. When the INFO Box is selected the G1000 softkeys
are blank. If multiple choices are available, scroll to the desired choice with the large FMS Knob and press the
ENT Key to complete the selection.
AUDIO PANEL
& CNS
5) Press the FMS Knob again to deactivate the cursor.
FLIGHT
MANAGEMENT
Info Available
on This Airport
HAZARD
AVOIDANCE
WX Info
When
Available
AFCS
Chart Not
To Scale
Figure 8-60 Weather Information Page, WX Softkey Selected
ADDITIONAL
FEATURES
Softkeys are
Blank during
Info Box
Selection
WX Softkey
Selected
APPENDICES
Selecting the GO BACK Softkey reverts to the previous page (Navigation Map Page or Flight Plan Page).
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
469
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
CHART OPTIONS
Selecting the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-49).
EIS
FLIGHT
INSTRUMENTS
Selecting the ALL Softkey shows the complete chart on the screen.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Complete
Chart
Shown
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 8-61 Airport Information Page, ALL View Selected
470
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Selecting the FIT WIDTH Softkey fits the width of the chart in the display viewing area. In the example
shown, the chart at close range is replaced with the full width chart.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Select FIT WDTH
Softkey to Show
Full Chart Width
Figure 8-62 Approach Information Page, FIT WDTH Softkey Selected
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
471
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Selecting the FULL SCN Softkey alternates between removing and replacing the data window to the right.
AFCS
HAZARD
AVOIDANCE
Select FULL SCN
Softkey to Switch
Between Chart on
Full Screen and Chart
with Info Window
ADDITIONAL
FEATURES
Figure 8-63 Airport Information Page, Full Screen and Info Window
INDEX
APPENDICES
Selecting the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys.
472
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
The full screen view can also be selected by using the page menu option.
Selecting full screen On or Off:
FLIGHT
INSTRUMENTS
1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key.
3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options.
4) Turn the small FMS Knob to choose between the On and Off Full Screen Options.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Chart Setup Option
Full Screen On/Off Selection
HAZARD
AVOIDANCE
Figure 8-64 Page Menus
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
473
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
DAY/NIGHT VIEW
FLIGHT
INSTRUMENTS
FliteCharts can be displayed on a white or black background for day or night viewing. The Day View offers
a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark
environment. When the CHART SETUP Box is selected the G1000 softkeys are blank.
Selecting Day, Night, or Automatic View:
1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key.
HAZARD
AVOIDANCE
Figure 8-65 Waypoint Information Page, OPTIONS Menu
3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑66).
4) Turn the small FMS Knob to choose between Day, Auto, and Night Options.
AFCS
5) If Auto Mode is selected, turn the large FMS Knob to select the percentage field. Use the small FMS Knob to
change the percentage value. The percentage value is the day/night crossover point based on the percentage of
backlighting intensity. For example, if the value is set to 15%, the day/night display changes when the display
backlight reaches 15% of full brightness.
ADDITIONAL
FEATURES
The display must be changed in order for the new setting to become active. This may be accomplished by
selecting another page or changing the display range.
INDEX
APPENDICES
6) Press the FMS Knob when finished to remove the Chart Setup Menu.
474
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 8-66 Approach Information Page, Day View
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
Figure 8-67 Approach Information Page, Night View
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
475
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
FLITECHARTS CYCLE NUMBER AND EXPIRATION DATE
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
FliteCharts data is revised every 28 days. Charts are still viewable during a period that extends from the cycle
expiration date to the disables date. FliteCharts is disabled 180 days after the expiration date and are no longer
available for viewing upon reaching the disables date. When turning on the system, the Power-up Page displays
the current status of the FliteCharts database. See the table below for the various FliteCharts Power-up Page
displays and the definition of each.
FLIGHT
MANAGEMENT
FliteCharts Database
HAZARD
AVOIDANCE
Figure 8-68 Power-up Page, FliteCharts Database
ADDITIONAL
FEATURES
AFCS
Power-up Page Display
Definition
Blank Line. system is not configured for FliteCharts. Contact a Garminauthorized service center for configuration.
System is configured for FliteCharts but no chart database is installed.
Refer to Updating Garmin Databases in Appendix B for the FliteCharts
database
Normal operation. FliteCharts database is valid and within current
cycle.
FliteCharts database is beyond the expiration date, but still within the
180 day viewing period.
FliteCharts database has timed out. Database is beyond 180 days
after expiration date. FliteCharts database is no longer available for
viewing.
APPENDICES
Table 8-3 FliteCharts Power-up Page Annunciations and Definitions
INDEX
Other possible AUX - System Status page conditions are shown in Figure 8-69. ‘FliteCharts Expires’ plus a
date in white, indicates the chart database is current. ‘Chart data is out of date!’ in yellow, indicates charts are
still viewable, but approaching the disable date.
When the 180 day grace period has expired, ‘Chart data is disabled.’ in yellow indicates that the FliteCharts
database has expired and is no longer viewable. ‘Chart Data: N/A’ appears in white if no FliteCharts data is
available on the database card or no database card is inserted.
476
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
FliteCharts time critical information can also be found on the AUX - System Status page. The FliteCharts
database REGION, CYCLE number, EFFECTIVE, EXPIRES, and DISABLES dates of the subscription appear in
either blue or yellow text. Dates shown in blue are current data. Dates shown in yellow indicate the data is not
within the current subscription period.
FLIGHT
INSTRUMENTS
FliteCharts becomes inoperative 180 days after the FliteCharts EXPIRES date is reached, and is no longer
available for viewing. This date is shown as the DISABLES date. After the disable date the SHW CHRT Softkey
label appears subdued and is unavailable until a revised issue of FliteCharts is installed.
NOTE: A subdued softkey label indicates the function is disabled.
EIS
AUDIO PANEL
& CNS
Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed
information by turning the FMS Knob or pressing the ENT Key until the FliteCharts database information is
shown.
The FliteCharts database cycle number shown in the figure, 1202, is deciphered as follows:
12 – Indicates the year 2012
02 – Indicates the second issue of the FliteCharts database for the year
FLIGHT
MANAGEMENT
The FliteCharts EFFECTIVE date 10–FEB–12 is the first date that this database is current.
The FliteCharts EXPIRES date 10–MAR–12 is the last date that this database is current.
The DISABLES date 06–SEP–12 is the date that this database becomes inoperative.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
FliteCharts
Data
Figure 8-69 AUX – System Status Page, FliteCharts Current and Available
INDEX
The FliteCharts database is provided from Garmin. Refer to Updating Garmin Databases in Appendix B for
instructions on revising the FliteCharts database.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
477
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
The other four possible AUX - System Status page conditions are shown here. The EFFECTIVE date, in
yellow, indicates the current date precedes the date the FliteCharts database becomes effective. The EXPIRES
date, in yellow, is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that
this database cycle is no longer viewable. NOT AVAILABLE in blue, indicate the FliteCharts database is not
available on the database card or no database card is inserted.
FliteCharts Expired, but is not Disabled
FliteCharts Database is Disabled
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Current Date is Before Effective Date
ADDITIONAL
FEATURES
FliteCharts Database is Not Available
INDEX
APPENDICES
Figure 8-70 AUX – System Status Page, FliteCharts Datbase Status
478
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
8.5 AIRPORT DIRECTORY
FLIGHT
INSTRUMENTS
The Aircraft Owners and Pilots Association (AOPA) and AC-U-KWIK Airport Directory databases offer detailed
information regarding services, hours of operation, lodging options, and more. This information is viewed on
the Airport Information Page by selecting the INFO Softkey until INFO-2 is displayed as shown in Figure 8-71. Both Airport Directories are available for downloading at flygarmin.com. However, copy only one of the
databases to the Supplemental Data Card. The system cannot recognize both databases simultaneously.
Selecting the Airport Directory Page:
EIS
1) Turn the large FMS Knob to select the ‘WPT’ page group.
2) Turn the small FMS Knob to select the AIRPORT INFORMATION Page. Initially, information for the airport closest
to the aircraft’s present position is displayed.
AUDIO PANEL
& CNS
3) If necessary, select the INFO softkey until INFO-2 is displayed.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 8-71 Airport Directory Information on the Airport Information Page
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
479
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
AIRPORT DIRECTORY DATABASE CYCLE NUMBER AND REVISION
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
The Airport Directory databases are revised every 56 days. Check fly.garmin.com for the current database. The Airport Directory is always available for use after the expiration date. When turning on the system, the
Power-up Page indicates whether the databases are current, out of date, or not available.
FLIGHT
MANAGEMENT
Airport Directory Database
Figure 8-72 Power-up Page, Airport Directory Database
HAZARD
AVOIDANCE
Power-up Page Display
Definition
Normal operation. Airport Directory database is valid and within
current cycle.
Airport Directory database has expired.
AFCS
Database card contains no Airport Directory data.
Table 8-4 Airport Directory Annunciation Definitions
INDEX
APPENDICES
ADDITIONAL
FEATURES
The Airport Directory Region, Version, Cycle, Effective date and Expires date of the database cycle can also be
found on the AUX - System Status page, as seen in Figure 8-73.
480
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed
information by turning the FMS Knob or pressing the ENT Key until the Airport Directory database information
is shown.
FLIGHT
INSTRUMENTS
The Airport Directory database cycle number shown in the figure, 12D1, is deciphered as follows:
12 – Indicates the year 2012
D – Indicates the data is for Airport Directory
1 – Indicates the first issue of the Airport Directory database for the year
EIS
The Airport Directory EFFECTIVE date 13–JAN–12 is the beginning date for the current database cycle. The
Airport Directory EXPIRES date 10–MAR–12 is the revision date for the next database cycle.
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Airport Directory
Data
HAZARD
AVOIDANCE
AFCS
Figure 8-73 AUX – System Status Page, Airport Directory Current Information
ADDITIONAL
FEATURES
APPENDICES
Airport Directory information appears in blue and yellow text. The EFFECTIVE date appears in blue when
data is current and in yellow when the current date is before the effective date. The EXPIRES date appears in
blue when data is current and in yellow when expired (Table 8-4). NOT AVAILABLE appears in blue in the
REGION field if Airport Directory data is not available on the database card. An expired Airport Directory
database is not disabled and will continue to function indefinitely.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
481
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
8.6 SIRIUSXM SATELLITE RADIO ENTERTAINMENT (OPTIONAL)
FLIGHT
INSTRUMENTS
NOTE: Refer to the Hazard Avoidance Section for information about SiriusXM Weather products.
The optional SiriusXM Satellite Radio entertainment feature of the GDL 69A Data Link Receiver is available for
the pilot’s and passengers’ enjoyment. The GDL 69A can receive SiriusXM Satellite Radio entertainment services
at any altitude throughout the Continental U.S. Entertainment audio is not available on the GDL 69 Data Link
Receiver.
AUDIO PANEL
& CNS
EIS
SiriusXM Satellite Radio offers a variety of radio programming over long distances without having to constantly
search for new stations. Based on signals from satellites, coverage far exceeds land-based transmissions. SiriusXM Satellite Radio services are subscription-based. For more information on specific service packages, visit
www.siriusxm.com.
ACTIVATING SIRIUSXM SATELLITE RADIO SERVICES
FLIGHT
MANAGEMENT
The service is activated by providing SiriusXM Satellite Radio with either one or two coded IDs, depending on
the equipment. Either the Audio Radio ID or the Data Radio ID, or both, must be provided to SiriusXM Satellite
Radio to activate the entertainment subscription.
It is not required to activate both the entertainment and weather service subscriptions with the GDL 69A. Either or both services can be activated. SiriusXM Satellite Radio uses one or both of the coded IDs to send an
activation signal that, when received by the GDL 69A, allows it to play entertainment programming.
HAZARD
AVOIDANCE
These IDs are located:
• On the label on the back of the Data Link Receiver
• On the XM Information Page on the MFD (Figure 8-74)
• On the XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N
190-00355-04)
AFCS
Contact the installer if the Data Radio ID and the Audio Radio ID cannot be located.
NOTE: The LOCK Softkey on the XM Information Page (Auxiliary Page Group) is used to save GDL 69A
INDEX
APPENDICES
ADDITIONAL
FEATURES
activation data when the SiriusXM services are initially set up. It is not used during normal SiriusXM
Satellite Radio operation, but there should be no adverse effects if inadvertently selected during flight.
Refer to the GDL 69/69A XM Satellite Radio Activation Instructions (190-00355-04, Rev H or later) for
further information.
482
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Activating the SiriusXM Satellite Radio services:
1) Contact SiriusXM Satellite Radio. Follow the instructions provided.
2) Select the Auxiliary Page Group.
FLIGHT
INSTRUMENTS
3) Select the next to last page in the AUX Page Group.
4) Select the INFO Softkey to display the XM Information Page.
5) Verify that the desired services are activated.
6) Select the LOCK Softkey.
EIS
7) Turn the large FMS Knob to highlight YES.
8) To complete activation, press the ENT Key.
AUDIO PANEL
& CNS
Audio
Radio ID
Data
Radio ID
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
Weather
Products
Window
AFCS
Figure 8-74 XM Information Page
APPENDICES
If SiriusXM Weather services have not been activated, all the weather product boxes are cleared on the XM
Information Page and a yellow Activation Required message is displayed in the center of the Weather Data
Link Page (Map Page Group). The Service Class refers to the groupings of weather products available for
subscription.
ADDITIONAL
FEATURES
RADIO
and INFO
Softkeys
LOCK Softkey
Used to Save
Activation Data
During Initial
Setup
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
483
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
USING SIRIUSXM SATELLITE RADIO
FLIGHT
INSTRUMENTS
The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM
Satellite Radio.
Selecting the XM Radio Page:
1) Turn the large FMS Knob to select the Auxiliary Page Group.
2) Turn the small FMS Knob to select the displayed AUX - XM Information Page.
EIS
3) Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Active
Channel
HAZARD
AVOIDANCE
Channel
List
Volume
Field
AFCS
Categories
Field
ADDITIONAL
FEATURES
Figure 8-75 XM Radio Page
ACTIVE CHANNEL AND CHANNEL LIST
APPENDICES
The Active Channel Box on the XM Radio Page displays the currently selected channel that the SiriusXM
Satellite Radio is using.
The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category. Channels can be stepped through one at a time or may be selected directly by channel number.
Selecting a channel from the channel list:
INDEX
1) While on the XM Radio Page, select the CHNL Softkey.
2) Select the CH + Softkey to go up through the list in the Channel Box, or move down the list with the CH – Softkey.
Or:
484
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
1) Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels.
2) Press the ENT Key to activate the selected channel.
Selecting a channel directly:
FLIGHT
INSTRUMENTS
1) While on the XM Radio Page, select the CHNL Softkey.
2) Select the DIR CH Softkey. The channel number in the Active Channel Box is highlighted.
3) Select the numbered softkeys located on the bottom of the display to directly select the desired channel number.
4) Press the ENT Key to activate the selected channel.
EIS
CATEGORY
AUDIO PANEL
& CNS
The Category Box of the XM Radio Page displays the currently selected category of audio. Categories of
channels such as jazz, rock, or news can be selected to list the available channels for a type of music or other
contents. One of the optional categories is PRESETS to view channels that have been programmed.
Selecting a category:
1) Select the CATGRY Softkey on the XM Radio Page.
FLIGHT
MANAGEMENT
2) Select the CAT + and CAT - Softkeys to cycle through the categories.
Or:
Turn the small FMS Knob to display the Categories list. Highlight the desired category with the small FMS Knob
and press the ENT Key. Selecting All Categories places all channels in the list.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
Figure 8-76 Categories List
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
485
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
PRESETS
FLIGHT
INSTRUMENTS
Up to 15 channels from any category can be assigned a preset number. The preset channels are selected by
selecting the PRESETS and MORE Softkeys. Then the preset channel can be selected directly and added to
the channel list for the Presets category.
Setting a preset channel number:
1) On the XM Radio Page, while listening to an Active Channel that is wanted for a preset, select the PRESETS
Softkey to access the first five preset channels (PS1 - PS5).
EIS
2) Select the MORE Softkey to access the next five channels (PS6 – PS10), and again to access the last five
channels (PS11 – PS15). Selecting the MORE Softkey repeatedly cycles through the preset channels.
3) Select any one of the (PS1 - PS15) softkeys to assign a number to the active channel.
AUDIO PANEL
& CNS
4) Select the SET Softkey on the desired channel number to save the channel as a preset.
FLIGHT
MANAGEMENT
Select PRESETS to
Access the Preset
Channels Softkeys
Select MORE to Cycle
Through the Preset
Channels
HAZARD
AVOIDANCE
Select SET
to Save Each
Preset Channel
Figure 8-77 Accessing and Selecting XM Preset Channels
Selecting the BACK Softkey, or waiting during 45 seconds of softkey inactivity, returns the system to the top
level softkeys.
AFCS
VOLUME
Radio volume is shown as a percentage of full volume. Volume level is controlled by selecting the VOL
Softkey, which brings up the MUTE Softkey and the volume increase and decrease softkeys.
ADDITIONAL
FEATURES
Adjusting the volume:
1) With the XM Radio Page displayed, select the VOL Softkey.
APPENDICES
2) Select the VOL – Softkey to reduce volume or select the VOL + Softkey to increase volume. (Once the VOL
Softkey is selected, the volume can also be adjusted using the small FMS Knob.)
INDEX
3) Select the MUTE Softkey to mute the audio. Select the MUTE Softkey again to unmute the audio.
Figure 8-78 Volume Control
486
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
8.7 SCHEDULER
FLIGHT
INSTRUMENTS
The Scheduler feature can be used to enter and display reminder messages (e.g., Change oil, Switch fuel tanks,
or Altimeter-Transponder Check) in the Alerts Window on the PFD. Messages can be set to display based on
a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently
whenever the message timer reaches zero (periodic). Message timers set to periodic alerting automatically reset
to the original timer value once the message is displayed. When power is cycled, all messages are retained until
deleted, and message timer countdown is resumed.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 8-79 Scheduler (Utility Page)
HAZARD
AVOIDANCE
Entering a scheduler message:
1) Select the AUX - Utility Page.
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the first empty scheduler message naming field.
AFCS
4) Use the FMS Knob to enter the message text to be displayed in the Alerts Window and press the ENT Key.
5) Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type.
6) Turn the small FMS Knob to select the message type:
ADDITIONAL
FEATURES
• Event—Message issued at the specified date/time
• One-time—Message issued when the message timer reaches zero (default setting)
• Periodic—Message issued each time the message timer reaches zero
7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field.
APPENDICES
8) For periodic and one-time message, use the FMS Knob to enter the timer value (HH:MM:SS) from which to
countdown and press the ENT Key.
9) For event-based messages:
a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key.
INDEX
b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field.
c) Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key.
10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
487
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
Deleting a scheduler message:
1) Select the AUX - Utility Page.
FLIGHT
INSTRUMENTS
2) Press the FMS Knob momentarily to activate the flashing cursor.
3) Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted.
4) Press the CLR Key to clear the message text. If the CLR Key is pressed again, the message is restored.
5) Press the ENT Key while the message line is cleared to clear the message text.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Scheduler messages appear in the Messages Window on the PFD. When a scheduler message is waiting, the
ALERTS Softkey label changes to ADVISORY. Selecting the ADVISORY Softkey opens the Messages Window
and acknowledges the scheduler message. The softkey label reverts to ALERTS when selected. Selecting the
ALERTS Softkey again removes the Messages Window from the display, and the scheduler message is deleted
from the message queue.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Figure 8-80 PFD Messages Window
488
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
8.8 ELECTRONIC CHECKLISTS (OPTIONAL)
NOTE: The checklists presented in this section are for example only and may not reflect checklists actually
FLIGHT
INSTRUMENTS
available for the Cessna Corvalis/Corvalis TT. The information described in this section is not intended
to replace the checklist information described in the AFM or the Pilot Safety and Warning Supplements
document.
NOTE: Garmin is not responsible for the content of checklists. User-defined checklists are created by the
EIS
aircraft manufacturer. Modifications or updates to the checklists are coordinated through the aircraft
manufacturer. The user cannot edit these checklists.
The optional checklist functions are displayed on two levels of softkeys that are available on any MFD page.
MAP
DCLTR
SHW CHRT CHKLIST
CHECK
EXIT
EMERGCY
FLIGHT
MANAGEMENT
SYSTEM
AUDIO PANEL
& CNS
(Optional)
SYSTEM
The CHECK Softkey label changes to UNCHECK
when the checklist item is already checked.
Figure 8-81 Checklist Softkeys
HAZARD
AVOIDANCE
The MFD is able to display optional electronic checklists which allow a pilot to quickly find the proper
procedure on the ground and during each phase of flight. The system accesses the checklists from an SD card
inserted into the bezel slot. If the SD card contains an invalid checklist file or no checklist, the Power-up Page
messages display ‘Checklist File: Invalid’ or ‘Checklist File: N/A’ (not available) and the CHKLIST Softkey is
not available.
AFCS
Accessing and navigating checklists:
1) From any page on the MFD, select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page.
2) Turn the large FMS Knob to select the ‘GROUP’ field.
ADDITIONAL
FEATURES
3) Turn the small FMS Knob to select the desired procedure and press the ENT Key.
4) Turn the large FMS Knob to select the ‘CHECKLIST’ field.
APPENDICES
5) Turn the FMS Knob to select the desired checklist and press the ENT Key. The selected checklist item is
indicated with white text surrounded by a white box.
6) Press the ENT Key or select the CHECK Softkey to check the selected checklist item. The line item turns green
and a checkmark is placed in the associated box. The next line item is automatically selected for checking.
Either FMS Knob can be used to scroll through the checklist and select the desired checklist item.
Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item.
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
489
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
7) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left
of the checklist window. If all items in the checklist have not be checked, ‘*CHECKLIST NOT FINISHED*’ will be
displayed in yellow text.\
FLIGHT
INSTRUMENTS
8) Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor.
9) Press the ENT Key to advance to the next checklist.
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
10) Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed.
INDEX
APPENDICES
ADDITIONAL
FEATURES
Figure 8-82 Sample Checklist
490
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
Accessing emergency procedures:
1) From any page on the MFD, select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page.
2) Select the EMERGCY Softkey.
FLIGHT
INSTRUMENTS
3) Turn the FMS Knob to select the desired emergency checklist and press the ENT Key.
4) Press the ENT Key or select the CHECK Softkey to check the selected emergency checklist item. The line item
turns green and a checkmark is placed in the box next to it. The next line item is automatically highlighted for
checking.
Either FMS Knob can be used to scroll through the checklist and select the desired checklist item.
EIS
Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item.
AUDIO PANEL
& CNS
5) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left
of the checklist window. If all items in the checklist have not be checked, ‘*CHECKLIST NOT FINISHED*’ will be
displayed in yellow text.\
6) Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor.
7) Press the ENT Key to advance to the next checklist.
FLIGHT
MANAGEMENT
8) Select the RETURN Softkey to return to the previous checklist.
9) Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed.
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Figure 8-83 Emergency Checklist Page Example
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
491
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
8.9 FLIGHT DATA LOGGING
NOTE: Some aircraft installations may not provide all aircraft/engine data capable of being logged by the
FLIGHT
INSTRUMENTS
system.
The Flight Data Logging feature will automatically store critical flight and engine data on an SD data card (up
to 16GB) inserted into the top card slot of the MFD. Approximately 1,000 flight hours can be recorded for each
1GB of available space on the card.
EIS
Data is written to the SD card once each second while the MFD is powered on. All flight data logged on a
specific date is stored in a file named in a format which includes the date, time, and nearest airport identifier. The
file is created automatically each time the G1000 system is powered on, provided an SD card has been inserted.
AUDIO PANEL
& CNS
The status of the Flight Data Logging feature can be viewed on the AUX-UTILITY Page. If no SD card has been
inserted, “NO CARD” is displayed. When data is being written to the SD card, “LOGGING DATA” is displayed.
The .csv file may be viewed with Microsoft Excel® or other spreadsheet applications.
FLIGHT
MANAGEMENT
The following is a list of data parameters the G1000 system is capable of logging for the Cessna Corvalis/
Corvalis TT aircraft.
• GPS fix
• Time
• Longitude (degrees; geodetic;
+East)
• GPS altitude (GSL)
• Magnetic Heading (degrees)
• GPS vertical alert limit
• GPS altitude (WGS84 datum)
• HSI source
• Baro-Corrected altitude (feet)
• Selected course
• SBAS GPS horizontal protection
level
• Baro Correction (in/Hg)
• Com1/Com2 frequency
• Indicated airspeed (kts)
• Nav1/Nav2 frequency
• SBAS GPS vertical protection
level
• Vertical speed (fpm)
• CDI deflection
• Fuel Qty (right & left)(gals)
• GPS vertical speed (fpm)
• VDI/GP/GS deflection
• Fuel Flow (gph)
• OAT (degrees C)
• Wind Direction (degrees)
• Fuel Pressure (psi)
• True airspeed (knots)
• Wind Speed (knots)
• Voltage 1 and/or 2
• Pitch Attitude Angle (degrees)
• Active Waypoint Identifier
• Amps 1 and/or 2
• Roll Attitude Angle (degrees)
• Distance to next waypoint (nm)
• Engine RPM
• Lateral and Vertical G Force (g)
• Bearing to next waypoint
(degrees)
• Oil Pressure (psi)
• Magnetic variation (degrees)
• TIT (deg. F)
• Autopilot On/Off
• Manifold Pressure (in. Hg)
• AFCS roll/pitch modes
• CHT
• AFCS roll/pitch commands
• EGT
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
• Date
• Ground Speed (kts)
• Ground Track (degrees
magnetic)
INDEX
• Latitude (degrees; geodetic;
+North)
492
• GPS horizontal alert limit
• Oil Temperature (deg. F)
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
The file containing the recorded data will appear in the format shown in Figure 8-84. This file can be imported
into most computer spreadsheet applications.
Local 24hr Time
HHMMSS
FLIGHT
INSTRUMENTS
Local Date
YYMMDD
Nearest Airport
(A blank will be
inserted if no
airport is found)
log_120210_104506_KIXD.csv
EIS
Figure 8-84 Log File Format
AUDIO PANEL
& CNS
Data logging status can be monitored on the AUX-UTILITY Page.
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
493
SYSTEM
OVERVIEW
8.10 AUXILIARY VIDEO (OPTIONAL)
FLIGHT
INSTRUMENTS
ADDITIONAL FEATURES
There are four modes of operation of the auxiliary video display: Full-Screen, Full-Screen with Digital Zoom,
Split-Screen with Map, and Split-Screen with Map and Digital Zoom.
The G1000 system provides a control and display interface to an optional auxiliary video system. The system
can display video for up to two inputs.
Displaying auxiliary video:
1) Turn the large FMS Knob to select the AUX page group.
EIS
2) Turn the small FMS Knob to select VIDEO and display the AUX-VIDEO Page.
AUDIO PANEL
& CNS
ENGINE
FLIGHT
MANAGEMENT
The video display softkeys shown below appear on the AUX - VIDEO Page.
MAP
CNTRST -
INPUT
SETUP
VID ZM+
VID ZM-
MAP ACTV HIDE MAP
VID ACTV
CNTRST +
BRIGHT -
BRIGHT +
SAT -
SAT +
RESET
BACK
Pressing the BACK Softkey returns
to the Previous Level Softkeys.
HAZARD
AVOIDANCE
Figure 8-85 Video Display Softkeys
APPENDICES
ADDITIONAL
FEATURES
AFCS
Control of the AUX - VIDEO Page can also be accessed through the Page Menu.
Figure 8-86 AUX - VIDEO Page Menu
Selecting video menu options:
INDEX
1) While viewing the AUX - VIDEO Page press the MENU Key to display the Page Menu OPTIONS.
2) Turn the large FMS Knob to highlight the desired video adjustment option and press the ENT Key.
Once the ENT key is pressed on any option, the page menu closes and returns to the AUX - VIDEO Page.
494
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
VIDEO SETUP
FLIGHT
INSTRUMENTS
Video brightness, contrast, and saturation may be adjusted be selecting the setup function. While viewing
the setup function softkeys, after 45 seconds of softkey inactivity, the system reverts to the AUX - VIDEO Page
softkeys.
Adjusting the video settings:
1) With the AUX-VIDEO Page displayed, select the SETUP Softkey.
2) Select the BRIGHT - or BRIGHT +, to adjust display brightness in five percent increments from 0 to 100%.
EIS
3) Select the CNTRST- or CNTRST +, to adjust display contrast in five percent increments from 0 to 100%.
4) Select the SAT - or SAT +, to adjust display saturationin five percent increments from 0 to 100%.
5) If desired, return the display to the default settings by selecting the RESET Softkey.
AUDIO PANEL
& CNS
6) Select the BACK Softkey to return to the previous softkey level.
DISPLAY SELECTION
FLIGHT
MANAGEMENT
Selecting the HIDE MAP Softkey removes the map and displays video on the full screen. The softkey label
changes to grey with black characters. Selecting the HIDE MAP Softkey again restores the map view and the
small video image. The softkey label returns to white characters on a black background.
HAZARD
AVOIDANCE
Video
Display
AFCS
ADDITIONAL
FEATURES
Map
View
APPENDICES
Figure 8-87 AUX - Video Split-Screen
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
495
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
Figure 8-88 Full Screen Video Display
HAZARD
AVOIDANCE
INPUT SELECTION
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
While on the AUX - VIDEO Page, select the INPUT Softkey to select the EVS or AUX video source.
496
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
ZOOM/RANGE
Selecting the VID ZM + or VID ZM - Softkeys increases or decreases video display magnification between
1x and 10x.
FLIGHT
INSTRUMENTS
The RANGE Knob can be used to increase or decrease the range setting on the map display or zoom in and
out on the video display. While in the Split-Screen mode, selecting the MAP ACTV or VID ACTV Softkey
determines which display the RANGE Knob adjusts. Selecting the softkey to display MAP ACTV allows the
RANGE Knob to control the range setting of the map display. Selecting the softkey to display VID ACTV allows
the RANGE Knob to control the zoom setting of the video display.
EIS
When zooming in on the video display, a Zoom Window will appear in the upper right of the display. A box
within this window indicates the portion of the display currently being viewed. The currently displayed portion
of the full display may be adjusted by using Joystick.
AUDIO PANEL
& CNS
Zoom
Window
FLIGHT
MANAGEMENT
Current
View
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
Figure 8-89 Zoom Window
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
497
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
8.11 ABNORMAL OPERATION
FLIGHT
INSTRUMENTS
SVS TROUBLESHOOTING
SVS is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVS is
disabled when valid attitude or heading data is not available for the display. In case of invalid SVS data, the PFD
display reverts to the standard blue-over-brown attitude display.
SVS becomes disabled without the following data resources:
EIS
• Attitude data
• Heading data
• GPS position data
AUDIO PANEL
& CNS
• 9 Arc-second Terrain data
• Obstacle data
• TAWS function is not available, in test mode, or failed
FLIGHT
MANAGEMENT
• The position of the aircraft exceeds the range of the terrain database.
REVERSIONARY MODE
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
SVS can be displayed on the Multifunction Display (MFD) in Reversionary Mode. If it is enabled when switching
to Reversionary Mode, SVS will take up to 30 seconds to be displayed. The standard, non-SVS PFD display will
be shown in the interim.
Figure 8-90 SVS Reversionary Mode
498
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
UNUSUAL ATTITUDES
FLIGHT
INSTRUMENTS
Unusual attitudes are displayed with red chevrons overlaid on the display indicating the direction to fly to
correct the unusual attitude condition. The display shows either a brown or blue colored bar at the top or
bottom of the screen to represent earth or sky. This is intended to prevent losing sight of the horizon during
extreme pitch attitudes.
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
Figure 8-91 Unusual Attitude Display
The blue colored bar is also displayed when terrain gradient is great enough to completely fill the display.
HAZARD
AVOIDANCE
Blue Band
AFCS
Terrain
Completely
Fills Display
ADDITIONAL
FEATURES
Figure 8-92 Blue Sky Bar with Full Display Terrain
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
499
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
GDL 69/69A DATA LINK RECEIVER TROUBLESHOOTING
Some quick troubleshooting steps listed below can be performed to find the possible cause of a failure.
FLIGHT
INSTRUMENTS
• Ensure the owner/operator of the aircraft in which the Data Link Receiver is installed has subscribed to
SiriusXM Satellite Radio services
• Ensure the SiriusXM subscription has been activated
• Perform a quick check of the circuit breakers to ensure that power is applied to the Data Link Receiver
EIS
For troubleshooting purposes, check the LRU Information Box on the AUX - System Status Page for Data Link
Receiver (GDL 69/69A) status, serial number, and software version number. If a failure has been detected in the
GDL 69/69A the status is marked with a red X.
Selecting the System Status Page:
AUDIO PANEL
& CNS
1) Turn the large FMS Knob to select the AUX Page Group.
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
2) Turn the small FMS Knob to select the System Status Page (the last page in the AUX Page Group).
INDEX
Figure 8-93 LRU Information Window on System Status Page
500
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
ADDITIONAL FEATURES
SYSTEM
OVERVIEW
If a failure still exists, the following messages may provide insight as to the possible problem:
NO SIGNAL
LOADING
OFF AIR
---
Message Location
XM Radio Page - active channel field
XM Radio Page - active channel field
XM Radio Page - active channel field
Weather Datalink Page - center of page
XM Radio Page - active channel field
XM Radio Page - active channel field
XM Radio Page - active channel field
Description
Data Link Receiver antenna error; service required
Data Link Receiver updating encryption code
FLIGHT
INSTRUMENTS
Message
CHECK ANTENNA
UPDATING
Loss of signal; signal strength too low for receiver
EIS
Acquiring channel audio or information
Channel not in service
Missing channel information
No communication from Data Link Receiver
WEATHER DATA LINK FAILURE Weather Datalink Page - center of page
within last 5 minutes
ACTIVATION REQUIRED
Weather Datalink Page - center of page SiriusXM subscription is not activated
AUDIO PANEL
& CNS
Table 8-5 GDL 69/69A Data Link Receiver Error Messages
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
501
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
ADDITIONAL FEATURES
Blank Page
502
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
ANNUNCIATIONS AND ALERTS
NOTE: The Airplane Flight Manual (AFM) supersedes information found in this document.
FLIGHT
INSTRUMENTS
The G1000 Alerting System conveys alerts to the pilot using the following items:
EIS
• Annunciation Window: The Annunciation Window displays abbreviated annunciation text. Text color is
based on alert levels described in the Alert Levels Definition section. The Annunciation Window is located to the
right of the Altimeter and Vertical Speed Indicator. All aircraft annunciations can be displayed simultaneously
in the Annunciation Window. A white horizontal line separates annunciations that are acknowledged from
annunciations that are not yet acknowledged. Higher priority annunciations are displayed towards the top of
the window.
AUDIO PANEL
& CNS
• Alerts Window: The Alerts Window displays text messages for up to 64 prioritized alert messages. Selecting
the ALERTS Softkey displays the Alerts Window. Selecting the ALERTS Softkey a second time removes the
Alerts Window from the display. When the Alerts Window is displayed, the pilot can use the large FMS Knob
can be used to scroll through the alert message list.
FLIGHT
MANAGEMENT
• Softkey Annunciation: During certain alerts, the ALERTS Softkey may appear as a flashing annunciation
to accompany an alert. The ALERTS Softkey assumes a new label consistent with the alert level (WARNING,
CAUTION, or ADVISORY). By selecting the softkey when flashing an annunciation, the alert is acknowledged.
The softkey label then returns to previous ALERTS. If alerts are still present, the ALERTS label is displayed in
white with black text. The pilot can select the ALERTS Softkey a second time views the alert text messages.
• System Annunciations: Typically, a large red ‘X’ appears in windows when a failure is detected in the LRU providing
the information to the window. See the G1000 System Annunciations section for more information.
HAZARD
AVOIDANCE
• Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met.
See the Alert Levels Definitions section for more information.
AFCS
ADDITIONAL
FEATURES
System
Annunciation
(Red ‘X’)
Alerts
Window
APPENDICES
Annunciation
Window
INDEX
Softkey
Annunciation
Figure A-1 G1000 Alerting System
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
503
SYSTEM
OVERVIEW
APPENDIX A
ALERT LEVEL DEFINITIONS
The G1000 Alerting System, as installed in Cessna Corvalis/Corvalis TT aircraft, uses three alert levels.
FLIGHT
INSTRUMENTS
• WARNING: This level of alert requires immediate pilot attention. A warning alert is annunciated in the
Annunciation Window and is accompanied by a continuous aural chime. Text appearing in the Annunciation
Window is RED. A warning alert is also accompanied by a flashing WARNING Softkey annunciation, as
shown in Figure A-2. Selecting the WARNING Softkey acknowledges the presence of the warning alert and
stops the aural chime.
AUDIO PANEL
& CNS
EIS
• CAUTION: This level of alert indicates the existence of abnormal conditions on the aircraft that may require
pilot intervention. A caution alert is annunciated in the Annunciation Window and is accompanied by
a single aural chime. Text appearing in the Annunciation Window is YELLOW. A caution alert is also
accompanied by a flashing CAUTION Softkey annunciation, as shown in Figure A-2. Selecting the CAUTION
Softkey acknowledges the presence of the caution alert.
FLIGHT
MANAGEMENT
• MESSAGE ADVISORY: This level of alert provides general information to the pilot. A message advisory
alert does not issue annunciations in the Annunciation Window. Instead, message advisory alerts only
issue a flashing ADVISORY Softkey annunciation, as shown in Figure A-2. Pressing the ADVISORY Softkey
acknowledges the presence of the message advisory alert and displays the alert text message in the Alerts
Window, and the softkey label changes to ALERTS.
HAZARD
AVOIDANCE
Figure A-2 Softkey Annunciation (ALERTS Softkey Labels)
• Audio Alerting System: The System issues audio alert tones when specific system conditions are met. See
the Alert Level Definitions Section for more information. The annunciation tone may be tested from the
AUX - System Status Page.
AFCS
Testing the system annunciation tone:
1) Use the FMS Knob to select the AUX - System Status Page.
2) Select the ANN TEST Softkey.
ADDITIONAL
FEATURES
Or:
a) Press the MENU Key.
b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key.
APPENDICES
Selecting the audio alert voice:
1) Use the FMS Knob to select the AUX - System Setup Page.
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the voice in the Audio Alert Box.
INDEX
4) Turn the small FMS Knob to select the desired voice, press the ENT Key.
504
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Figure A-3 Audio Alert
(AUX - System Status Page)
FLIGHT
MANAGEMENT
The status of detected LRUs can be checked on the AUX - System Status Page. Active LRUs are indicated
by green check marks; failed, by red ‘X’s. Failed LRUs should be noted and a service center or Garminauthorized dealer informed.
Viewing LRU information:
HAZARD
AVOIDANCE
1) Use the FMS Knob to select the AUX - System Status Page.
2) To place the cursor in the ‘LRU Info’ Box,
a) Select the LRU Softkey.
Or:
a) Press the MENU Key.
AFCS
b) With ‘Select LRU Window’ highlighted, press the ENT Key.
3) Use the FMS Knob to scroll through the box to view LRU status information.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
505
SYSTEM
OVERVIEW
APPENDIX A
AIRCRAFT ALERTS
FLIGHT
INSTRUMENTS
The following alerts are configured specifically for the Cessna Corvalis/Corvalis TT. Red annunciation window
text signifies warnings and yellow, cautions, and white, annunciation advisories. See the Airplane Flight Manual
(AFM) for recommended pilot actions.
Alerts Window Message
Audio Alert/Voice Message
Door not secured
Chime/”Door Open”
Fuel tank is not correctly selected
Chime/”Fuel Valve”
No power on the left bus
Chime/None
No power on the right bus
Chime/None
Carbon Monoxide level is too high
Chime/”Carbon Monoxide”
Low oil pressure
Chime/”Oil Pressure Low”
Left Alternator offline
Single Chime/”Left Alternator Out”
Right Alternator offline
Single Chime/”Right Alternator Out”
Fuel pressure low or backup pump is on
Single Chime/”Fuel Pump”
Low fuel in the left tank
Single Chime/None
Low fuel in the right tank
Single Chime/None
Rudder limiter is engaged
Single Chime/None
Starter relay has power applied
Single Chime/None
Pressure above 12,000 ft and oxygen off
Single Chime/None
Oxygen outlet pressure below 60 psi
Single Chime/None
Oxygen outlet pressure below 16.5 psi
Single Chime/None
Oxygen quantity below 250 psi.
Single Chime/None
Reminder: Turn off oxygen
None
Speed brakes are active
None
Rudder Hold is engaged
None
AP/TRIM master switch is in the OFF
None
PFD FAN FAIL – Cooling fan for the PFD is
None
inoperative.
None
MFD FAN FAIL – Cooling fan for the MFD is
None
inoperative.
None
AVIONICS FAN – Cooling fan for remote avionics is
None
inoperative.
None
TIMER ZERO – Timer has counted down to zero.
“Timer Expired”
None
FUEL IMBAL – Fuel imbalance is greater than 10
None
gallons.
None
LOW MAN PRES – Manifold pressure is below 15 in.
None
None
VAPOR SUPPR** – Turn on Vapor Suppression.
None
*Corvalis only / **Corvalis TT only / High pressure oxygen outlet only / †Low pressure oxygen outlet only
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Annunciation Window Text
DOOR OPEN
FUEL VALVE
L BUS OFF
R BUS OFF
CO LVL HIGH
OIL PRES LOW
L ALT OUT
R ALT OUT
FUEL PUMP
L LOW FUEL
R LOW FUEL
RUDR LMTR*
STARTER ENGD
OXYGEN
OXYGEN PRES
OXYGEN PRES†
OXYGEN QTY
OXYGEN ON
SPEED BRAKES
RUDR HOLD**
AP/TRIM OFF
None
506
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
CO GUARDIAN MESSAGES
Comments
There is a problem within the CO Guardian that requires services.
FLIGHT
INSTRUMENTS
Alerts Window Message
CO DET SRVC – The carbon monoxide
detector needs service.
CO DET FAIL – The carbon monoxide
detector is inoperative.
Loss of communication between the G1000 and the CO Guardian.
EIS
G1000 SYSTEM ANNUNCIATIONS
AUDIO PANEL
& CNS
When a new alert is issued, the ADVISORY Softkey flashes to alert the pilot of a new message. It continues to
flash until acknowledged by pressing the ADVISORY Softkey. When the softkey is pressed, the softkey name
changes to ALERTS and the Alerts Window is displayed. Active alerts are displayed in white text. Alerts that
become inactive while the Alerts Window is displayed change to gray text. The ADVISORY Softkey flashes if a
new alert is issued. Press the ALERTS Softkey to remove the Alerts Window. This also removes inactive alerts
from the Alerts Window the next time the window is shown.
FLIGHT
MANAGEMENT
The G1000 System Messages convey messages to the pilot regarding problems with the G1000 system. When
an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with the failed data.
The following section describes various system annunciations. Refer to the Airplane Flight Manual (AFM) for
additional information regarding pilot responses to these annunciations.
HAZARD
AVOIDANCE
NOTE: Upon power-up of the G1000 system, certain windows remain invalid as the equipment begins to
initialize. All windows should be operational within one minute of power-up. If any window continues to
remain flagged, the G1000 system should be serviced by a Garmin-authorized repair facility.
GEA 71 Engine
Airframe Unit
Or
GIA 63/63W
Integrated
Avionics Unit
Database
Mismatch in
PFD and MFD
ADDITIONAL
FEATURES
GIA 63/63W
Integrated
Avionics Units
GDC 74A
Air Data
Computer
AFCS
GIA 63/63W
Integrated
Avionics Units
APPENDICES
GRS 77 AHRS
Or
GMU 44
Magnetometer
GDC 74A Air
Data Computer
.
190-00552-05 Rev. A
INDEX
GIA 63/63W
Integrated
Avionics Units
GTX 33 Transponder Or
GIA 63/63W Integrated
Avionics Units
Figure A-4 System Failure Annunciations
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
507
SYSTEM
OVERVIEW
APPENDIX A
System Annunciation
Comment
System Annunciation
FLIGHT
INSTRUMENTS
Attitude and Heading
Reference System is aligning.
Display system is not receiving
airspeed input from air data
computer.
AUDIO PANEL
& CNS
EIS
Display system is not receiving
attitude information from the
AHRS.
Display system is not receiving
vertical speed input from the
air data computer.
FLIGHT
MANAGEMENT
AHRS calibration incomplete or
configuration module failure.
Display system is not receiving
valid heading input from AHRS.
AFCS
HAZARD
AVOIDANCE
This annunciation is seen only
when the autopilot is engaged.
The annunciation indicates an
AHRS monitor has detected
an abnormal flight parameter,
possibly caused by strong
turbulence. In this case, the
situation should correct itself
within a few seconds. If there
is an actual failure, a red “X”
soon appears over the Attitude
Indicator.
APPENDICES
ADDITIONAL
FEATURES
‘LOI’ Indicates Loss of Integrity
of GPS information. GPS
information is either not
present or is invalid for
navigation use. Note that
AHRS utilizes GPS inputs
during normal operation.
AHRS operation may be
degraded if GPS signals are not
present (see AFM).
INDEX
Display system is not receiving
valid ISA information from air
data computer.
508
Comment
Display system is not receiving
altitude input from the air data
computer.
Other Various Red X
Indications
Different versions of GDU
software are installed in the
PFD and MFD. This can also
indicate different versions
of the navigation database
installed in the PFD and MFD.
In some circumstances, a
cross-talk error between the
PFD and MFD can cause this
annunciation.
Display system is not receiving
valid OAT information from air
data computer.
Display system is not receiving
valid transponder information.
A red ‘X’ through any other
display field (such as engine
instrumentation fields)
indicates that the field is not
receiving valid data.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
OTHER VOICE ALERTS
Alert Trigger
Issued when the aircraft transitions through the minimum descent altitude/decision height (MDA/DH)
Aircraft is one minute from Top of Descent - issued only when vertical navigation is enabled
TIS voice alert - issued when a Traffic Advisory (TA) is issued
TIS voice alert - issued when the TIS traffic system fails or cannot communicate
EIS
Voice Alert
“Minimums, Minimums”
“Vertical Track”
“Traffic”
“TIS Not Available”
FLIGHT
INSTRUMENTS
The following audio alerts are announced by the system using a voice of male or female gender as selected
on the AUX - System Setup Page on the MFD. If the optional Terrain-SVS or Terrain Awareness and Warning
System is installed, terrain voice alerts are also generated (refer to the Terrain-SVS and TAWS alerts section).
AUDIO PANEL
& CNS
NOTE: Voice alerts are provided to the G1000 by GIA 63/W #1. Should this unit fail, audio and voice alerts are no
longer available.
G1000 SYSTEM MESSAGE ADVISORIES
FLIGHT
MANAGEMENT
NOTE: This Section provides information regarding G1000 message advisories that may be displayed by
the system. Knowledge of the aircraft, systems, flight conditions, and other existing operational priorities
must be considered when responding to a message. Always use sound pilot judgment. The Airplane Flight
Manual (AFM) takes precedence over any conflicting guidance found in this section.
HAZARD
AVOIDANCE
This section describes various G1000 System message advisories. Certain messages are issued due to an LRU
or LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as
shown previously in the G1000 System Annunciations section.
GDU 104X PRIMARY FLIGHT DISPLAY & MULTI FUNCTION DISPLAY MESSAGE ADVISORIES
ADDITIONAL
FEATURES
The PFD and/or MFD self-test has detected a problem. The G1000 system should be
serviced.
APPENDICES
The PFD and/or MFD has incorrect software installed. The G1000 system should be
serviced.
The PFD configuration settings do not match backup configuration memory. The
G1000 system should be serviced.
The MFD configuration settings do not match backup configuration memory. The
G1000 system should be serviced.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
190-00552-05 Rev. A
Comments
The pilot profile data was lost. System reverts to default pilot profile and settings. The
pilot may reconfigure the MFD & PFD with preferred settings, if desired.
The MFD and PFD are not communicating with each other. The G1000 system should
be serviced.
AFCS
Message
DATA LOST – Pilot stored data was
lost. Recheck settings.
XTALK ERROR – A flight display
crosstalk error has occurred.
PFD1 SERVICE – PFD1 needs service.
Return unit for repair.
MFD1 SERVICE – MFD1 needs
service. Return unit for repair.
MANIFEST – PFD1 software
mismatch, communication halted.
MANIFEST – MFD1 software
mismatch, communication halted.
PFD1 CONFIG – PFD1 configuration
error. Config service req’d.
MFD1 CONFIG – MFD1 configuration
error. Config service req’d.
509
SYSTEM
OVERVIEW
APPENDIX A
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Message
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 KEYSTK – PFD1 [keyname] Key
is stuck.
MFD1 KEYSTK – MFD [keyname] Key
is stuck.
CNFG MODULE – PFD1 configuration
module is inoperative.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage.
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage.
Comments
The MFD and PFD have different software versions installed. The G1000 system
should be serviced.
The PFD and/or MFD is overheating and is reducing power consumption by dimming
the display. If problem persists, the G1000 system should be serviced.
A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing
it several times. The G1000 system should be serviced if the problem persists.
The PFD1 configuration module backup memory has failed. The G1000 system should
be serviced.
The PFD1 voltage is low. The G1000 system should be serviced.
The MFD voltage is low. The G1000 system should be serviced.
DATABASE MESSAGE ADVISORIES
Comments
The MFD and/or PFD detected a failure in the navigation database. Attempt to reload
the navigation database. If problem persists, the system should be serviced.
The MFD and/or PFD detected a failure in the basemap database.
The MFD and/or PFD detected a failure in the terrain database. Ensure that the
terrain card is properly inserted in display. Replace terrain card. If problem persists,
the system should be serviced.
The terrain database is present on another LRU, but is missing on the specified LRU.
The MFD and/or PFD detected a failure in the obstacle database. Ensure that the data
card is properly inserted. Replace data card. If problem persists, the system should be
serviced.
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
Message
MFD1 DB ERR – MFD1 navigation
database error exists.
PFD1 DB ERR – PFD1 navigation
database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
510
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
The MFD and/or PFD detected a failure in the airport terrain database. Ensure that
the data card is properly inserted. Replace data card. If problem persists, the system
should be serviced.
The airport terrain database is present on another LRU, but is missing on the specified
LRU.
AUDIO PANEL
& CNS
The MFD and/or PFD detected a failure in the Safe Taxi database. Ensure that the
data card is properly inserted. Replace data card. If problem persists, the system
should be serviced.
FLIGHT
MANAGEMENT
The PFD and/or MFD detected a failure in the Airport Directory database. Ensure the
data card is properly inserted. Replace data card. If problem persists, the system should
be serviced.
The MFD detected a failure in the FliteCharts database (optional feature). Ensure
the data card is properly inserted. Replace data card. If problem persists, the system
should be serviced.
The MFD detected a failure in the ChartView database (optional feature). Ensure the
data card is properly inserted. Replace data card. If the problem persists, the system
should be serviced.
HAZARD
AVOIDANCE
AFCS
The MFD and/or PFD detected a failure in more than one database. If problem
persists, the system should be serviced.
ADDITIONAL
FEATURES
MFD1 DB ERR – MFD1 multiple
database errors exists.
PFD1 DB ERR – PFD1 multiple
database errors exists.
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
The obstacle database is present on another LRU, but is missing on the specified LRU.
EIS
MFD1 DB ERR – MFD1 Chartview
database error exists.
Comments
FLIGHT
INSTRUMENTS
MFD1 DB ERR – MFD1 FliteCharts
database error exists.
SYSTEM
OVERVIEW
Message
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
MFD1 DB ERR – MFD1 airport terrain
database error exists.
PFD1 DB ERR – PFD1 airport terrain
database error exists.
MFD1 DB ERR – MFD1 airport terrain
database missing.
PFD1 DB ERR – PFD1 airport terrain
database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Airport
Directory database error exists.
MFD1 DB ERR – MFD1 Airport
Directory database error exists.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
190-00552-05 Rev. A
APPENDICES
The PFD and MFD have different navigation database versions or regions installed.
Crossfill is off. Check the AUX-SYSTEM STATUS Page to determine versions or regions.
Also, check the AUX-SYSTEM STATUS Page for a database synchronization function
not completed. After synchronization is complete, power must be turned off, then on.
DB MISMATCH – Standby Navigation The PFD and MFD have different standby navigation database versions or regions
database mismatch.
installed. Check the AUX-SYSTEM STATUS Page to determine versions or regions.
Also, check the AUX-SYSTEM STATUS Page for a database synchronization function
not completed. After synchronization is complete, power must be turned off, then on.
DB MISMATCH – Terrain database
The PFD and MFD have different terrain database versions or regions installed. Check
mismatch.
the AUX-SYSTEM STATUS Page to determine versions or regions. Also, check the AUXSYSTEM STATUS Page for a database synchronization function not completed. After
synchronization is complete, power must be turned off, then on.
511
SYSTEM
OVERVIEW
APPENDIX A
Comments
The PFD and MFD have different obstacle database versions or regions installed.
Check the AUX-SYSTEM STATUS Page to determine versions or regions. Also,
check the AUX-SYSTEM STATUS Page for a database synchronization function not
completed. After synchronization is complete, power must be turned off, then on.
DB MISMATCH – Airport Terrain
The PFD and MFD have different airport terrain database versions or regions installed.
database mismatch.
Check the AUX-SYSTEM STATUS Page to determine versions or regions. Also,
check the AUX-SYSTEM STATUS Page for a database synchronization function not
completed. After synchronization is complete, power must be turned off, then on.
NAV DB UPDATED – Active
System has updated the active navigation database from the standby navigation
navigation database updated.
database.
TERRAIN DSP – [PFD1 or MFD1]
One of the terrain, airport terrain, or obstacle databases required for TAWS in the PFD
Terrain awareness display unavailable. or MFD is missing or invalid.
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Message
DB MISMATCH – Obstacle database
mismatch.
GIA 63 INTEGRATED AVIONICS UNIT MESSAGE ADVISORIES
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
MANIFEST – GFC software mismatch,
communication halted.
MANIFEST – GIA1 software
mismatch, communication halted.
MANIFEST – GIA2 software
mismatch, communication halted.
512
Comments
The GIA1 and/or GIA2 configuration settings do not match backup configuration
memory. The G1000 system should be serviced.
The GIA1 and/or GIA2 have an error in the audio configuration. The G1000 system
should be serviced.
The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to
warm up to operating temperature.
The GIA1 and/or GIA2 temperature is too high. If problem persists, the G1000 system
should be serviced.
The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system
should be serviced.
Incorrect servo software is installed, or gain settings are incorrect.
The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should be
serviced.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
COM1 and/or COM2 software mismatch. The G1000 system should be serviced.
FLIGHT
INSTRUMENTS
NAV1 and/or NAV2 software mismatch. The G1000 system should be serviced.
The system has detected an over temperature condition in COM1 and/or COM2. The
transmitter will operate at reduced power. If the problem persists, the G1000 system
should be serviced.
EIS
AUDIO PANEL
& CNS
The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may
still be usable. The G1000 system should be serviced when possible.
The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or
“pressed”) position. Press the PTT switch again to cycle its operation.
If the problem persists, the G1000 system should be serviced.
FLIGHT
MANAGEMENT
The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”)
position. Press the transfer switch again to cycle its operation. If the problem
persists, the G1000 system should be serviced.
HAZARD
AVOIDANCE
COM1 and/or COM2 configuration settings do not match backup configuration
memory. The G1000 system should be serviced.
AFCS
GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity
Monitoring (RAIM) from the FAF to the MAP waypoints.
Loss of GPS integrity monitoring.
ADDITIONAL
FEATURES
Loss of GPS navigation due to insufficient satellites.
Loss of GPS navigation due to position error.
APPENDICES
Loss of GPS navigation due to GPS failure.
Abort approach due to loss of GPS navigation.
Displayed after passing the first waypoint of a true north approach when the nav
angle is set to ‘AUTO’.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
190-00552-05 Rev. A
SYSTEM
OVERVIEW
MANIFEST– COM1 software
mismatch, communication halted.
MANIFEST– COM2 software
mismatch, communication halted.
MANIFEST– NAV1 software
mismatch, communication halted.
MANIFEST– NAV2 software
mismatch, communication halted.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk key
is stuck.
COM2 PTT – COM2 push-to-talk key
is stuck.
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
COM1 CONFIG – COM1 config error.
Config service req’d.
COM2 CONFIG– COM2 config error.
Config service req’d.
RAIM UNAVAIL – RAIM is not
available from FAF to MAP waypoints.
LOI – GPS integrity lost. Crosscheck
with other NAVS.
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
ABORT APR – Loss of GPS navigation.
Abort approach.
TRUE APR – True north approach.
Change HDG reference to TRUE.
513
SYSTEM
OVERVIEW
APPENDIX A
GPS1 FAIL – GPS1 is inoperative.
FLIGHT
INSTRUMENTS
GPS2 FAIL – GPS2 is inoperative.
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
GPS1 SERVICE – GPS1 needs service.
Return unit for repair.
GPS2 SERVICE – GPS2 needs service.
Return unit for repair.
NAV1 SERVICE – NAV1 needs service.
Return unit for repair.
NAV2 SERVICE – NAV2 needs service.
Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
G/S1 FAIL – G/S1 is inoperative.
G/S2 FAIL – G/S2 is inoperative.
HAZARD
AVOIDANCE
G/S1 SERVICE – G/S1 needs service.
Return unit for repair.
G/S2 SERVICE – G/S2 needs service.
Return unit for repair.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is
unavailable. The G1000 system should be serviced.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be serviced.
A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be serviced.
The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”)
state. Press the transfer switch again to cycle its operation. If the problem persists,
the G1000 system should be serviced.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000
system should be serviced.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver
may still be available. The G1000 system should be serviced when possible.
GIA 63W MESSAGE ADVISORIES
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
514
Comments
The GIA1 and/or GIA2 configuration settings do not match backup configuration
memory. The system should be serviced.
The GIA1 and/or GIA2 have an error in the audio configuration. The system should be
serviced.
The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to
warm up to operating temperature.
The GIA1 and/or GIA2 temperature is too high. If problem persists, the system should
be serviced.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
Comments
The GIA1 and/or GIA2 self-test has detected a problem in the unit. The system should
be serviced.
FLIGHT
INSTRUMENTS
A GIA mismatch has been detected, where only one is SBAS capable.
EIS
The GIA1 and/or GIA 2 has incorrect software installed. The system should be
serviced.
AUDIO PANEL
& CNS
Incorrect servo software is installed, or gain settings are incorrect.
FLIGHT
MANAGEMENT
COM1 and/or COM2 software mismatch. The G1000 system should be serviced.
HAZARD
AVOIDANCE
NAV1 and/or NAV2 software mismatch. The G1000 system should be serviced.
The system has detected an over temperature condition in COM1 and/or COM2. The
transmitter operates at reduced power. If the problem persists, the system should be
serviced.
AFCS
The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may
still be usable. The system should be serviced when possible.
ADDITIONAL
FEATURES
The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or
“pressed”) position. Press the PTT switch again to cycle its operation.
If the problem persists, the system should be serviced.
APPENDICES
The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”)
position. Press the transfer switch again to cycle its operation. If the problem
persists, the system should be serviced.
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
190-00552-05 Rev. A
SYSTEM
OVERVIEW
Message
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
HW MISMATCH – GIA hardware
mismatch. GIA1 communication
halted.
HW MISMATCH – GIA hardware
mismatch. GIA2 communication
halted.
MANIFEST – GIA1 software
mismatch, communication halted.
MANIFEST – GIA2 software
mismatch, communication halted.
MANIFEST – GFC software mismatch,
communication halted.
MANIFEST– COM1 software
mismatch, communication halted.
MANIFEST– COM2 software
mismatch, communication halted.
MANIFEST– NAV1 software
mismatch, communication halted.
MANIFEST– NAV2 software
mismatch, communication halted.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE – COM1 needs
service. Return unit for repair.
COM2 SERVICE – COM2 needs
service. Return unit for repair.
COM1 PTT – COM1 push-to-talk key
is stuck.
COM2 PTT – COM2 push-to-talk key
is stuck.
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
515
SYSTEM
OVERVIEW
APPENDIX A
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Message
COM1 CONFIG – COM1 config error.
Config service req’d.
COM2 CONFIG – COM2 config error.
Config service req’d.
LOI – GPS integrity lost. Crosscheck
with other NAVS.
GPS NAV LOST – Loss of GPS
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
ABORT APR – Loss of GPS navigation.
Abort approach.
APR DWNGRADE – Approach
downgraded.
TRUE APR – True north approach.
Change HDG reference to TRUE.
GPS1 SERVICE – GPS1 needs service.
Return unit for repair.
GPS2 SERVICE – GPS2 needs service.
Return unit for repair.
NAV1 SERVICE – NAV1 needs service.
Return unit for repair.
NAV2 SERVICE – NAV2 needs service.
Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
G/S1 FAIL – G/S1 is inoperative.
G/S2 FAIL – G/S2 is inoperative.
Comments
The COM1 and/or COM2 configuration settings do not match backup configuration
memory. The G1000 system should be serviced.
GPS integrity is insufficient for the current phase of flight.
Loss of GPS navigation due to insufficient satellites.
Loss of GPS navigation due to position error.
Loss of GPS navigation due to GPS failure.
Abort approach due to loss of GPS navigation.
Vertical guidance generated by SBAS is unavailable, use LNAV only minimums.
Displayed after passing the first waypoint of a true north approach when the nav angle is
set to ‘AUTO’.
A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still
be available. The system should be serviced.
A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still
be available. The system should be serviced.
The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”)
state. Press the transfer switch again to cycle its operation. If the problem persists,
the system should be serviced.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The system
should be serviced.
INDEX
APPENDICES
G/S1 SERVICE – G/S1 needs service.
Return unit for repair.
A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver
G/S2 SERVICE – G/S2 needs service. may still be available. The system should be serviced when possible.
Return unit for repair.
FAILED PATH – A data path has failed.
A data path connected to the GDU or the GIA 63/W has failed.
516
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
GDC 74A MESSAGE ADVISORIES
Comments
The GDC 74A has incorrect software installed. The G1000 system should be serviced.
FLIGHT
INSTRUMENTS
Message
MANIFEST – GDC1 software
mismatch, communication halted.
GEA 71 MESSAGE ADVISORIES
Comments
The GEA1 configuration settings do not match those of backup configuration memory.
The G1000 system should be serviced.
The #1 GEA 71 has incorrect software installed. The G1000 system should be
serviced.
EIS
Message
GEA1 CONFIG – GEA1 config error.
Config service req’d.
MANIFEST – GEA1 software
mismatch, communication halted.
AUDIO PANEL
& CNS
GTX 33 MESSAGE ADVISORIES
Comments
The transponder configuration settings do not match those of backup configuration
memory. The G1000 system should be serviced.
The transponder has incorrect software installed. The G1000 system should be
serviced.
FLIGHT
MANAGEMENT
The #1 transponder should be serviced when possible.
There is no communication with the #1 transponder.
HAZARD
AVOIDANCE
Message
XPDR1 CONFIG – XPDR1 config error.
Config service req’d.
MANIFEST – GTX1 software
mismatch, communication halted.
XPDR1 SRVC – XPDR1 needs service.
Return unit for repair.
XPDR1 FAIL – XPDR1 is inoperative.
GMU 44 MESSAGE ADVISORIES
Comments
A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The G1000 system should be serviced.
The GMU 44 has incorrect software installed. The G1000 system should be serviced.
AFCS
Message
HDG FAULT – AHRS1 magnetometer
fault has occurred.
MANIFEST – GMU1 software
mismatch, communication halted.
AHRS1 GPS – AHRS1 using backup
GPS source.
Comments
The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS
relies on GPS information to augment the lack of airspeed. The G1000 system should
be serviced.
The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The G1000
system should be serviced when possible.
APPENDICES
Message
AHRS1 TAS – AHRS1 not receiving
airspeed.
ADDITIONAL
FEATURES
GRS 77 MESSAGE ADVISORIES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
517
SYSTEM
OVERVIEW
APPENDIX A
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Message
AHRS1 GPS – AHRS1 not receiving
any GPS information.
AHRS1 GPS – AHRS1 not receiving
backup GPS information.
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS1 SRVC – AHRS1 Magnetic-field
model needs update.
GEO LIMITS – AHRS1 too far North/
South, no magnetic compass.
MANIFEST – GRS1 software
mismatch, communication halted.
Comments
The #1 AHRS is not receiving any or any useful GPS information. Check AFMS
limitations. The G1000 system should be serviced.
The #1 AHRS is not receiving backup GPS information. The G1000 system should be
serviced.
The #1 AHRS is operating exclusively in no-GPS mode. The G1000 system should be
serviced.
The #1 AHRS earth magnetic field model is out of date. Update magnetic field model
when practical.
The aircraft is outside geographical limits for approved AHRS operation. Heading is
flagged as invalid.
The #1 AHRS has incorrect software installed. The G1000 system should be serviced.
GCU 476 MESSAGE ADVISORIES
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Alerts Window Message
GCU CNFG – GCU config error.
Config service req’d.
GCU FAIL – GCU is inoperative.
GCU KEYSTK – GCU [key name] Key
is stuck.
MANIFEST – GCU software mismatch,
communication halted.
Comments
GCU 476 configuration settings do not match those of backup configuration memory.
The G1000 System should be serviced.
The GCU 476 has failed. The G1000 System should be serviced when possible.
A key is stuck on the GCU 476 bezel. Attempt to free the stuck key by pressing it
several times. The G1000 system should be serviced if the problem persists.
The GCU 476 has incorrect software installed. The G1000 system should be serviced.
GDL 69/69A SATELLITE DATALINK RECEIVER MESSAGE ADVISORIES
ADDITIONAL
FEATURES
AFCS
Message Advisory
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
GDL69 FAIL – GDL 69 has failed.
Comments
GDL 69 configuration settings do not match those of backup configuration memory.
The G1000 system should be serviced.
A failure has been detected in the GDL 69. The receiver is unavailable. The G1000
system should be serviced.
MANIFEST – GDL software mismatch,
The GDL 69 has incorrect software installed. The G1000 system should be serviced.
communication halted.
APPENDICES
GMA 1347 MESSAGE ADVISORIES
Comments
The audio panel self-test has detected a failure. The audio panel is unavailable. The
G1000 system should be serviced.
GMA1 CONFIG – GMA1 configuration The audio panel configuration settings do not match backup configuration memory.
error. Config service req’d.
The G1000 system should be serviced.
MANIFEST – GMA1 software
The audio panel has incorrect software installed. The G1000 system should be
mismatch. Communication halted.
serviced.
INDEX
Message
GMA1 FAIL – GMA1 is inoperative.
518
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
Message
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
FLIGHT
INSTRUMENTS
Comments
The audio panel self-test has detected a problem in the unit. Certain audio functions
may still be available, and the audio panel may still be usable. The G1000 system
should be serviced when possible.
MISCELLANEOUS MESSAGE ADVISORIES
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
AUDIO PANEL
& CNS
190-00552-05 Rev. A
EIS
Message
Comments
FPL WPT LOCK – Flight plan waypoint Upon power-up, the system detects that a stored flight plan waypoint is locked. This
is locked.
occurs when an navigation database update eliminates an obsolete waypoint. The
flight plan cannot find the specified waypoint and flags this message. This can also
occur with user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it no longer exists in any database,
Or
Update the waypoint name/identifier to reflect the new information.
FPL WPT MOVE – Flight plan
The system has detected that a waypoint coordinate has changed due to a new
waypoint moved.
navigation database update. Verify that stored flight plans contain correct waypoint
locations.
TIMER EXPIRD – Timer has expired.
The system notifies the pilot that the timer has expired.
DB CHANGE – Database changed.
This occurs when a stored flight plan contains an airway that is no longer consistent
Verify user modified procedures.
with the navigation database. This alert is issued only after an navigation database
update. Verify that the user-modified procedures in stored flight plans are correct and
up to date.
DB CHANGE – Database changed.
This occurs when a stored flight plan contains an airway that is no longer consistent
Verify stored airways.
with the navigation database. This alert is issued only after an navigation database
update. Verify use of airways in stored flight plans and reload airways as needed.
FPL TRUNC – Flight plan has been
This occurs when a newly installed navigation database eliminates an obsolete
truncated.
approach or arrival used by a stored flight plan. The obsolete procedure is removed
from the flight plan. Update flight plan with current arrival or approach.
LOCKED FPL – Cannot navigate
This occurs when the pilot attempts to activate a stored flight plan that contains
locked flight plan.
locked waypoint. Remove locked waypoint from flight plan. Update flight plan with
current waypoint.
WPT ARRIVAL – Arriving at waypoint
Arriving at waypoint [xxxx], where [xxxx] is the waypoint name.
-[xxxx]
STEEP TURN – Steep turn ahead.
A steep turn is 15 seconds ahead. Prepare to turn.
INSIDE ARSPC – Inside airspace.
The aircraft is inside the airspace.
ARSPC AHEAD – Airspace ahead less Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace within
than 10 minutes.
10 minutes.
ARSPC NEAR – Airspace near and
Special use airspace is near and ahead of the aircraft position.
ahead.
ARSPC NEAR – Airspace near – less
Special use airspace is within 2 nm of the aircraft position.
than 2 nm.
APPR INACTV – Approach is not
The system notifies the pilot that the loaded approach is not active. Activate
active.
approach when required.
519
SYSTEM
OVERVIEW
APPENDIX A
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Message
SLCT FREQ – Select appropriate
frequency for approach.
SLCT NAV – Select NAV on CDI for
approach.
PTK FAIL – Parallel track unavailable:
bad geometry.
PTK FAIL – Parallel track unavailable:
invalid leg type.
PTK FAIL – Parallel track unavailable:
past IAF.
UNABLE V WPT – Can’t reach current
vertical waypoint.
VNV – Unavailable. Unsupported leg
type in flight plan.
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Parallel course
selected.
NON WGS84 WPT – Do not use GPS
navigation to [xxxx].
AFCS
STRMSCP FAIL – Stormscope has
failed.
TRAFFIC FAIL – Traffic device has
failed.
FAILED PATH – A data path has failed.
MAG VAR WARN – Large magnetic
variance. Verify all course angles.
Comments
The system notifies the pilot to load the approach frequency for the appropriate NAV
receiver. Select the correct frequency for the approach.
The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI to
the correct NAV receiver.
Bad parallel track geometry.
Invalid leg type for parallel offset.
IAF waypoint for parallel offset has been passed.
The current vertical waypoint can not be reached within the maximum flight path
angle and vertical speed constraints. The system automatically transitions to the next
vertical waypoint.
The lateral flight plan contains a procedure turn, vector, or other unsupported leg
type prior to the active vertical waypoint. This prevents vertical guidance to the active
vertical waypoint.
The current crosstrack exceeds the limit, causing vertical deviation to go invalid.
The current track angle error exceeds the limit, causing the vertical deviation to go
invalid.
A parallel course has been selected, causing the vertical deviation to go invalid.
The position of the selected waypoint [xxxx] is not calculated based on the WGS84
map reference datum and may be positioned in error as displayed. Do not use GPS to
navigate to the selected non-WGS84 waypoint.
Stormscope has failed. The G1000 system should be serviced.
INDEX
APPENDICES
ADDITIONAL
FEATURES
The system is no longer receiving data from the traffic system. The traffic device
should be serviced.
A data path connected to the GDU or the GIA 63/W has failed.
The GDU’s internal model cannot determine the exact magnetic variance for
geographic locations near the magnetic poles. Displayed magnetic course angles may
differ from the actual magnetic heading by more than 2°.
SVS – SVS DISABLED: Out of available Synthetic Vision is disabled because the aircraft is not within the boundaries of the
terrain region.
installed terrain database.
SVS – SVS DISABLED: Terrain DB
Synthetic Vision is disabled because a terrain database of sufficient resolution (9 arcresolution too low.
second or better) is not currently installed.
SCHEDULER [#] – <message>.
Message criteria entered by the user.
CHECK CRS – Database course for
Selected course for LOC1 differs from published localizer course by more than 10
LOC1 / [LOC ID] is [CRS]°.
degrees.
CHECK CRS – Database course for
Selected course for LOC2 differs from published localizer course by more than 10
LOC2 / [LOC ID] is [CRS]°.
degrees.
520
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
Comments
The SD card was removed from the top card slot of the PFD or MFD. The SD card
needs to be reinserted.
The SD card was removed from the bottom card slot of the PFD or MFD. The SD card
needs to be reinserted.
FLIGHT
INSTRUMENTS
The SD card in the top card slot of the PFD or MFD contains invalid data.
The SD card in the bottom card slot of the specified PFD or MFD contains invalid data.
EIS
The audio source for terrain awareness is offline. Check GIA1 or GIA 2.
Terrain audio alerts are not configured properly. The system should be serviced
AUDIO PANEL
& CNS
Message
[PFD1, or MFD1] CARD 1 REM –
Card 1 was removed. Reinsert card.
[PFD1, or MFD1] CARD 2 REM –
Card 2 was removed. Reinsert card.
[PFD1, or MFD1] CARD 1 ERR – Card
1 is invalid.
[PFD1, or MFD1] CARD 2 ERR – Card
2 is invalid.
TRN AUD FAIL – Trn Awareness audio
source unavailable.
TERRAIN AUD CFG – Trn Awareness
audio config error. Service req’d.
FLIGHT PLAN IMPORT/EXPORT MESSAGES
‘Too many points. Flight plan truncated.’
‘User waypoint database full. Not all loaded.’
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
‘Flight plan successfully exported.’
‘Flight plan export failed.’
APPENDICES
‘One or more user waypoints renamed.’
ADDITIONAL
FEATURES
‘Some waypoints not loaded. Waypoints
locked.’
AFCS
‘File contained user waypoints only.’
Description
A flight plan file stored on the SD card was successfully imported as a stored flight plan.
The file stored on the SD card did not contain a flight plan, only user waypoints. These
waypoints have been saved to the system user waypoints. No flight plans stored in the
system have been modified.
The SD card contains no flight plan data.
Flight plan data was not successfully imported from the SD card.
Some flight plan waypoints were successfully imported from the SD card, however others
had errors and were not imported. A partial stored flight plan now exists in the system.
The file stored on the SD card did not contain a flight plan, only user waypoints. One or
more of these waypoints did not import successfully.
The flight plan on the SD card contains more waypoints than the system can support. The
flight plan was imported with as many waypoints as possible.
The flight plan on the SD card contains one or more waypoints that the system cannot find
in the navigation database. The flight plan has been imported, but must be edited within
the system before it can be activated for use.
The flight plan file on the SD card contains user waypoints. The quantity of stored user
waypoints has exceeded system capacity, therefore not all the user waypoints on the SD
card have been imported. Any flight plan user waypoints that were not imported are
locked in the flight plan. The flight plan must be edited within the system before it can be
activated for use.
One or more imported user waypoints were renamed when imported due to naming
conflicts with waypoints already existing in the system.
The stored flight plan was successfully exported to the SD card.
The stored flight plan was not successfully exported to the SD card. The SD card may not
have sufficient available memory or the card may have been removed prematurely.
HAZARD
AVOIDANCE
Flight Plan Import/Export Results
‘Flight plan successfully imported.’
‘File contained user waypoints only. User
waypoints imported successfully. No stored
flight plan data was modified.’
‘No flight plan files found to import.’
‘Flight plan import failed.’
‘Flight plan partially imported.’
FLIGHT
MANAGEMENT
In some circumstances, some messages may appear in conjunction with others.
521
SYSTEM
OVERVIEW
APPENDIX A
AFCS STATUS ANNUNCIATIONS
FLIGHT
INSTRUMENTS
The following annunciations (listed in order of increasing priority) can appear on the PFD above the Airspeed
and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality.
EIS
AFCS Status
Annunciation
AUDIO PANEL
& CNS
Figure A-6 AFCS Status Annunciation
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
Condition
Pitch Failure
AFCS
Description
Pitch axis control failure. AP is inoperative.
Roll Failure
Roll axis control failure. AP is inoperative.
MET Switch Stuck, or
Pitch Trim Axis Control
Failure
System Failure
If annunciated when AP is engaged, take control of the aircraft and disengage the autopilot.
If annunciated when AP is not engaged, move each half of the MET switch separately to
check if a stuck switch is causing the annunciation.
AP and MET are unavailable. FD may still be available.
Elevator Mistrim Up
A condition has developed causing the pitch servo to provide a sustained force. Be prepared
to apply nose up control wheel force upon autopilot disconnect.
A condition has developed causing the pitch servo to provide a sustained force. Be prepared
to apply nose down control wheel force upon autopilot disconnect.
A condition has developed causing the roll servo to provide a sustained left force. Ensure
the slip/skid indicator is centered and observe any maximum fuel imbalance limits.
A condition has developed causing the roll servo to provide a sustained right force. Ensure
the slip/skid indicator is centered and observe any maximum fuel imbalance limits.
Performing preflight system test. Upon completion of the test, the aural alert is heard.
Elevator Mistrim
Down
Aileron Mistrim Left
Aileron Mistrim Right
ADDITIONAL
FEATURES
Annunciation
Preflight Test
APPENDICES
Preflight system test has failed.
NOTE: Do not press the AP DISC switch during servo power-up and preflight system tests as this may cause
INDEX
the preflight system test to fail or never to start (if servos fail their power-up tests). Power must be cycled
to the servos to remedy the situation.
522
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
TERRAIN-SVS ALERTS
Alert Type
MFD Map Page PopUp Alert (except
Terrain-SVS Page)
PFD/MFD* Alert
Annunciation
Aural Message
“Warning; Terrain, Terrain”
Imminent Terrain Impact Warning (ITI)
“Warning; Terrain, Terrain”
Reduced Required Obstacle Clearance Warning (ROC)
“Warning; Obstacle, Obstacle”
Imminent Obstacle Impact Warning (IOI)
“Warning; Obstacle, Obstacle”
“Caution; Terrain, Terrain”
Imminent Terrain Impact Caution (ITI)
“Caution; Terrain, Terrain”
“Caution; Obstacle, Obstacle”
Imminent Obstacle Impact Caution (IOI)
“Caution; Obstacle, Obstacle”
AUDIO PANEL
& CNS
Reduced Required Obstacle Clearance Caution (ROC)
EIS
Reduced Required Terrain Clearance Caution (RTC)
FLIGHT
INSTRUMENTS
Reduced Required Terrain Clearance Warning (RTC)
FLIGHT
MANAGEMENT
* Annunciation shown on MFD when terrain display is enabled
TERRAIN-SVS SYSTEM STATUS ANNUNCIATIONS
None
None
“Terrain System Test OK”
None
None
TERRAIN DATABASE FAILURE
None
Terrain System Test Fail
TERRAIN FAIL
“Terrain System Failure”
Terrain or Obstacle database unavailable or
invalid, invalid software configuration, system
audio fault
TERRAIN FAIL
“Terrain System Failure”
NO GPS POSITION
“Terrain System Not Available”
None
“Terrain System Not Available”
None
“Terrain System Available”
System Test Pass
None
Terrain Alerting is disabled
MFD Terrain or Obstacle database unavailable or
invalid. Terrain-SVS operating with PFD Terrain
or Obstacle databases
None
No GPS position
Excessively degraded GPS signal, Out of
database coverage area
Sufficient GPS signal received after loss, Aircraft
returns to database coverage area
None
APPENDICES
TERRAIN TEST
System Test in Progress
ADDITIONAL
FEATURES
Aural Message
AFCS
Terrain-SVS Page Center
Banner Annunciation
Alert Type
HAZARD
AVOIDANCE
PFD/MFD*
Status
Annunciation
* Annunciation shown on MFD when terrain display is enabled
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
523
SYSTEM
OVERVIEW
APPENDIX A
TAWS-B ALERTS
FLIGHT
INSTRUMENTS
Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
PFD/MFD* Alert
Annunciation
Alert Type
MFD Map Page
Pop-Up Alert (except
TAWS-B Page)
Excessive Descent Rate Warning (EDR)
“Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”
or
“Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up, Pull Up”
Reduced Required Obstacle Clearance
Warning (ROC)
or
“Obstacle, Obstacle; Pull Up, Pull Up”
or
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
Imminent Obstacle Impact Warning
(IOI)
or
“Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull Up, Pull Up”
Reduced Required Terrain Clearance
Caution (RTC)
or
“Caution, Terrain; Caution, Terrain”
or
“Terrain Ahead; Terrain Ahead”
or
“Terrain Ahead; Terrain Ahead”
or
“Caution, Terrain; Caution, Terrain”
or
“Caution, Obstacle; Caution, Obstacle”
or
“Obstacle Ahead; Obstacle Ahead”
or
“Obstacle Ahead; Obstacle Ahead”
or
“Caution, Obstacle; Caution, Obstacle”
EIS
Reduced Required Terrain Clearance
Warning (RTC)
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
Imminent Terrain Impact Warning (ITI)
Imminent Terrain Impact Caution (ITI)
AFCS
Reduced Required Obstacle Clearance
Caution (ROC)
ADDITIONAL
FEATURES
Imminent Obstacle Impact Caution
(IOI)
Premature Descent Alert Caution
(PDA)
Altitude Callout “500”
“Too Low, Terrain”
None
None
Excessive Descent Rate Caution (EDR)
“Five-Hundred”
“Sink Rate”
Negative Climb Rate Caution (NCR)
APPENDICES
Aural Message
or
“Don’t Sink”
or
“Too Low, Terrain”
INDEX
* Annunciation shown on MFD when terrain display is enabled
524
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX A
SYSTEM
OVERVIEW
TAWS-B SYSTEM STATUS ANNUNCIATIONS
Alert Type
PFD/MFD* Status
Annunciation
Aural Message
TAWS TEST
None
None
“TAWS System Test OK”
MFD Terrain or Obstacle database unavailable or
invalid. TAWS operating with PFD Terrain or Obstacle
databases
None
TERRAIN DATABASE FAILURE
None
TAWS-B System Test Fail
TAWS FAIL
“TAWS System Failure”
Terrain or Obstacle database unavailable or invalid,
invalid software configuration, system audio fault
TAWS FAIL
“TAWS System Failure”
NO GPS POSITION
“TAWS Not Available”
None
“TAWS Not Available”
None
“TAWS Available”
No GPS position
Excessively degraded GPS signal, Out of database
coverage area
Sufficient GPS signal received after loss, Aircraft returns
to database coverage area
None
AUDIO PANEL
& CNS
None
EIS
System Test Pass
FLIGHT
INSTRUMENTS
System Test in Progress
TAWS-B Page Center
Banner Annunciation
FLIGHT
MANAGEMENT
* Annunciation shown on MFD when terrain display is enabled
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
525
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
APPENDIX A
Blank Page
526
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX B
SYSTEM
OVERVIEW
DATABASE MANAGEMENT
CAUTION: Never disconnect power to the system when loading a database. Power interuption during the
FLIGHT
INSTRUMENTS
database loading process could result in maintenance being required to reboot the system.
The system uses Secure Digital (SD) cards to load and store various types of data. For basic flight operations, SD
cards are required for database storage as well as Jeppesen navigation and ChartView database updates. Not all SD
cards are compatible with the G1000 system. Use only SD cards supplied by Garmin or the aircraft manufacturer.
EIS
CAUTION: When downloading updates to the Jeppesen Navigation Database, copy the data to an SD card
other than a Garmin Supplemental Data Card. Otherwise, data corruption can occur.
AUDIO PANEL
& CNS
NOTE: When loading database updates, the ‘DB Mismatch’ message will be displayed until database
synchronization is complete, followed by turning system power off, then on. Synchronization can be
monitored on the AUX-SYSTEM STATUS Page.
NOTE: Loading a database in the system prior to its effective date will result in the expiration date on the
FLIGHT
MANAGEMENT
power-up screen and the effective date on the AUX-System Status Page being displayed in yellow.
NOTE: Garmin requests the flight crew report any observed discrepancies related to database information.
HAZARD
AVOIDANCE
These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles
and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go
to FlyGarmin.com and select “Aviation Data Error Report”.
JEPPESEN DATABASES
AFCS
The navigation database is updated on a 28-day cycle. The ChartView database is updated on a 14-day
cycle. If the ChartView database is not updated within 70 days of the expiration date, ChartView will no longer
function. Both of these databases are provided directly from Jeppesen.
NOTE: The Jeppesen aviation navigation database is now referred to as the ‘navigation database’. Previously
ADDITIONAL
FEATURES
this database had been referred to as the ‘aviation database’.
The ChartView database should be copied to the Garmin supplied Supplemental Data Card which will reside
in the bottom card slot on the MFD. The navigation database must be installed from the Jeppesen or user
supplied SD data card. Contact Jeppesen (www.jeppesen.com) for subscription and update information.
APPENDICES
NOTE: After the navigation database is installed, the card may be removed.
Updating the active navigation database (not using the Dual Navigation Database or Automatic
Database Synchronization Features):
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the
display (PFD1 or MFD) to be updated (label of SD card facing left).
527
SYSTEM
OVERVIEW
APPENDIX B
FLIGHT
INSTRUMENTS
2) Turn the system ON. A prompt similar to the following is displayed in the upper left corner of the display:
EIS
Figure B-1 Standby Navigation Database Prompt
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
3) Press the NO Softkey to proceed to loading the active database.
4) A prompt similar to the following is displayed, press the YES Softkey to update the active navigation database.
Figure B-2 Database Update Confirmation
AFCS
5) After the update completes, the display starts in normal mode. Do not remove power while the display is
starting.
6) Turn the system OFF and remove the SD card from the top card slot.
ADDITIONAL
FEATURES
7) Repeat steps 1 through 6 for the other display (PFD1 or MFD). Remove the SD card when finished.
8) Apply power to the system and press the ENT Key to acknowledge the startup screen.
9) Turn the large FMS Knob to select the AUX Page group on the MFD.
10) Turn the small FMS Knob to select the System Status Page.
APPENDICES
11) Press the Display Database Selection Softkey to show active navigation database information for each display (MFD1
DB, PFD1 DB). Verify the correct active navigation database cycle information is shown for each display.
DUAL NAVIGATION DATABASE FEATURE
INDEX
The dual navigation database feature allows each display to store an upcoming navigation database on the
bottom SD card so that the system can automatically load it to replace the active database when the new
database becomes effective (the next cycle becomes available seven days prior to its effective date).
528
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX B
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
If a navigation database loader card is inserted into the top SD card slot of a display, and an SD card is in the
bottom slot, the system will prompt the user (upon on-ground power up) as to whether the database should
be stored on the bottom SD card as the standby database. If the user responds affirmatively, the system will
copy the navigation database from the top SD card to the bottom SD card. As long as the bottom SD card
remains in the card slot, this standby navigation database will be available for the system to use as the active
database as soon as it becomes effective.
EIS
The system checks the active and standby databases upon (on-ground only) power-up. If the standby
database is current and the active database is out of date, the display will upload the standby database into
the active internal database location. Loading the standby database to the active location takes approximately
45-55 seconds. During the loading process ‘Please Wait. Navigation Database Update in Progress. Do Not
Remove Power from Displays’ will be displayed on screen. After startup is complete, the pilot is alerted that
the update is complete by a system alert message, ‘NAV DB UPDATED’.
AUDIO PANEL
& CNS
Loading a standby navigation database:
1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot
of the MFD.
2) Verify that an SD card is inserted in the bottom slot of the PFD and the MFD.
FLIGHT
MANAGEMENT
3) Turn the system ON. A prompt similar to the following is displayed.
HAZARD
AVOIDANCE
Figure B-3 Standby Navigation Database Prompt
AFCS
4) Press the YES Softkey. The navigation database is copied to the SD card in the bottom card slot of the MFD.
5) After the navigation database files are copied to the bottom SD card, the display will appear as shown in Figure
B-4.
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
529
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
APPENDIX B
AUDIO PANEL
& CNS
Figure B-4 Standby Navigation Database Update Complete
FLIGHT
MANAGEMENT
6) As instructed on the display, press any key to continue. The display will now appear as shown in Figure B-5.
Figure B-5 Navigation Database Verification Prompt
AFCS
HAZARD
AVOIDANCE
7) Press any key to continue. The display will now appear as shown in Figure B-6.
ADDITIONAL
FEATURES
Figure B-6 Active Navigation Database Prompt
8) Press the NO Softkey. The display now starts in normal mode. Since the database effective date is not yet valid,
it should not be loaded as the active database. The display now starts in normal mode. Do not remove power
while the display is starting.
APPENDICES
9) Press the ENT Key to acknowledge the startup screen.
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
11) Turn the small FMS Knob to select the System Status Page.
INDEX
12) The new database is copied to the SD card in the bottom card slot of the PFD. Progress can be monitored in the
SYNC STATUS field. When copying is finished, ‘Complete’ is displayed.
13) Turn system power OFF.
530
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX B
SYSTEM
OVERVIEW
14) Remove the SD card from the top card slot of the MFD.
15) Turn system power ON.
16) Press the ENT Key to acknowledge the startup screen.
FLIGHT
INSTRUMENTS
17) Turn the large FMS Knob to select the AUX Page group on the MFD.
18) Turn the small FMS Knob to select the System Status Page.
19) Press the Display Database Selection Softkey to show standby navigation database information for each display
(MFD1 DB, PFD1 DB). Verify the correct standby navigation database cycle information is shown for each
display.
EIS
GARMIN DATABASES
The following databases are stored on Supplemental Data Cards provided by Garmin:
• Airport terrain
• SafeTaxi
• Terrain
• Obstacle
• FliteCharts
AUDIO PANEL
& CNS
• Expanded basemap
• Airport Directory
(AOPA or AC-UKWIK)
FLIGHT
MANAGEMENT
After subscribing to the desired database product, these database products will be downloaded and ultimately
stored on two Supplemental Data Cards (with the exception of FliteCharts, which is loaded on only one card).
Each Supplemental Data Card resides in the bottom card of each display as shown in Figure B-7. These cards
must not be removed except to update the databases stored on each card.
HAZARD
AVOIDANCE
AFCS
MFD
ADDITIONAL
FEATURES
PFD
APPENDICES
Figure B-3 Correct Database Locations
INDEX
Since these databases are not stored internally in the displays, a Supplemental Data Card containing identical
database versions must be kept in each display unit.
The basemap database contains data for the topography and land features, such as rivers, lakes, and towns.
It is updated only periodically, with no set schedule. There is no expiration date.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
531
SYSTEM
OVERVIEW
APPENDIX B
The terrain database contains the terrain mapping data. The airport terrain database contains increased
resolution terrain data around airports. These databases are updated periodically and have no expiration date.
FLIGHT
INSTRUMENTS
The obstacle database contains data for obstacles, such as towers, that pose a potential hazard to aircraft.
Obstacles 200 feet and higher are included in the obstacle database. It is very important to note that not all
obstacles are necessarily charted and therefore may not be contained in the obstacle database. This database is
updated on a 56-day cycle.
NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin
EIS
accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of
the data.
AUDIO PANEL
& CNS
The AOPA or AC-U-KWIK Airport Directory provides detailed information about airports and heliports,
along with the names and phone numbers of thousands of FBOs. The AOPA Airport Directory covers U.S.
airports, while the AC-U-KWIK Airport Directory coverage area may be worldwide or regional, depending on
the database purchased. Both AOPA and AC-U-KWIK Airport Directory databases are updated every 56 days.
FLIGHT
MANAGEMENT
The SafeTaxi database contains detailed airport diagrams for selected airports. These diagrams aid in following
ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways,
ramps, runways, terminals, and services. This database is updated on a 56-day cycle.
The FliteCharts database contains procedure charts for the United States only. This database is updated on a
28-day cycle. If not updated within 180 days of the expiration date, FliteCharts will no longer function.
AUTOMATIC DATABASE SYNCHRONIZATION FEATURE
HAZARD
AVOIDANCE
The automatic database synchronization feature automatically transfers the database from a single
SD database card to the SD cards on the PFD and the MFD to ensure that all databases are synchronized
throughout the system. After power-up, the system compares all copies of each applicable database. If similar
databases do not match, the most recent valid database is automatically copied to each card in the system that
does not already contain that database.
ADDITIONAL
FEATURES
AFCS
The following databases are checked and synchronized: Basemap, Safetaxi, Airport Terrain, Obstacle,
Airport Directory (AOPA or AC-U-KWIK), and Terrain. This feature applies only to databases that are stored
on the SD card that resides in the bottom slot of each display. This feature does not apply to the navigation
database which is stored internally in each display, or to the charts databases (FliteCharts and ChartView)
which are only required to be present on the MFD. The typical procedure would be to download new
databases to the MFD card, then synchronize the data to the PFD.
NOTE: The 9-arc second terrain database may take as long as 100 minutes to synchronize using this method.
APPENDICES
Therefore the user may want to transfer the data using a PC, or connect the system to a ground power
source while performing the database synchronization.
INDEX
The synchronization progress may be monitored on the AUX-System Status Page in the Sync Status section
of the Database Window (Figure B-8). This section shows the synchronization status of each applicable
database, including the percent complete, time remaining, and to which displays the databases are being
copied. When the synchronization is complete, the status is listed as ‘Complete’, followed by the displays to
532
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX B
SYSTEM
OVERVIEW
which the databases were copied. This sub-section is only present when a sync is occurring or has occurred
on the current power-up.
FLIGHT
INSTRUMENTS
An indication of ‘Complete’ still requires a power cycle before the synchronized databases will be used by
the system.
EIS
AUDIO PANEL
& CNS
Figure B-5 AUX-System Status Page, Database Window
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
The Display Database Softkey (Figure B-11) is used to place the cursor in the Database Window. Upon
first press of the Display Database Softkey, the softkey will change to a selected state (black text on gray
background) and the cursor will appear in the Database Window. At this point the user can scroll through
all databases in the Database Window to view status information. If the Display Database Softkey is pressed
repeatedly, the softkey will cycle through PFD1, PFD2, and MFD. Database status information in the Database
Window will reflect the database of the selected PFD or MFD. After a successful sync and restart, verify that
the proper databases are now in use on the AUX–System Status Page (Figure B-8).
AFCS
If an error occurs during the synchronization, an error message will be displayed, followed by the affected
display in the Sync Status section of the Database Window (Figure B-9). If a synchronization completes on
one display, but an error occurs on another, the error message will be displayed with the affected diaplay
listed after it. When an error message (Table B-1) is displayed, the problem must be corrected before the
synchronization can be completed. A power cycle is required to restart synchronization when ‘Card Full’ or
‘Err’ is shown.
ADDITIONAL
FEATURES
APPENDICES
Database
Synchronization
Error Message
Figure B-6 Synchronization Error Message
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
533
SYSTEM
OVERVIEW
APPENDIX B
FLIGHT
INSTRUMENTS
Error Message
Description
Canceled
Database synchronization has been canceled by removing the bottom SD card in
display being updated
Card Full
SD card does not contain sufficient memory
Err
Displayed for all other errors that may cause the synchronization process to be halted
Timeout
System timed-out prior to the database transfer completing
Table B-1 Database Synchronization Error Messages
EIS
UPDATING GARMIN DATABASES
AUDIO PANEL
& CNS
The Garmin database updates can be obtained by following the instructions detailed in the ‘Aviation
Databases’ section of the Garmin website (fly.garmin.com). Once the updated files have been downloaded
from the website, a PC equipped with an appropriate SD card reader is used to unpack and program the new
databases onto an existing Supplemental Data Card. Equipment required to perform the update is as follows:
• Windows-compatible PC computer (running Windows XP, Vista, or Windows 7)
• SD Card Reader: SanDisk SDDR-93, SanDisk SDDR-99, Verbatim #96504, or equivalent
FLIGHT
MANAGEMENT
• Updated database obtained from the Garmin website
• Existing Supplemental Database SD Cards (010-00330-42, or -43) from both PFDs and MFD
HAZARD
AVOIDANCE
In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database
product functional. It may also be necessary to have the system configured by a Garmin authorized service
facility in order to use some database features.
After the data has been copied to the appropriate data card, perform the following steps:
1) With system power OFF, remove the MFD database card from the bottom card slot of the MFD.
AFCS
2) Update the Garmin databases on the MFD card.
3) Insert the MFD database card into the bottom card slot of the MFD.
INDEX
APPENDICES
ADDITIONAL
FEATURES
4) Apply power to the system, check that the databases are initialized and displayed on the power-up screen
(Figure B-10). When updating the terrain and FliteCharts databases, a ‘Verifying’ message may be seen. If this
message is present, wait for the system to finish loading before proceeding to step 5.
534
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX B
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Figure B-10 Database Information on the Power-up Screen
5) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right-most softkey.
6) Turn the large FMS Knob to select the AUX Page group on the MFD.
FLIGHT
MANAGEMENT
7) Turn the small FMS Knob to select the System Status Page.
8) Monitor the Sync Status in the Database Window. Wait for all databases to complete synching, indicated by
‘Complete’ being displayed as seen in Figure B-9.
9) Remove and reapply power to the system.
HAZARD
AVOIDANCE
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
11) Turn the small FMS Knob to select the System Status Page.
12) Press the Display Database Selection Softkey to show database information for each display (MFD1 DB, PFD1
DB). Verify the correct database cycle information is shown for each database for each display.
AFCS
Unselected
MFD1 DB Selected PFD1 DB Selected
Figure B-11 Display Database Softkey
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
535
SYSTEM
OVERVIEW
APPENDIX B
MAGNETIC FIELD VARIATION DATABASE UPDATE
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
A copy of the current magnetic field variation database (MV DB) is included with the navigation database.
At startup, the system compares this version of the MV DB with that presently being used by each AHRS
(GRS1 and GRS2). If the system determines the MV DB needs to be updated, a prompt is displayed on the
Navigation Map Page, as shown in Figure B-12. Note, in the following example, GRS1 is the first AHRS to
indicate an update is available. In actuality, this is dependent on which AHRS is the first to report status to the
system. GRS2 may be displayed before GRS1. The order is not important, only that both AHRS be updated.
Figure B-12 GRS1 Magnetic Field Variation Database Update Prompt
FLIGHT
MANAGEMENT
Loading the magnetic field variation database update:
AFCS
HAZARD
AVOIDANCE
1) With ‘OK’ highlighted, as seen in Figure B-12, press the ENT Key on the MFD. A progress monitor is displayed
as shown in Figure B-13.
ADDITIONAL
FEATURES
Figure B-13 Uploading Database to GRS1
APPENDICES
2) When the upload is complete, the prompt for the next GRS upload is displayed, as seen in Figure B-14.
INDEX
Figure B-14 GRS2 Magnetic Field Variation Database Update Prompt
536
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX B
SYSTEM
OVERVIEW
3) With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor is displayed as shown in Figure B-15.
When the upload is complete, the system is ready for use.
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
Figure B-15 Uploading Database to GRS2
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
537
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
APPENDIX B
Blank Page
538
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX C
SYSTEM
OVERVIEW
GLOSSARY
Course to Steer
INDEX
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
APPENDICES
CRS
CRS
CRSR
CTA
CTRL
ADDITIONAL
FEATURES
CR
CRG
CRNT
Crosstrack Error
AFCS
190-00552-05 Rev. A
barometric altitude
barometric setting
battery
backcourse
CO
COM
CONFIG
COOL
COPLT
Course
HAZARD
AVOIDANCE
B ALT
BARO
BATT
BC
CD
CDI
CDU
CF
CHT
CHKLIST
CHNL
CI
CLD
CLR
cm
CNS
FLIGHT
MANAGEMENT
ATK
AUTOSEQ
AUX
AWOS
BFO
BKSP
BRG
C
ºC
CA
CALC
Calibrated Airspeed
The compass direction from the
present position to a destination
waypoint
beat frequency oscillator
backspace
bearing
center runway
degrees Celsius
Course to Altitude
calculator
Indicated airspeed corrected for
installation and instrument errors.
Course to DME distance
Course Deviation Indicator
Control Display Unit
Course to Fix
Cylinder Head Temperature
checklist
channel
Course to Intercept
cloud
clear
centimeter
Communication, Navigation, &
Surveillance
carbon monoxide
communication radio
configuration
coolant
co-pilot
The line between two points to be
followed by the aircraft
The recommended direction to steer
in order to reduce course error or
stay on course. Provides the most
efficient heading to get back to the
desired course and proceed along
the flight plan
Course to Radial
Cockpit Reference Guide
current
The distance the aircraft is off a
desired course in either direction, left
or right
course
Course to Steer
cursor
Control Area
control
AUDIO PANEL
& CNS
ATC
ATCRBS
ATIS
Bearing
EIS
AIM
AIRMET
ALRT
ALT
ALT, ALTN
AMPS
ANNUNC
ANT
AP
AP DISC
APR
APT
ARINC
ARSPC
ARTCC
ARV
AS
ASB
ASOS
accuracy
active, activate
air data computer
Automatic Direction Finder
Attitude Direction Indicator
Arc to fix
Automatic Flight Control System
Airplane Flight Manual
Airplane Flight Manual Supplement
airframe
Above Ground Level
Attitude and Heading Reference
System
Airman’s Information Manual
Airman’s Meteorological Information
alert
altitude
alternator
amperes
annunciation
antenna
autopilot
autopilot disconnect
approach
airport, aerodrome
Aeronautical Radio Incorporated
airspace
Air Route Traffic Control Center
arrival
airspeed
Aviation Support Branch
Automated Surface Observing
System
Air Traffic Control
ATC Radar Beacon System
Automatic Terminal Information
Service
along-track
automatic sequence
auxiliary
Automated Weather Observing
System
FLIGHT
INSTRUMENTS
ACC
ACT, ACTV
ADC
ADF
ADI
AF
AFCS
AFM
AFMS
AFRM
AGL
AHRS
539
SYSTEM
OVERVIEW
APPENDIX C
FLIGHT
INSTRUMENTS
Cumulative
CVR
CVRG
CWS
CYL
The total of all legs in a flight plan.
Cockpit Voice Recorder
coverage
control wheel steering
cylinder
density altitude
database
decibels ‘Z’ (radar return)
declutter
decrease fuel
degree
de-icing
departure
The desired course between the
active “from” and “to” waypoints
DEST
destination
DF
Direct to Fix
DFLT
default
DGRD
degrade
DH
decision height
Dilution of Precision A measure of GPS satellite geometry
quality on a scale of one to ten (lower
numbers equal better geometry,
where higher numbers equal poorer
geometry)
DIR
direction
DIS
distance
Distance
The ‘great circle’ distance from the
present position to a destination
waypoint
DME
Distance Measuring Equipment
DOP
Dilution of Precision
DP
Departure Procedure
DPRT
departure
DR
dead reckoning
DSBL
disabled
DTK
Desired Track
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
D ALT
DB, DBASE
dBZ
DCLTR, DECLTR
DEC FUEL
deg
DEIC, DEICE
DEP
Desired Track
APPENDICES
E
ECU
Efficiency
EGNOS
INDEX
EGT
EIS
ELEV
ELEV
EMERGCY
540
empty, east
Engine Control Unit
A measure of fuel consumption,
expressed in distance per unit of fuel
European Geostationary Navigation
Overlay Service
Exhaust Gas Temperature
Engine Indication System
elevation
elevator
emergency
EMI
ENDUR
Endurance
Electromagnetic Interference
endurance
Flight endurance, or total possible
flight time based on available fuel on
board
ENG
engine
ENGD
engaged
ENR
enroute
Enroute Safe Altitude The recommended minimum altitude
within ten miles left or right of the
desired course on an active flight
plan or direct-to
ENT
enter
EPE
Estimated Position Error
EPU
Estimated Position Uncertainty
ERR
error
ESA
Enroute Safe Altitude
Estimated Position Error A measure of horizontal GPS position
error derived by satellite geometry
conditions and other factors
Estimated Time of Arrival The estimated time at which the
aircraft should reach the destination
waypoint, based upon current speed
and track
Estimated Time Enroute The estimated time it takes to reach
the destination waypoint from the
present position, based upon current
ground speed
ETA
Estimated Time of Arrival
ETE
Estimated Time Enroute
EXPIRD
expired
ºF
FA
FAA
FADEC
FAF
FAIL
FC
FCC
FCST
FD
FD
FDE
FFLOW
FIS-B
FISDL
FL
FLC
degrees Fahrenheit
Course From Fix to Altitude
Federal Aviation Administration
Full Authority Digital Engine Control
Final Approach Fix
failure
Course From Fix to Distance
Federal Communication Commission
forecast
Course From Fix to DME Distance
flight director
Fault Detection and Exclusion
fuel flow
Flight Information ServicesBroadcast
Flight Information Service Data Link
flight level
Flight Level Change
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX C
AFCS
ADDITIONAL
FEATURES
APPENDICES
key stuck
kilogram
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
190-00552-05 Rev. A
HAZARD
AVOIDANCE
Groundspeed
FLIGHT
MANAGEMENT
KEYSTK
kg
GMA
GMT
GMU
GND
gph
GPS
Grid MORA
AUDIO PANEL
& CNS
Hold Terminating at Altitude
heading
G/S, GS
GA
gal, gl
GBOX
GDC
GDL
GDU
GEA
GEO
GFC
GIA
GLS
EIS
HA
HDG
Fuel On Board
Heading
FLIGHT
INSTRUMENTS
Ground Track
GRS
GS
GTX
glideslope
go-around
gallon(s)
gearbox
Garmin Air Data Computer
Garmin Satellite Data Link
Garmin Display Unit
Garmin Engine/Airframe Unit
geographic
Garmin Flight Control
Garmin Integrated Avionics Unit
Global Navigation Satellite Landing
System
Garmin Audio Panel System
Greenwich Mean Time
Garmin Magnetometer Unit
ground
gallons per hour
Global Positioning System
Grid Minimum Off-Route Altitude;
one degree latitude by one degree
longitude in size and clears the
highest elevation reference point in
the grid by 1000 feet for all areas of
the grid
The velocity that the aircraft is
travelling relative to a ground
position
see Track
Garmin Reference System
Ground speed
Garmin Transponder
The direction an aircraft is pointed,
based upon indications from a
magnetic compass or a properly set
directional gyro
HF
Hold Terminating at Fix
HFOM
Horizontal Figure of Merit
Hg
mercury
HI
high
HI SENS
High Sensitivity
HM
Hold with Manual Termination
Horizontal Figure of Merit A measure of the uncertainty in the
aircraft’s horizontal position
hPa
hectopascal
HPL
Horizontal Protection Level
hr
hour
HSDB
High-Speed Data Bus
HSI
Horizontal Situation Indicator
HT
heat
HUL
Horizontal Uncertainty Level
Hz
Hertz
I
Inner Marker
IAF
Initial Approach Fix
IAT
Indicated Air Temperature
IAU
Integrated Avionics Unit
ICAO
International Civil Aviation
Organization
ICS
Intercom System
ID
Identification/Morse Code Identifier
IDENT, IDNT
identification
IF
Initial Fix
IFR
Instrument Flight Rules
IG
Imperial gallon
ILS
Instrument Landing System
IMC
Instrument Meteorological
Conditions
in
inch
INACTV
inactive
INC FUEL
increase fuel
IND
indicated
Indicated
Information provided by properly
calibrated and set instrumentation
on the aircraft panel
INFO
information
in HG
inches of mercury
INT
intersection(s)
INTEG
integrity (RAIM unavailable)
IrDA, IRDA
Infrared Data Association
FMS
FOB
FPL
fpm
FREQ
FRZ
FSS
ft
Fuel Flow
Course From Fix to Manual
Termination
Flight Management System
Fuel On Board
flight plan
feet per minute
frequency
freezing
Flight Service Station
foot/feet
The fuel flow rate, expressed in units
of fuel per hour
The total amount of usable fuel on
board the aircraft
SYSTEM
OVERVIEW
FM
541
SYSTEM
OVERVIEW
APPENDIX C
kHz
km
kt
kilohertz
kilometer
knot
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
L
left, left runway
LAT
latitude
LBL
label
lb
pound
LCD
Liquid Crystal Display
LCL
local
LED
Light Emitting Diode
Left Over Fuel On Board The amount of fuel remaining on
board after the completion of one or
more legs of a flight plan or directto
Left Over Fuel Reserve The amount of flight time remaining,
based on the amount of fuel on
board after the completion of one or
more legs of a flight plan or directto, and a known consumption rate
Leg
The portion of a flight plan between
two waypoints
LIFR
Low Instrument Flight Rules
LNAV
Lateral Navigation
LO
low
LOC
localizer
LOI
loss of integrity (GPS)
LON
longitude
LPV
Localizer Performance with Vertical
guidance
LRU
Line Replacement Unit
LT
left
LTNG
lightning
LVL
level
APPENDICES
ADDITIONAL
FEATURES
M
m
MAG
MAG VAR
MAHP
MAN IN
MAN SQ
MAP
MASQ
MAX
MAXSPD
MDA
INDEX
MET
METAR
542
Middle Marker
meter
Magnetic
Magnetic Variation
Missed Approach Hold Point
manifold pressure (inches Hg)
Manual Squelch
Missed Approach Point
Master Avionics Squelch
maximum
maximum speed (overspeed)
barometric minimum descent
altitude
manual electric trim
Meteorological Aviation Routine
MEPT
manual electric pitch trim
MFD
Multi Function Display
MGRS
Military Grid Reference System
MHz
megahertz
MIC
microphone
MIN
minimum
Minimum Safe Altitude Uses Grid MORAs to determine a
safe altitude within ten miles of the
aircraft present position
MKR
marker beacon
MOA
Military Operations Area
MOV
movement
mpm
meters per minute
MSA
Minimum Safe Altitude
MSAS
Multi-functional Satellite
Augmentation System
MSG
message
MSL
Mean Sea Level
MT
meter
mV
millivolt(s)
MVFR
Marginal Visual Flight Rules
N
NAV
NAVAID
NDB
NEXRAD
nm
NPT
NRST
north
navigation
NAVigation AID
Non-directional Beacon
Next Generation Radar
nautical mile(s)
nearest
O
OAT
OBS
OFST
OXY
Outer Marker
Outside Air Temperature
Omni Bearing Selector
offset
oxygen
P ALT
PA
PA
PASS
PC
PFD
PI
PIT, PTCH
POSN
PPM
P. POS
PRES, PRESS
PROC
pressure altitude
Passenger Address
Proximity Advisory
passenger(s)
personal computer
Primary Flight Display
Procedure Turn to Course Intercept
pitch
position
parts per million
Present Position
pressure
procedure(s), procedure turn
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX C
RAM
REF
REM
REQ
RES
REV
RF
RMI
RMT
RNG
RNWY
ROL
ROM
rpm
RST FUEL
RSV
SCIT
190-00552-05 Rev. A
TRG
TRK
TRSA
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
SID
SIGMET
Track Angle Error
APPENDICES
SD
sec
SEL, SLCT
SFC
SIAP
south
Selective Availability
Static Air Temperature
Satellite-Based Augmentation
System
Storm Cell Identification and
Tracking
Secure Digital
second(s)
select
surface
Standard Instrument Approach
Procedures
Standard Instrument Departure
Significant Meteorological
Information
ADDITIONAL
FEATURES
S
SA
SAT
SBAS
true
Traffic Advisory
Tactical Air Navigation System
Terminal Aerodrome Forecast
True Airspeed
Traffic Advisory System
Total Air Temperature
Terrain Awareness and Warning System
Terminal Control Area
Traffic Collision Avoidance System
telephone
temperature
terminal
Track Between Two Fixes
Temporary Flight Restriction
True Heading
Traffic Information System
Turbine Inlet Temperature
Track Angle Error
Terminal Maneuvering Area
Timer/Reference
topographic
Direction of aircraft movement relative
to a ground position; also ‘Ground
Track’
The angle difference between the
desired track and the current track
target
track
Terminal Radar Service Area
AFCS
RT
RVRSNRY
RX
T
TA
TACAN
TAF
TAS
TAS
TAT
TAWS
TCA
TCAS
TEL
TEMP
TERM
TF
TFR
T HDG
TIS
TIT
TKE
TMA
TMR/REF
Topo
Track
HAZARD
AVOIDANCE
right, right runway
radial
Receiver Autonomous Integrity
Monitoring
random access memory
reference
remaining (fuel remaining)
required
reserve (fuel reserve entered by
pilot)
reverse, revision, revise
Constant Radius Turn to Fix
Radio Magnetic Indicator
remote
range
runway
roll
read only memory
revolutions per minute
reset fuel
reserve (fuel reserve entered by
pilot)
right
reversionary
receive
FLIGHT
MANAGEMENT
R
RAD
RAIM
AUDIO PANEL
& CNS
quantity
simulator
slip/skid
symbol
speed
Special Position Identification
speaker
squelch
service
stall
Standard Terminal Arrival Route
statistics
standby
standard
Stormscope
Special Use Airspace
suspend
Synthetic Vision System
software
system
EIS
QTY
Sim
SLP/SKD
SMBL
SPD
SPI
SPKR
SQ
SRVC, SVC
STAL
STAR
STATS
STBY
STD
STRMSCP
SUA
SUSP
SVS
SW
SYS
FLIGHT
INSTRUMENTS
pounds per square inch
Procedure Turn
parallel track
Push-to-Talk
power
SYSTEM
OVERVIEW
psi
PT
PTK
PTT
PWR
543
truncated
total
procedure turn
transmit
UNAVAIL
USR
UTC
UTM/UPS
unavailable
user
Coordinated Universal Time
UniversalTransverse Mercator/ Universal
Polar Stereographic Grid
velocity (airspeed)
Heading Vector to Altitude
VOR approach
variation
Heading Vector to DME Distance
volts, direct current
vertical
A measure of the uncertainty in the
aircraft’s vertical position
Vertical Speed Required The vertical speed necessary to
descend/climb from a current
position and altitude to a defined
target position and altitude, based
upon current groundspeed
VFOM
Vertical Figure of Merit
VFR
Visual Flight Rules
VHF
Very High Frequency
VI
Heading Vector to Intercept
VLOC
VOR/Localizer Receiver
VM
Heading Vector to Manual Termination
VMC
Visual Meteorological Conditions
VNAV, VNV
vertical navigation
VOL
volume
VOR
VHF Omni-directional Range
VORTAC
very high frequency omnidirectional
range station and tactical air
navigation
VPL
Vertical Protection Level
VPROF
VNV profile, vertical profile
VPTH
VNV path, vertical path
VR
Heading Vector to Radial
VS
vertical speed
VSI
Vertical Speed Indicator
VSR
Vertical Speed Required
VTF
vector to final
W
WAAS
WGS-84
WPT
WW
WX
waypoint(s)
world wide
weather
XFER, XFR
XPDR
XTALK
XTK
transfer
transponder
cross-talk
cross-track
V, Vspeed
VA
VAPP
VAR
VD
Vdc
VERT
Vertical Figure of Merit
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
APPENDICES
TRUNC
TTL
TURN
TX
INDEX
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
APPENDIX C
544
watt(s), west
Wide Area Augmentation System
World Geodetic System - 1984
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX D
SYSTEM
OVERVIEW
FREQUENTLY ASKED QUESTIONS
FLIGHT
INSTRUMENTS
If a particular aspect of G1000 operational capability is not addressed by these commonly asked questions or in
the index, contact Garmin (see the copyright page or back cover for contact information) or a Garmin-authorized
dealer. Garmin is dedicated to supporting its products and customers.
What is SBAS?
EIS
The Satellite Based Augmentation System (SBAS) uses a system of ground stations to correct any GPS signal
errors. These ground stations correct for errors caused by ionospheric disturbances, timing, and satellite
orbit errors. It also provides vital integrity information regarding the health of each GPS satellite. The signal
correction is then broadcast through geostationary satellites. This correction information can then be received
by any SBAS-enabled GPS receiver.
AUDIO PANEL
& CNS
SBAS is designed to provide the additional accuracy, availability, and integrity necessary to enable users to rely
on GPS for all phases of flight.
FLIGHT
MANAGEMENT
There are several SBAS systems serving different parts of the world. The Wide Area Augmentation System
(WAAS) is currently available in the United States, including Alaska and Hawaii. The European Geostationary
Navigation Overlay Service (EGNOS) offers coverage of Europe, parts of the middle east and northern Africa. The
Multi-functional Satellite Augmentation System (MSAS) covers mainly Japan and parts of northern Australia.
How does SBAS affect approach operations?
HAZARD
AVOIDANCE
Both LNAV/VNAV and LPV approaches use the accuracy of SBAS to include vertical (glide path) guidance
capability. The additional accuracy and vertical guidance capability allows improved instrument approaches to
an expanded number of airports throughout the U.S.
AFCS
The implementation of LPV approaches further improves precision approach capabilities. LPV approaches
are designed to make full use of the improved GPS signal from the SBAS. This approach combines the LNAV/
VNAV vertical accuracy with lateral guidance similar to the typical Instrument Landing System (ILS). LPV
approaches allow lower approach minimums.
What is RAIM and how does it affect approach operations?
ADDITIONAL
FEATURES
RAIM is an acronym for Receiver Autonomous Integrity Monitoring. RAIM is a GPS receiver function that
performs the following functions:
• Monitors and verifies integrity and geometry of tracked GPS satellites
• Notifies the pilot when satellite conditions do not provide the necessary coverage to support a certain phase
of flight
APPENDICES
• Predicts satellite coverage of a destination area to determine whether the number of available satellites is
sufficient to satisfy requirements
NOTE: If RAIM is not predicted to be available for the final approach course, the approach does not become
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
INDEX
active, as indicated by the “RAIM not available from FAF to MAP” message and the LOI annunciation
flagging on the HSI.
545
SYSTEM
OVERVIEW
APPENDIX D
For RAIM to work correctly, the GPS receiver must track at least five satellites. A minimum of six satellites is
required to allow RAIM to eliminate a single corrupt satellite from the navigation solution.
FLIGHT
INSTRUMENTS
RAIM ensures that satellite geometry allows for a navigation solution calculation within a specified protection
limit (2.0 nm for oceanic and en route, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). The
G1000 System monitors RAIM and issues an alert message when RAIM is not available (see Appendix A).
Without RAIM, GPS position accuracy cannot be monitored. If RAIM is not available when crossing the FAF,
the pilot must fly the missed approach procedure.
Why might there be no approaches available for a flight plan?
EIS
Approaches are available for the final destination airport in a flight plan or as a direct-to (keep in mind
that some VOR/VORTAC identifiers are similar to airport identifiers). If a destination airport does not have a
published approach, the G1000 indicates “NONE” for the available procedures.
AUDIO PANEL
& CNS
What happens when an approach is selected? Can a flight plan with an approach, a departure, or an
arrival be stored?
FLIGHT
MANAGEMENT
When an approach, departure, or arrival is loaded into the active flight plan, a set of approach, departure,
or arrival waypoints is inserted into the flight plan, along with a header line showing the title of the selected
instrument procedure. The original enroute portion of the flight plan remains active, unless the instrument
procedure is activated. This may be done either when the procedure is loaded or at a later time.
HAZARD
AVOIDANCE
Flight plans can also be stored with an approach, a departure, or an arrival. Note that the active flight plan
is erased when the system is turned off. Also, the active flight plan is overwritten when another flight plan is
activated. When storing flight plans with an approach, a departure, or an arrival, the G1000 uses the waypoint
information from the current database to define the waypoints. If the database is changed or updated, the
G1000 System automatically updates the information, provided the procedure has not been modified. Should
an approach, departure, or arrival procedure no longer be available, the flight plan becomes locked until the
procedure is deleted from the flight plan.
AFCS
Can “slant Golf” (“/G”) be filed using the G1000?
ADDITIONAL
FEATURES
“/G” may be filed for a flight plan. GPS approaches are not to be flown with an expired database. See
the approved Airplane Flight Manual (AFM) as well as the Aeronautical Information Manual (AIM) for more
information.
What does the OBS Softkey do?
INDEX
APPENDICES
The OBS Softkey is used to select manual sequencing of waypoints. Activating OBS mode sets the current
active-to waypoint as the primary navigation reference and prevents the system from sequencing to the next
waypoint in a flight plan. When OBS mode is cancelled, automatic waypoint sequencing is continued, and
the G1000 automatically activates the next waypoint in the flight plan once the aircraft has crossed the present
active waypoint.
546
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX D
• Manual course change on HSI not possible
• Manually select course to waypoint from
HSI
• Always navigates ‘TO’ the active waypoint
• Indicates ‘TO’ or ‘FROM’ waypoint
• Must be in this mode for final approach
course
• Cannot be set for final approach course or
published holding patterns
FLIGHT
INSTRUMENTS
OBS
• Manual sequencing - ‘holds’ on selected
waypoint
SYSTEM
OVERVIEW
Normal (OBS not activated)
• Automatic sequencing of waypoints
EIS
When OBS mode is active, the G1000 allows the pilot to set a desired course to/from a waypoint using the
CRS/BARO Knob and HSI (much like a VOR).
AUDIO PANEL
& CNS
The most common application for using the OBS Softkey is the missed approach. The G1000 suspends
automatic waypoint sequencing (indicated by a ‘SUSP’ annunciation placed on the HSI) when the missed
approach point (MAP) is crossed. This prevents the G1000 from automatically sequencing to the missed
approach holding point (MAHP). During this time, the OBS Softkey designation changes to SUSP. Selecting
the SUSP Softkey reactivates automatic waypoint sequencing. The OBS Softkey then resumes its normal
functionality.
FLIGHT
MANAGEMENT
Why might the G1000 not automatically sequence to the next waypoint?
HAZARD
AVOIDANCE
The G1000 only sequences flight plan waypoints when automatic sequencing is enabled (i.e., no ‘OBS’ or
‘SUSP’ annunciation on the HSI). For automatic sequencing to occur, the aircraft must also cross the bisector of
the turn being navigated. The bisector is a line passing through the waypoint common to two flight plan legs
at an equal angle from each leg.
How can a waypoint be skipped in an approach, a departure, or an arrival?
AFCS
The G1000 allows the pilot to manually select any approach, departure, or arrival leg as the active leg of
the flight plan. This procedure is performed on the MFD from the Active Flight Plan Page by highlighting the
desired waypoint and selecting the ACT LEG Softkey then the ENT Key to approve the selection. The GPS
then provides navigation along the selected flight plan leg.
ADDITIONAL
FEATURES
When does turn anticipation begin?
The G1000 smooths adjacent leg transitions based on a normal 15° bank angle (with the ability to roll up to
30°) and provides three pilot cues for turn anticipation:
APPENDICES
• A waypoint alert (‘Next DTK ###° in # seconds’ or ‘Next HDG ###° in # seconds’) appears on the PFD 10
seconds before the turn point and flashes as it counts down to zero.
• A flashing turn advisory (‘Turn [right/left] to ###° in # seconds’) appears on the PFD 10 seconds before the
turn and flashes as it counts down to zero. ‘Turn [right/left] to ###° now’ or ‘Next [DTK/HDG] to ###° now’
is displayed when the pilot is to begin the turn and the HSI (GPS mode) automatically sequences to the next
DTK or HDG value.
INDEX
• The To/From indicator on the HSI flips momentarily to indicate that the midpoint of the turn has been
crossed.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
547
SYSTEM
OVERVIEW
APPENDIX D
When does the CDI scale change?
FLIGHT
INSTRUMENTS
Once a departure is activated, the G1000 Course Deviation Indicator (CDI) full scale deflection is set to 0.3
nm. The CDI scale changes to 1.0 nm (terminal mode) then ramps up to 2.0 nm (enroute mode) at 30 nm
from the departure airport. When 31 nm from the destination, the CDI scale smoothly transition from 2.0 nm
back to 1.0 nm (terminal mode). At 2.0 nm before the FAF during an active approach, the CDI scale transitions
down further based on the type of approach activated (LNAV, LNAV/VNAV, LPV). When a missed approach is
activated, the CDI is set to 0.3 nm. See the Flight Instruments Section for more details on CDI scaling.
Why does the HSI not respond like a VOR when OBS mode is active?
AUDIO PANEL
& CNS
EIS
Unlike a VOR, the CDI scale used on GPS equipment is based on the crosstrack distance to the desired
course, not on the angular relationship to the destination. Therefore, the CDI deflection on the GPS is constant
regardless of the distance to the destination and does not become less sensitive when further away from the
destination.
What is the correct missed approach procedure? How is the missed approach holding point selected?
FLIGHT
MANAGEMENT
To comply with TSO specifications, the G1000 does not automatically sequence past the MAP. The first
waypoint in the missed approach procedure becomes the active waypoint when the SUSP Softkey is selected
after crossing the MAP. All published missed approach procedures must be followed, as indicated on the
approach plate.
To execute the missed approach procedure prior to the MAP (not recommended), select the Active Flight Plan
Page and use the ACT LEG Softkey to activate the missed approach portion of the procedure.
HAZARD
AVOIDANCE
After a missed approach, how can the same approach be re-selected? How can a new approach be
activated?
NOTE: Do not attempt to reactivate the current approach prior to crossing the missed approach point
AFCS
(MAP). If an attempt to do so is made, an alert message “Are you sure you want to discontinue the current
approach?” appears. The G1000 directs the pilot back to the transition waypoint and does not take into
consideration any missed approach procedures, if the current approach is reactivated.
ADDITIONAL
FEATURES
After flying the missed approach procedure, the pilot may reactivate the same approach for another attempt by
pressing the PROC Key. Once the clearance is given for another attempt, activate the approach by highlighting
‘ACTIVATE APPROACH’ using the large FMS Knob and pressing the ENT Key. The G1000 provides navigation
along the desired course to the waypoint and rejoins the approach in sequence from that point.
APPENDICES
To activate a new approach for the same airport, select the new procedure by pressing the PROC Key. Choose
‘SELECT APPROACH’, select the desired approach from the list shown, and press the ENT Key. Select the
desired transition, then activate the approach using the ENT Key.
INDEX
To activate a new approach to a different airport, press the Direct-to Key and select the desired airport using
the FMS Knobs. Press the ENT Key to accept the selected airport, then follow the steps in the preceding
paragraph to select an approach for the new airport.
548
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX E
SYSTEM
OVERVIEW
GENERAL TIS INFORMATION
INTRODUCTION
FLIGHT
INSTRUMENTS
NOTE: Aircraft without an operating transponder are invisible to TIS.
EIS
The Traffic Information Service (TIS) provides traffic advisory information to non-TAS/TCAS-equipped
aircraft. TIS is a ground-based service providing the relative locations of all ATCRBS Mode-A and Mode-C
transponder equipped aircraft within a specified service volume. The TIS ground sensor uses real-time track
reports to generate traffic notification. The G1000 System displays TIS traffic information on the Traffic Map
Page of the MFD. TIS information may also be displayed for overlay on the MFD Navigation Map Page, as
well as on the PFD Inset Map. Surveillance data includes all transponder-equipped aircraft within the coverage
volume. The G1000 System displays up to eight traffic targets within a 7.5 nm radius, from 3,000 feet below,
to 3,500 feet above the requesting aircraft.
AUDIO PANEL
& CNS
TIS VS. TAS/TCAS
FLIGHT
MANAGEMENT
The Traffic Information System (TIS) requires contact with a ground station through a data link radio in
order to receive traffic information. Traffic Advisory (TAS) and Traffic Collision Avoidance Systems (TCAS) are
self-contained. TAS/TCAS uses an airborne interrogator with a half-second update rate, while TIS utilizes the
terminal Mode-S ground interrogator and accompanying data link to provide a five-second update rate. TIS
and TAS/TCAS have similar ranges.
HAZARD
AVOIDANCE
TIS LIMITATIONS
NOTE: TIS is not intended to be used as a collision avoidance system and does not relieve the pilot of the
responsibility to “see and avoid” other aircraft. TIS should not be used for avoidance maneuvers during
instrument meteorological conditions (IMC) or when there is no visual contact with the intruder aircraft.
AFCS
NOTE: Refer to the TIS Limitations section of the Aeronautical Information Manual (AIM) for a more
comprehensive explanation of limitations and anomalies associated with TIS.
ADDITIONAL
FEATURES
APPENDICES
TIS relies on surveillance of the Mode-S radar system, which is a “secondary surveillance” radar system
similar to that used by ATCRBS. Many limitations are inherent in secondary radar surveillance. Information
provided by TIS is neither better nor more accurate than the information used by ATC. TIS is intended only
to assist in visual acquisition of other aircraft in visual meteorological conditions (VMC). While TIS is a useful
aid for visual traffic avoidance, system limitations must be considered to ensure proper use. No recommended
avoidance maneuvers are given, nor authorized, as a direct result of a TIS intruder display or TIS advisory.
• TIS operation may be intermittent during turns or other maneuvering.
INDEX
• TIS is dependent on two-way, line-of-sight communications between the aircraft and the Mode-S radar
antenna. Whenever the structure of the aircraft comes between the transponder antenna and the groundbased radar antenna, the signal may be temporarily interrupted.
• Other limitations and anomalies associated with TIS are described in the AIM.
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
549
SYSTEM
OVERVIEW
APPENDIX E
WARNING: Garmin is not responsible for Mode S geographical coverage. Operation of the ground stations
FLIGHT
INSTRUMENTS
is the responsibility of the FAA. Refer to the AIM for a Terminal Mode S radar site map.
NOTE: TIS is unavailable at low altitudes in many areas of the United States. This is often the case in
mountainous regions.
AUDIO PANEL
& CNS
EIS
TIS information is collected during a single radar sweep. Collected information is then sent through the
Mode S uplink on the next radar sweep. Because of this, the surveillance information is approximately five
seconds old. TIS ground station tracking software uses prediction algorithms to compensate for this delay.
These algorithms use track history data to calculate expected intruder positions consistent with the time of
display. Occasionally, aircraft maneuvering may cause variations in this calculation and create slight errors on
the Traffic Map Page. Errors affect relative bearing information and target track vector. This can cause a delay in
the displayed intruder information. However, intruder distance and altitude typically remain relatively accurate
and may be used to assist in spotting traffic.
The following errors are common examples:
FLIGHT
MANAGEMENT
• When the client or intruder aircraft maneuvers excessively or abruptly, the tracking algorithm may report
incorrect horizontal position until the maneuvering aircraft stabilizes.
• When a rapidly closing intruder is on a course that intercepts the client aircraft course at a shallow angle
(either overtaking or head-on) and either aircraft abruptly changes course within 0.25 nm, TIS may display
the intruder aircraft on the incorrect side of the client aircraft.
HAZARD
AVOIDANCE
These are rare occurrences and are typically resolved within a few radar sweeps once the client/intruder
aircraft course stabilizes.
AFCS
Pilots using TIS can provide valuable assistance in the correction of malfunctions by reporting observations
of undesirable performance. Reports should identify the time of observation, location, type and identity of
the aircraft, and describe the condition observed. Reports should also include the type of transponder and
transponder software version. Since TIS performance is monitored by maintenance personnel, not ATC,
malfunctions should be reported in the following ways:
• By telephone to the nearest Flight Service Station (FSS) facility
INDEX
APPENDICES
ADDITIONAL
FEATURES
• By FAA Form 8000-7, Safety Improvement Report (postage-paid card can be obtained at FAA FSSs, General
Aviation District Offices, Flight Standards District Offices, and General Aviation Fixed Base Operators).
550
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX F
SYSTEM
OVERVIEW
MAP SYMBOLS
AIRPORTS
BASEMAP
Item
Symbol
Unknown Airport
Interstate Highway
Non-towered, Non-serviced Airport
State Highway
FLIGHT
INSTRUMENTS
Item
Symbol
EIS
US Highway
Towered, Non-serviced Airport
National Highway
Non-towered, Serviced Airport
AUDIO PANEL
& CNS
City
Towered, Serviced Airport
State/Province Border
Restricted (Private) Airport
Heliport
FLIGHT
MANAGEMENT
International Border
Road
Railroad
NAVAIDS
Symbol
HAZARD
AVOIDANCE
Item
Latitude/Longitude
Intersection
LOM (compass locator at outer marker)
AIRSPACE BOUNDARIES
Mode C Tower Area
VOR/ILS
VORTAC
Warning Area Prohibited Area
Alert Area
Restricted Area
Caution Area Training Area
Danger Area
Unknown Area
Class C
Terminal Radar Service Area
Mode C Area
APPENDICES
TACAN
ADDITIONAL
FEATURES
VOR/DME
Symbol
AFCS
VOR
Item
ICAO Control Area
Class B Airspace
NDB (non-directional radio beacon)
Military Operations Area (MOA)
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
551
SYSTEM
OVERVIEW
APPENDIX F
HAZARD AVOIDANCE FEATURES
FLIGHT
INSTRUMENTS
Feature
Symbol
Item
Terrain display enabled
Non-threat Traffic
Traffic display enabled
Proximity Advisory (not used with TIS)
NEXRAD display enabled
Traffic Advisory, Out of Range
Cloud Top display enabled
EIS
TRAFFIC
Symbol
Traffic Advisory
AUDIO PANEL
& CNS
Echo Top display enabled
XM Lightning display enabled
MISCELLANEOUS
Item
Cell Movement display enabled
FLIGHT
MANAGEMENT
SIGMETs/AIRMETs display enabled
METARs display enabled
HAZARD
AVOIDANCE
City Forecast display enabled
Surface Analysis display enabled
APPENDICES
ADDITIONAL
FEATURES
AFCS
Freezing Levels display enabled
ARTCC Frequency or FSS Frequency
Map Pointer (when panning)
Elevation Pointer
(on Topography Scale when panning)
Measuring Pointer
Wind Vector
Winds Aloft display enabled
Overzoom Indicator
County Warnings display enabled
User Waypoint
Cyclone Warnings display enabled
Vertical Navigation Along Track Waypoint
Loss of hazard avoidance feature
(loss of GPS position)
Parallel Track Waypoint
Turbulence
Unanchored Flight Path Waypoint
Icing Potential
PIREPs
Symbol
Top of Descent (TOD)
Bottom of Descent (BOD)
INDEX
AIREPs
Navigating using Dead Reckoning
552
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
APPENDIX F
SYSTEM
OVERVIEW
OBSTACLE DATABASE
Unlighted Obstacle
Lighted Obstacle
< 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL
Obstacle Location
FLIGHT
INSTRUMENTS
Red obstacle is above or within 100 ft
below the aircraft altitude
Yellow obstacle is between 100 ft and
1000 ft below the aircraft altitude
EIS
Gray obstacle is more than 1000 ft
below aircraft altitude
AUDIO PANEL
& CNS
Table F-1 Obstacle Colors
TERRAIN AVOIDANCE COLORS AND SYMBOLS
FLIGHT
MANAGEMENT
Terrain Above Aircraft Altitude
Aircraft Altitude
100 ft Threshold
Red terrain is above
or within 100 ft below
the aircraft altitude
HAZARD
AVOIDANCE
1000 ft
Yellow terrain is between 100 ft and 1000 ft below the aircraft altitude
Black terrain is more than 1000 ft below the aircraft altitude
AFCS
Figure F-1 Terrain Altitude/Color Correlation
ADDITIONAL
FEATURES
Figure F-2 TAWS-B and Terrain-SVS
Potential Impact Points
APPENDICES
INDEX
190-00552-05 Rev. A
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
553
INDEX
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
SYSTEM
OVERVIEW
APPENDIX F
Blank Page
554
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
INDEX
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
EIS
190-00552-05 Rev. A
Altitude Reference----------------------------- 379, 380, 388
Ammeter------------------------------------------------------ 86
Annunciations
AFCS Status-----------------------------------------------522
G1000 System--------------------------------------------- 17
Test tone---------------------------------------------- 43, 504
Annunciations, softkey-------------------------------------- 75
Annunciation Window-------------------------------------- 75
Annunciator lights------------------------------------------128
ANT/BFO-----------------------------------------------------121
AOPA--------------------------------------421, 479, 531, 532
AOPA Airport Directory------------------------------ 480, 481
AP-------------------------------------------------------------522
Approach-----------------------------------------------------546
Activating-------------------------------------------------243
ILS----------------------------------------------------------412
Loading--------------------------------------- 211, 240, 242
Missed-----------------------------------------------------416
Removing--------------------------------------------------243
WAAS------------------------------------------------------414
Approach box-----------------------------------------------465
Approach Mode, AFCS------------------------------ 412, 414
Approach Mode (GPS, VAPP, LOC)-----------------------398
APR softkey------------------------------------------- 242, 248
Arrival procedure-196, 209, 237, 238, 239, 242, 261, 263,
272
Assist, engine leaning---------------------------------- 90–92
Attitude and Heading Reference System (AHRS)----4, 13,
16–17
Attitude Indicator-----------------------------------50, 54–55
Audio alerting system------------------------------- 503, 504
Audio Panel------------------------------------------------ 2, 15
Audio panel controls
SPKR-------------------------------------------------------128
Audio panel fail-safe operation---------------------------135
Automatic Flight Control System (AFCS)------ 1, 371–420
Alerts and annunciations------------------------ 419–420
Controls-------------------------------------------- 372–373
Example procedures------------------------------ 403–410
Automatic squelch------------------------------------------109
Autopilot--------------------------------- 371, 401–402, 522
Autopilot disconnect-------------------------- 373, 392, 402
Auto-tuning--------------------------------------------------117
Auto-tuning, COM------------------------------------------104
Auto-tuning, NAV-------------------------------------------113
Auto Zoom---------------------------------------------------143
Auxiliary Pages (AUX)--------------------------------------- 33
AUX - System Status Page-438, 440, 460, 461, 476, 477,
478, 480
Aviation Symbols------------------------------------- 154, 196
FLIGHT
INSTRUMENTS
Activate a Flight Plan---------------------------------------214
Active channel-----------------------------------------------484
Active database-------------------------------------- 528, 529
Active frequency------------------------------------- 100, 110
ADF---------------------------------------------------------119
AC-U-KWIK-------------------------------421, 479, 531, 532
ADF
ADF mode------------------------------------------ 119, 121
ANT mode-------------------------------------------------121
Volume-----------------------------------------------------119
ADF audio----------------------------------------------------111
ADF/BFO-----------------------------------------------------121
ADF/DME tuning--------------------------------------------122
ADF frequency tuning--------------------------------------120
ADF volume--------------------------------------------------121
AFCS Status Box--------------------------------------- 50, 375
AHRS--------------------------------------------------- 517, 518
Aileron trim-----------------------------------------------84, 86
Air Data Computer (ADC)------------------------------------ 3
AIRMET-------------------------------------------------------302
Airport
Information-----------------------------------------------174
Nearest----------------------------------------------------- 41
Airport Directory-------------------------421, 479, 480, 531
Airspace alerts-----------------------------------------------189
Airspace Alerts----------------------------------------------190
Airspeed Indicator----------------------------------50, 52–53
Airspeed Reference---------------------------------- 382, 419
Airways
Collapsed--------------------------------------------------227
Expanded--------------------------------------------------227
Alerting system----------------------------------------------503
Alerting System---------------------------------------------507
Alert levels---------------------------------------------------504
Alerts---------------------------------------------------------503
Aircraft-----------------------------------------------------506
Airspace---------------------------------------------------- 38
Arrival------------------------------------------------------- 39
Audio voice------------------------------------------ 39, 509
Alerts Window------------------------------------------------ 75
Along Track Offset------------------------------------------219
ALT------------------------------------------------------------276
Alternator current (ALT AMPS)----------------------------- 86
Altimeter---------------------------------------------50, 55–56
Altimeter barometric setting---------------------------50, 56
Altitude alerting---------------------------------------------- 78
Altitude buffer------------------------------------------------ 39
Altitude capture---------------------------------------------388
Altitude constraints-----------------------------------------230
Altitude Hold Mode (ALT)----------------------------------379
SYSTEM
OVERVIEW
A
I-1
SYSTEM
OVERVIEW
INDEX
B
FLIGHT
INSTRUMENTS
Backcourse Mode-------------------------------------------400
Backlighting-------------------------------------------------- 47
Barometric setting, Altimeter---------------------------50, 56
Battery current (BATT AMPS)------------------------------ 86
Bearing/distance, measuring------------------------------148
Bearing pointer----------------------------------------------- 62
Bearing source----------------------------------------------- 63
Bus voltage (BUS VOLTS)----------------------------------- 86
C
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
EIS
Calibrated Airspeed-----------------------------------------245
Carbon monoxide detection-------------------------------- 88
CAUTION-----------------------------------------------------504
CDI---------------------------- 239, 252, 263, 271, 278, 520
Chart Not Available---------------------------------- 443, 463
Chart options----------------------------------------- 451, 470
Chart setup box-------------------------------------- 457, 474
ChartView--------------------------------------- 421, 441, 460
ChartView database----------------------------------------460
ChartView functions----------------------------------------442
ChartView plan view---------------------------------------452
ChartView profile view-------------------------------------453
ChartView softkeys-----------------------------------------442
Checklists--------------------------------------------- 489–490
Checklist softkeys-------------------------------------------489
Closest Point-------------------------------------------------227
COM channel spacing--------------------------------------108
COM frequency box----------------------------------- 95, 100
Command Bars, flight director----------------------------376
Communication (COM) Frequency Box------------------- 50
COM radio
Channel spacing------------------------------------------ 41
COM tuning failure-----------------------------------------135
Controls
PFD/MFD--------------------------------------------- 7–8, 30
Softkeys------------------------------------------------ 18–21
Control Wheel Steering (CWS)--------------------- 373, 402
Copy a Flight Plan------------------------------------------214
Course Deviation Indicator (CDI)-----------------41, 64–65
Changing scale-------------------------------------------548
Course To Altitude------------------------------------------244
Cylinder Head Temperature (CHT °F)------------ 84, 87, 89
D
INDEX
Data Bar fields, MFD---------------------------------------- 40
Databases------------------------------------------ 13, 43, 527
Database Synchronization-------------------- 527, 532, 534
Data entry------------------------------------------------ 29–30
Data Link Receiver--------------------------------------------- 4
Datalink receiver troubleshooting------------------------500
I-2
Data logging-------------------------------------------------493
Data Logging----------------------------------------- 421, 492
Date and time------------------------------------------------ 36
Day/Night views-------------------------------------- 457, 474
Day view----------------------------------457, 458, 474, 475
DB Mismatch------------------------------------------------527
Dead Reckoning---------------------------------------------- 80
Decision Height (DH)---------------------------------------- 79
Declutter, display--------------------------------------------- 81
Declutter EIS----------------------------------------------23, 89
Declutter maps-------------------------------------------19, 23
Delete Flight Plans------------------------------------------214
Deleting an entire airway--------------------------- 216, 217
Deleting an entire procedure----------------------- 216, 217
Deleting an individual waypoint------------------- 215, 216
Deleting Flight Plan Items---------------------------------215
Density Altitude---------------------------------------------247
Departure
Select------------------------------------234, 237, 240, 243
Timer-------------------------------------------------------- 46
Departure procedure--------------------207, 221, 234, 236
Departure Time----------------------------------------------245
Dilution of Precision (DOP)--------------------------------- 25
Direct-to-- 167, 191, 192, 193, 194, 195, 228, 229, 261,
263, 278
Display backup------------------------------------ 15, 97, 135
Display controls------------------------------------------- 7–14
DME
HOLD mode-----------------------------------------------122
NAV1 mode-----------------------------------------------122
NAV2 mode-----------------------------------------------122
Tuning mode--------------------------------------- 119, 122
DME audio---------------------------------------------------111
DME information-----------------------------------------62, 63
Dual navigation database---------------------------------528
E
Electronic checklists- 421–422, 489, 489–490, 490, 491
Elevator trim----------------------------------------------84, 86
Emergency checklist----------------------------------------491
Emergency frequency---------------------------------------135
Endurance, calculated (ENDUR)-----------------------86, 88
Engine Airframe Unit------------------------------------------ 3
Engine Indication System (EIS)------------------------ 83–92
Engine leaning assist----------------------------------- 90–92
Engine Manifold Pressure (MAN IN HG)-------------84, 86
Entering Flight ID-------------------------------------------123
Entertainment inputs---------------------------------------133
Estimated Position Error (EPE)----------------------------- 25
EVS------------------------------------------------------------496
Exhaust Gas Temperature (EGT °F)---- 84, 87, 89, 90–91
Export Flight Plan-------------------------------------------521
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
INDEX
I
ID indicator--------------------------------------------------113
ILS approach-------------------------------------------------412
Import Flight Plan-------------------------------------------521
Indicated Altitude-------------------------------------------245
INFO box-----------------------------------------------------466
Integrated Avionics Unit (IAU)------------------------------- 3
Intercom system (ICS)--------------------------------------133
Intersection
Information---------------------------------------- 175–176
Inverting a flight plan--------------------------------------214
IOI------------------------------------------338, 349, 523, 524
FLIGHT
MANAGEMENT
J
HAZARD
AVOIDANCE
Jeppesen aviation database-------------------------------527
L
Land Symbols------------------------------------------------153
Line Replaceable Units (LRU)-----------------------------2–5
LNAV----------------------------------------------------------252
Log File-------------------------------------------------------493
Logging Data------------------------------------------------492
LO SENS------------------------------------------------------118
Low Altitude Annunciation--------------------------------- 78
LPV----------------------------------------------------- 252, 278
LPV approach------------------------------------------------403
AFCS
ADDITIONAL
FEATURES
M
Manual Electric Trim (MET)------------------- 371, 373, 401
Map Pages (MAP)------------------------------------------- 32
Map Panning------------------------------------------------145
Map symbols------------------------------------------------551
Marker beacon----------------------------------------------118
Marker Beacon Annunciations----------------------------- 76
MASQ processing-------------------------------------------- 93
Measurement units, changing displayed----------------- 37
Menus--------------------------------------------------------- 29
INDEX
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
APPENDICES
190-00552-05 Rev. A
Heading------------------------------------------------------- 50
Heading Select Mode (HDG)----------------------- 395, 404
HI SENS-------------------------------------------------------118
Horizontal Situation Indicator (HSI)--------------50, 59–70
HSI double green arrow------------------------------------110
HSI magenta arrow-----------------------------------------110
HSI single green arrow-------------------------------------110
AUDIO PANEL
& CNS
GDL 69/69A-------------------------------------------------284
geodetic sea level------------------------------ 324, 332, 342
GFC 700 AFCS--------------------------------------- 371–420
Glidepath-----------------------------------------------------276
Glidepath Indicator------------------------------------------ 58
Glidepath Mode (GP)-------------------------- 389, 398, 414
Glideslope----------------------------------------------------276
Glideslope Indicator----------------------------------------- 58
Glideslope Mode (GS)------------------------- 373, 391, 412
Global Positioning System (GPS)
Navigation----------------------------------------- 191–282
Receiver information--------------------------------- 24–26
Go Around Mode (GA)----------------- 373, 392, 416–417
H
EIS
G
GPS Window-------------------------------------------------533
GSL----------------------------------------------- 324, 332, 342
GTX 33 Transponder----------------------------------------123
FLIGHT
INSTRUMENTS
FD-------------------------------------------------------------522
Field of View (SVS)------------------------------------------165
Flight director-----------------------------------371, 374–375
Pitch modes---------------------------------------- 377–383
Roll modes------------------------------------------------393
Flight Level Change Mode (FLC)------382, 408, 410, 419
Flight plan
Closest point to reference------------------------------227
Storing-----------------------------------------------------546
Flight Plan Pages (FPL)-------------------------------------- 34
Flight timer---------------------------------------------------- 45
FliteCharts-------------------------------------------- 421, 462
FliteCharts®-------------------------------------------------421
FliteCharts cycle---------------------------------------------477
FliteCharts expiration--------------------------------------477
FliteCharts functions---------------------------------------462
FPA----------------------------------------------------- 230, 268
Frequency
Nearest----------------------------------------------------187
Frequency spacing------------------------------------------108
Frequency transfer arrow----------------------------------101
Frequently asked questions--------------------------------545
Fuel
Efficiency--------------------------------------------------247
Endurance-------------------------------------------------247
Remaining-------------------------------------------------247
Required---------------------------------------------------247
Fuel calculations--------------------------------------------- 88
Fuel Flow (FFLOW GPH)--------------------------- 84, 87, 90
Fuel flow totalizer-------------------------------------------- 88
Fuel on Board-----------------------------------------------247
Fuel Quantity (FUEL QTY GAL)-------------------------84, 87
Fuel remaining, calculated (GAL REM)---------------86, 88
Fuel Statistics------------------------------------------------247
Fuel used, calculated (GAL USED)---------------------86, 88
SYSTEM
OVERVIEW
F
I-3
SYSTEM
OVERVIEW
INDEX
AUDIO PANEL
& CNS
EIS
FLIGHT
INSTRUMENTS
Message advisories--------- 504, 509, 510, 517, 518, 519
MET-----------------------------------------------------------522
METAR--------------------------------------------------------303
Metric display, Altimeter------------------------------- 55–56
MFD Data Bar fields----------------------------------------- 40
MFD/PFD Control Unit------------------------10–11, 30–31
Minimum Descent Altitude (MDA)------------------------ 79
Missed Approach-----196, 244, 249, 252, 277, 278, 416
Mistrim-------------------------------------------------------522
Mode S------------------------------------------------ 123, 124
Morse code identifier---------------------------------------113
Multi Function Display (MFD)-------------------------------- 2
Controls---------------------------------------------------7–8
Softkeys----------------------------------------------------- 23
Music 1-------------------------------------------------------133
Music 2-------------------------------------------------------133
N
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
National Weather Service----------------------------------311
NAV1 audio--------------------------------------------------111
NAV2 audio--------------------------------------------------111
NAV frequency box------------------------------------------ 95
Navigation database-------------------------------- 230, 231
Navigation Map---------------------------------------------193
Navigation Mode, AFCS----------------------------- 406–407
Navigation mode selection--------------------------------110
Navigation Mode (VOR, GPS, LOC, BC)-----------------396
Navigation (NAV) Frequency Box-------------------------- 50
Navigation source-------------------------------------- 64–66
Navigation Status Box-------------------------------------- 50
Nav radio selection-----------------------------------------110
Nearest
Airports---------------------------------------- 41, 187–190
VOR------------------------------------------------- 187–188
nearest airport---------------------------------- 171, 172, 173
Nearest Airport-------------------- 171, 172, 173, 174, 242
Minimum Runway Length------------------------------174
Surface Matching----------------------------------------174
Nearest Airports Page------------------------- 172, 173, 174
Nearest Pages (NRST)--------------------------------------- 33
Night view--------------------------------457, 458, 474, 475
Non-path descent------------------------------387, 410–411
Normal display operation----------------------------------- 14
APPENDICES
O
INDEX
OBS Mode----------------------------------------------- 69–70
Obstacles---------------------------------------------- 512, 515
Oil Pressure (OIL PSI)------------------------------------84, 86
Oil Temperature (OIL °F)--------------------------------84, 86
Omni Bearing Selector (OBS)----------------------- 546–547
Other Statistics--------------------------------------- 245, 247
Outside Air Temperature (OAT)------------------------50, 71
I-4
Overspeed protection, autopilot--------------------------419
Oxygen Outlet Pressure (OXY OUTLET PSI)-------------- 86
Oxygen Quantity (OXY QTY PSI)--------------------------- 86
P
Page menus--------------------------------------------------- 29
Parallel Track------------------------------------------ 220, 221
Passenger address------------------------------------------131
PA system----------------------------------------------------131
Pitch Hold Mode (PIT)------------------------------- 378, 419
Pitch indication----------------------------------------------- 54
Pitch modes, flight director------------------------- 377–383
Pitch Reference----------------------------------------------378
Power-up page----------------------------------------------489
Power-up, system-------------------------------------------- 13
Primary Flight Display (PFD)---------------------------------- 2
Controls---------------------------------------------------7–8
Softkeys------------------------------------------------ 18–20
Procedure examples, AFCS------------------------- 403–410
Procedure Loading Pages (PROC)------------------------- 34
Profile Path--------------------------------------------------330
Profile View--------------------------------------------------329
Q
Quick tuning 121.500 MHz-------------------------------103
R
RAIM---------------------------------------239, 249, 250, 251
Range---------------------------------------------------------163
Range, calculated (RANGE NM)--------------------------- 86
Receiver Autonomous Integrity Monitoring (RAIM)-26–27,
249, 545
Required Vertical Speed------------------------------------269
Required Vertical Speed Indicator------------------------269
ROC----------------------------------------338, 349, 523, 524
Roll Hold Mode (ROL)------------------------------- 373, 394
Roll modes, flight director-------------------------- 393–396
Roll Reference-----------------------------------------------394
Runway
Minimum length------------------------------------------- 41
Surface------------------------------------------------------ 41
RVSI---------------------------------------------------- 269, 270
RX Indicator-------------------------------------------------101
S
SafeTaxi------------------------------------------ 421, 435, 438
SafeTaxi®----------------------------------------------------421
SafeTaxi database-------------------------------------------439
SBAS-------------------------------- 249, 250, 251, 515, 545
Scheduler----------------------------------------421–422, 487
Secure Digital (SD) card-------------------------12, 489, 527
Selected Altitude----------------------50, 78, 384, 388, 404
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
INDEX
SVS------------------------------------------------------------520
SVS troubleshooting----------------------------------------498
Symbols, map------------------------------------------------551
Synthetic vision (SVS)------------------------------- 421, 422
System annunciations------------------------------- 503, 507
System Annunciations--------------------------------------- 17
System power-up-------------------------------------------- 13
System Setup Page------------------------------------------ 35
System Status Page------------------------------------------ 42
System time-----------------------------------------------36, 50
FLIGHT
INSTRUMENTS
T
EIS
Tachometer (RPM)---------------------------------------84, 86
TAF------------------------------------------------------------303
TAWS---------------------------------------------------- 77, 524
TAWS-B-------------------------------------------------------342
Terminal procedures charts------------------------- 443, 463
Terrain--------------------------------------------------------511
Color indications-----------------------------------------553
Terrain Awareness and Warning System (TAWS)-------- 77
Terrain Proximity--------------------------------------------324
TERRAIN-SVS------------------------------------------- 77, 332
Timer
Departure--------------------------------------------------- 46
Flight-------------------------------------------------------- 45
Timer, PFD generic------------------------------------------- 43
Time, system-------------------------------------------------- 36
TIS-------------------------------------------------------------356
TOD---------------------------------------------- 268, 269, 275
TOPO DATA------------------------------------- 150, 151, 160
Top of Descent--------------------------------------- 268, 269
TOPO SCALE-------------------------------------------------152
Track----------------------------------------------------------- 59
Track indicator------------------------------------------------ 59
Traffic advisory (TA)------------------------------------------ 76
Traffic Information Service (TIS)-------------------- 549–550
Voice alerts------------------------------------------------- 76
Transponder----------------------------------------------------- 3
Transponder code entry------------------------------------126
Transponder data box-----------------------------------93, 95
Transponder ground mode--------------------------------124
Transponder mode field----------------------------- 124, 125
Transponder softkeys---------------------------------------124
Transponder standby mode-------------------------------125
Transponder Status Box------------------------------------- 50
Trend Vector
Turn Rate--------------------------------------------------- 62
Trim--------------------------------------------------------84, 86
Trim adapter-------------------------------------------------401
Trip Planning------------------------------------ 245, 246, 247
Trip Statistics------------------------------------------ 246, 247
True Airspeed-------------------------------------- 50, 52, 247
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
AUDIO PANEL
& CNS
190-00552-05 Rev. A
SYSTEM
OVERVIEW
Selected Altitude Bug--------------------------------------- 50
Selected Altitude Capture Mode (ALTS)---------- 380, 384
Selected Altitude Intercept Arc----------------------------166
Selected Course--------------------------- 60, 397, 399, 400
Selected heading--------------------------------------------- 60
Selecting a COM radio-------------------------------------100
Sequencing, automatic-------------------------------------547
Sequencing waypoints, suspend--------------------------- 70
Service class-------------------------------------------------483
Servos------------------------------------------------------4, 401
SIGMET-------------------------------------------------------302
SiriusXM
Radio------------------------------------------------ 284, 482
Receiver troubleshooting-------------------------------500
SiriusXM channel list---------------------------------------484
SiriusXM radio entertainment-----------------------------133
SiriusXM radio volume-------------------------------------486
SiriusXM Satellite Radio------------------- 4, 482, 484, 486
SiriusXM Weather-------------------------------------------284
Airrep------------------------------------------------------315
Cell Movement-------------------------------------------301
City Forecast----------------------------------------------305
Cloud Tops------------------------------------------------299
County Warning------------------------------------------311
Cyclone (Hurricane)--------------------------------------312
Echo Tops--------------------------------------------------298
Freezing Level---------------------------------------------307
Icing (CIP & SLD)-----------------------------------------313
Lightning--------------------------------------------------300
NEXRAD---------------------------------------------------293
Limitations------------------------------------------------295
Pirep--------------------------------------------------------315
PIREPs-----------------------------------------------------315
Surface Analysis------------------------------------------305
Turbulence-------------------------------------------------314
Winds Aloft------------------------------------------------308
Slip/Skid Indicator----------------------------------------50, 54
Softkey annunciations--------------------------------------- 75
Softkeys
EIS---------------------------------------- 23, 83, 86, 88, 90
MFD--------------------------------------------------------- 23
PFD-------------------------------------------------18–20, 50
Speaker-------------------------------------------------------128
Split COM operation----------------------------------------132
Standby frequency----------------------------- 100, 104, 110
ADF---------------------------------------------------------119
Standby frequency field------------------------------------100
Standby Navigation Database--------------------- 529, 531
Stereo headsets---------------------------------------------128
Stuck microphone-------------------------------------------135
Sunrise--------------------------------------------------------246
Sunset--------------------------------------------------------246
I-5
SYSTEM
OVERVIEW
INDEX
FLIGHT
INSTRUMENTS
True Airspeed (TAS)-----------------------------------------517
Turbine Inlet Temperature (TIT °F)---------------- 84, 87, 92
Turn anticipation--------------------------------------------547
Turn Rate Indicator--------------------------------------50, 62
TX indicator--------------------------------------------------101
U
Unable to display chart----------------------------- 443, 463
Updating Garmin databases------------------------------439
Updating Jeppesen databases----------------------------460
EIS
V
WARNING----------------------------------------------------504
Waypoint
Automatic sequencing----------------------------------547
Skipping---------------------------------------------------547
Waypoint Pages (WPT)-------------------------------------- 32
Waypoint Selection Submenu--- 192, 198, 199, 203, 249
Wind--------------------------------------------------- 140, 162
Wings level------------------------------------------- 392, 394
Z
Zoom
Auto--------------------------------------------------------143
APPENDICES
ADDITIONAL
FEATURES
AFCS
HAZARD
AVOIDANCE
FLIGHT
MANAGEMENT
AUDIO PANEL
& CNS
VDI----------------------------------------------------- 269, 270
Vertical deviation-------------------------------------------386
Vertical deviation guidance-------------------------------231
Vertical Deviation Indicator-------------------------------269
Vertical Deviation Indicator (VDI)-------------------------- 58
Vertical navigation------------------------------------------230
Direct-to---------------------------------------------------229
Vertical Navigation (VNV)
Flight control--------------------------------------- 384–388
Vertical Path Tracking Mode (VPTH)--------384–385, 409
Vertical speed guidance-----------------------------------231
Vertical Speed Indicator (VSI)--------------------------50, 57
Vertical Speed Mode (VS)----------------------------------381
Vertical Speed Reference----------------------------------381
VFR code-----------------------------------------------------127
Video settings-----------------------------------------------495
Video source-------------------------------------------------496
Video system----------------------------------------- 421, 494
VNAV-------------------------------------------------- 195, 520
VNV---------------------------------------------------- 268, 544
VNV guidance
Disabling--------------------------------------------------228
Enabling---------------------------------------------------228
VNV indications, PFD---------------------------------------- 74
VNV Target Altitude--------------------------------- 384–387
VNV Target Altitude Capture Mode (ALTV)-------------388
Voice alerts, TIS Traffic---------------------------76, 360, 509
VOL annunciation-------------------------------------------130
Voltmeter------------------------------------------------------ 86
Volume level
ADF-------------------------------------------------- 119, 121
VOR
Nearest--------------------------------------------- 187–188
VOR selection------------------------------------------------110
VSI-------------------------------------------------------------270
VS TGT------------------------------------------------- 230, 268
INDEX
W
WAAS-------------------------------------------- 252, 403, 545
WAAS precision approach---------------------------------414
I-6
Garmin G1000 Pilot’s Guide for the Cessna Corvalis/Corvalis TT
190-00552-05 Rev. A
G1000
®
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p:886/02.2642.9199
f:886/02.2642.9099
www.garmin.com
Cessna
Corvalis/Corvalis TT
Garmin (Europe) Ltd.
Liberty House, Bulls Copse Road
Houndsdown Business Park
Southampton, SO40 9RB, U.K.
p:44/0870.8501241
f:44/0870.8501251
®
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p:503.391.3411
f:503.364.2138
G1000 Pilot’s Guide
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p:913.397.8200
f:913.397.8282
190-00552-05
Revision A
Integrated Flight Deck
Pilot’s Guide
Was this manual useful for you? yes no
Thank you for your participation!

* Your assessment is very important for improving the work of artificial intelligence, which forms the content of this project

Download PDF

advertising