Garmin Software Version 0534.21 Cockpit Reference Guide

G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
FLIGHT INSTRUMENTS
ENGINE INDICATION SYSTEM
NAV/COM/TRANSPONDER/AUDIO PANEL
AUTOMATIC FLIGHT CONTROL SYSTEM
GPS NAVIGATION
FLIGHT PLANNING
PROCEDURES
HAZARD AVOIDANCE
ADDITIONAL FEATURES
ABNORMAL OPERATION
ANNUNCIATIONS & ALERTS
APPENDIX
INDEX
Copyright © 2006-2010, 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
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Tel: 44/0870.8501241
Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199
Fax: 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,
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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. FliteCharts®
and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be
used without the express permission of Garmin.
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.
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.
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
190-00567-05 Rev. A
Printed in the U.S.A.
Warnings, Cautions & 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 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.
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.
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Warnings, Cautions & Notes
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 self-test 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.
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 utilize 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
Cessna Corvalis/Corvalis TT Pilot’s Operating Handbook (POH). 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.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Warnings, Cautions & Notes
WARNING: The illustrations in this guide are only examples. Never use
the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory
Circular, Subject: Thunderstorms, and the Aeronautical Information Manual
(AIM) recommend avoiding “by at least 20 miles any thunderstorm identified
as severe or giving an intense radar echo.”
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 ANTIREFLECTIVE 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 antireflective 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.
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Warnings, Cautions & Notes
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.
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: 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.
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: 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 yards 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 purpose of this Cockpit Reference Guide is to provide th e pilot
a resource with which to find operating instructions on the major features
of the G1000 system more easily. It is not intended to be a comprehensive
operating guide. Complete operating procedures for the system are found
in the G1000 Pilot’s Guide for this aircraft.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Record of Revisions
Part Number
190-00567-00
Rev A
Change Summary
Production release
Rev B
190-00567-01
Rev A
Added C350 parameters, TAWS changes, and Stormscope.
Rev B
190-00567-02
Changed company references to Cessna
Reformatted manual
Added GDU 9.03 parameters
190-00567-03
Added GDU 9.05 with Synthethic Vision System (SVS)
Removed Stormscope
Added Tach Timer
Added Flight Plan Import/Export
Added AOPA Airport Directory
Added Auxiliary Video
Added temporary user waypoints
Added CDI availability during Dead Reckoning mode
Added new MFD page navigation
Added other GDU 10.01 parameters
Updated to GDU 12.03 parameters
Added METAR, STRMSCP, and weather LEGEND softkey functions
Added Profile View
Added AC-U-KWIK Airport Directory
Added MV DB update procedure
Added Stormscope
Added flight plan enhancements
Updated weather legend
Updated database procedures
Updated message advisories
190-00567-04
190-00567-05
Revision
A
190-00567-05 Rev. A
Added GDU 8.10 parameters, WAAS, VNAV, Airways, and Charts
Date of Revision
August, 2012
Affected Pages
All
Description
Production Release
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Table of Contents
FLIGHT INSTRUMENTS................................................................................................................. 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Change Altimeter and Selected Altitude Display Units.................................................... 1
Change Navigation Sources.................................................................................................... 2
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs............................................................................................................. 2
Set Barometric Minimum Descent Altitude......................................................................... 3
Displaying Wind Data............................................................................................................... 3
Changing HSI Format................................................................................................................ 3
ENGINE INDICATION SYSTEM.................................................................................................. 5
Engine Page................................................................................................................................ 6
Engine Leaning Assist Mode.................................................................................................. 10
NAV/COM/TRANSPONDER/AUDIO PANEL........................................................................ 13
ADF Tuning (Optional)............................................................................................................. 13
DME Tuning (Optional)............................................................................................................ 13
Enter a Transponder Code..................................................................................................... 13
Selecting a COM Radio........................................................................................................... 14
Selecting a NAV Radio............................................................................................................ 14
NAV/COM Tuning...................................................................................................................... 14
Split COM................................................................................................................................... 14
Digital Clearance Recorder and Player............................................................................... 15
Intercom System (ICS) Isolation........................................................................................... 15
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM........................................................ 17
Flight Director Activation...................................................................................................... 17
Vertical Modes.......................................................................................................................... 18
Lateral Modes........................................................................................................................... 19
GPS NAVIGATION......................................................................................................................... 21
Direct-to Navigation............................................................................................................... 21
Activate a Stored Flight Plan................................................................................................ 22
Activate a Flight Plan Leg...................................................................................................... 22
Stop Navigating a Flight Plan............................................................................................... 23
Vertical Navigation (VNAV)................................................................................................... 23
FLIGHT PLANNING....................................................................................................................... 25
Trip Planning............................................................................................................................. 25
Create a User Waypoint Defined by Latitude & Longitude............................................ 27
Create a User Waypoint Defined by Radials from Other Waypoints............................ 27
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
i
Table of Contents
Create a User Waypoint Defined by a Radial & Distance from Another Waypoint... 29
Create a User Waypoint using the Map Pointer............................................................... 30
Delete a User Waypoint.......................................................................................................... 31
Create a Flight Plan................................................................................................................. 32
Import a Flight Plan from an SD Card................................................................................. 33
Insert a Waypoint in the Active Flight Plan....................................................................... 33
Enter an Airway in a Flight Plan........................................................................................... 34
Invert An Active Flight Plan................................................................................................... 35
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 35
Store a Flight Plan................................................................................................................... 35
Edit a Stored Flight Plan........................................................................................................ 36
Delete a Waypoint from the Flight Plan............................................................................. 36
Invert and Activate a Stored Flight Plan............................................................................ 36
Copy a Flight Plan.................................................................................................................... 37
Delete a Flight Plan................................................................................................................. 37
Graphical Flight Plan Creation.............................................................................................. 38
Export a Flight Plan to an SD Card...................................................................................... 38
PROCEDURES.................................................................................................................................. 39
Load and Activate a Departure Procedure........................................................................ 39
Activate A Departure Leg...................................................................................................... 39
Load An Arrival Procedure..................................................................................................... 40
Activate An Arrival Leg.......................................................................................................... 40
Load and/or Activate an Approach Procedure.................................................................. 41
Activate An Approach in the Active Flight Plan................................................................ 42
Activate a Vector to Final Approach Fix............................................................................. 42
Activate A Missed Approach in the Active Flight Plan.................................................... 42
HAZARD AVOIDANCE................................................................................................................. 43
Customizing the Hazard Displays on the Navigation Map............................................. 43
STORMSCOPE® (Optional)...................................................................................................... 43
SiriusXM Weather (Optional)................................................................................................ 45
Traffic Systems......................................................................................................................... 47
Terrain And Obstacle Proximity............................................................................................ 49
Terrain-SVS................................................................................................................................ 50
Terrain Awareness & Warning System (TAWS) Display (Optional)................................ 52
ADDITIONAL FEATURES............................................................................................................ 55
Synthetic Vision (Optional).................................................................................................... 55
Terminal Procedure Charts.................................................................................................... 56
Airport Directory..................................................................................................................... 58
SiriusXM Radio Entertainment............................................................................................. 59
Auxiliary Video (Optional)..................................................................................................... 61
Electronic Checklists............................................................................................................... 63
ii
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Table of Contents
ABNORMAL OPERATION.......................................................................................................... 65
Reversionary Mode................................................................................................................. 65
Abnormal COM Operation..................................................................................................... 65
Audio Panel Fail-safe Operation.......................................................................................... 65
Hazard Displays with Loss of GPS Position........................................................................ 65
Unusual Attitudes.................................................................................................................... 66
Dead Reckoning....................................................................................................................... 66
ANNUNCIATIONS & ALERTS.................................................................................................... 69
G1000 System Annunciations................................................................................................ 69
WARNING Alerts....................................................................................................................... 71
CAUTION Alerts......................................................................................................................... 71
Annunciation Advisory........................................................................................................... 72
Message Advisory Alerts........................................................................................................ 72
CO Guardian Messages........................................................................................................... 72
AFCS Alerts................................................................................................................................ 73
Terrain-SVS Alerts.................................................................................................................... 74
Terrain-SVS System Status Annunciations......................................................................... 74
TAWS-B Alerts........................................................................................................................... 75
Voice Alerts............................................................................................................................... 78
MFD & PFD Message Advisories........................................................................................... 78
Database Message Advisories.............................................................................................. 79
GMA 1347 Message Advisories............................................................................................. 83
GIA 63 Message Advisories.................................................................................................... 83
GIA 63W Message Advisories................................................................................................ 86
GEA 71 Message Advisories................................................................................................... 90
GTX 33 Message Advisories................................................................................................... 90
GRS 77 Message Advisories................................................................................................... 91
GMU 44 Message Advisories................................................................................................. 91
GDL 69A Message Advisories................................................................................................ 92
GDC 74A Message Advisories................................................................................................ 92
GCU 476 Message Advisories................................................................................................ 92
Miscellaneous Message Advisories...................................................................................... 93
Flight Plan Import/Export Messages................................................................................... 97
APPENDIX........................................................................................................................................ 99
PFD Softkey Map..................................................................................................................... 99
MFD Softkey Map.................................................................................................................. 105
Loading Updated Databases............................................................................................... 107
INDEX..........................................................................................................................................Index-1
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
iii
Table of Contents
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iv
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
EIS
Turn the BARO Knob to select the desired setting.
Nav/Com/
XPDR/Audio
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
1) Select the PFD Softkey.
AFCS
2) Select the STD BARO Softkey to set standard barometric pressure.
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
GPS Nav
1) Select the PFD Softkey to display the second-level softkeys.
2) Select the ALT UNIT Softkey.
Procedures
Or:
Flight
Planning
3) Select the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Select the HPA Softkey to display the barometric pressure setting in
hectopascals.
Hazard
Avoidance
4) Select the BACK Softkey to return to the top-level softkeys.
CHANGE ALTIMETER AND SELECTED ALTITUDE DISPLAY UNITS
Additional
Features
1) Select the PFD Softkey to display the second-level softkeys.
2) Select the ALT UNIT Softkey.
Abnormal
Operation
3) Select the METERS Softkey to add or remove the metric units display for
the altimeter and selected altitude.
Annun/
Alerts
4) Select the BACK Softkey to return to the top-level softkeys.
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
1
CHANGE 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.
EIS
Flight
Instruments
Flight Instruments
3) Select the CDI Softkey a third time to return to GPS.
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1) Select the OBS Softkey to select OBS Mode.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
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 OBS Softkey again to disable OBS Mode.
GENERIC TIMER
1) Select the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
Hazard
Avoidance
Procedures
Flight
Planning
2) Turn a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
Additional
Features
2) Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
CONFIGURE VSPEED BUGS
1) Select the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
Appendix
Annun/
Alerts
Abnormal
Operation
3) Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it starts counting UP after reaching zero). Press the CLR
Key or the TMR/REF Softkey to remove the window.
Index
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Instruments
Flight
Instruments
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.
EIS
6) To remove the window, press the CLR Key or the TMR/REF Softkey.
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
Nav/Com/
XPDR/Audio
1) Select the TMR/REF Softkey.
AFCS
2) Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.
3) Turn the small FMS Knob clockwise to BARO.
GPS Nav
4) Press the ENT Key.
5) Use the small FMS Knob to enter the desired altitude.
Flight
Planning
6) Press the ENT Key.
7) To remove the window, press the CLR Key or select the TMR/REF Softkey.
Procedures
DISPLAYING WIND DATA
1) Select the PFD Softkey.
Hazard
Avoidance
2) Select the WIND Softkey to display wind data to the left of the HSI.
3) Select one of the OPTN softkeys to change how wind data is displayed.
Additional
Features
4) To remove the Wind Data Window, select the OFF Softkey.
CHANGING HSI FORMAT
Abnormal
Operation
1) Select the PFD Softkey.
2) Select the HSI FRMT Softkey.
Annun/
Alerts
3) Select the 360 HSI Softkey to display the full size HSI.
Or:
Select the ARC HSI Softkey to display the arc style HSI.
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Instruments
Blank Page
4
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Engine Indication System
Flight
Instruments
ENGINE INDICATION SYSTEM
EIS
1
Nav/Com/
XPDR/Audio
AFCS
2
GPS Nav
3
Flight
Planning
4
6
Procedures
5
6
Hazard
Avoidance
7
8
Additional
Features
9
9
10
10
Abnormal
Operation
Corvalis
Corvalis TT
EIS Display
Tachometer
3
Fuel Quantity Indicator
4
Fuel Flow Indicator
5
Oil Pressure Indicator
6
Oil Temperature Indicator
190-00567-05 Rev. A
Exhaust Gas Temperature Indicator
(Corvalis only)
8 Turbine Inlet Temperature Indicator
(Corvalis TT only)
9 Cylinder Head Temperature Indicator
10
Trim Group
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
2
7
Appendix
Engine Manifold Pressure Gauge
Annun/
Alerts
1
5
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
ENGINE PAGE
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.
Oxygen quantity and outlet pressure are also shown on the Engine Page. The
OXYGEN Softkey can be used to turn the optional oxygen system on/off. If an oxygen
system is not installed, blank gauges are displayed.
2
3
4
Flight
Planning
GPS Nav
AFCS
1
Hazard
Avoidance
Procedures
11
10
7
9
8
Additional
Features
Carbon
Monoxide
Warning
Appendix
Annun/
Alerts
Abnormal
Operation
Engine Page (Corvalis)
1
Oil Temperature/Pressure Gauge
7
Electrical Group
2
Engine Manifold Pressure Gauge
8
Trim Group
3
Tachometer
9
Engine Temperature Group
4
Fuel Calculations Group
10
Fuel Quantity Gauges
11
Fuel Flow Gauge
5
Index
Oxygen Quantity Gauge (Corvalis
TT only)
6 Oxygen Outlet Pressure Gauge (Low
Pressure Gauge shown, High Pressure
Gauge optional)(Corvalis TT only)
6
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Engine Indication System
2
3
4
5
Flight
Instruments
1
EIS
7
9
8
GPS Nav
10
AFCS
6
Nav/Com/
XPDR/Audio
11
Flight
Planning
Procedures
Engine Page (Corvalis TT)
Carbon Monoxide Detection
Hazard
Avoidance
Additional
Features
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.
When a warning is generated, the CO RST Softkey becomes available to reset the
CO Guardian and acknowledge the alert.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
7
Engine Indication System
Flight
Instruments
Fuel Calculations Group
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and
are calculated from the last time 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
• INC FUEL – Increases totalizer-based fuel remaining in one-gallon
increments
• RST FUEL – Resets totalizer-based fuel remaining to the aircraft’s fuel capacity
(98 gal or 102 gal usable) and sets the GAL USED display to zero
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Fuel
Remaining
Endurance
Calculation
Fuel Used
Calculation
Range
Calculation
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Fuel Calculations Group
8
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Engine Indication System
Nav/Com/
XPDR/Audio
AFCS
• DCLTR – Removes/displays the EGT and CHT readouts from the display
• ASSIST – Accesses the Engine Leaning Assist Mode
EIS
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, Turbine Inlet Temperature (TIT) is shown on a
sliding bar scale.
The following softkeys can be used to modify the display of engine temperature
information:
Flight
Instruments
Engine Temperature Group
Cylinder Head
Temperature
GPS Nav
Exhaust Gas
Temperature
Flight
Planning
Procedures
Hazard
Avoidance
Engine Temperature Group (Corvalis)
Additional
Features
Turbine Inlet
Temperature
Cylinder Head
Temperature
Abnormal
Operation
Exhaust Gas
Temperature
Annun/
Alerts
Appendix
Index
Engine Temperature Group (Corvalis TT)
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
9
Flight
Instruments
Engine Indication System
ENGINE LEANING ASSIST MODE
AFCS
Nav/Com/
XPDR/Audio
EIS
NOTE: Consult the Cessna Corvalis/Corvalis TT Aircraft 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.
While in Assist Mode, the EIS Display is shown along with the Fuel Flow Gauge
and an expanded Engine Temperature Group.
GPS Nav
Corvalis
Flight
Planning
When the ASSIST Softkey is selected, the system initially highlights the
number and EGT readout of the cylinder with the hottest EGT.
Hazard
Avoidance
Procedures
Fuel Flow Gauge
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
EGT Deviation
from Peak
Index
Engine Leaning Assist Mode (Corvalis)
10
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Engine Indication System
EIS
Temperature Deviation from Peak
(First Cylinder)
Flight
Instruments
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.
Nav/Com/
XPDR/Audio
AFCS
Light
Blue Bar
Represents
Peak
GPS Nav
Indicates
First
Cylinder
to Peak
Flight
Planning
Assist Mode - First Peaked Cylinder (Corvalis)
Hazard
Avoidance
Additional
Features
Temperature Deviation from Peak
(Last Cylinder)
Procedures
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.
Abnormal
Operation
Annun/
Alerts
Appendix
Indicates
Last
Cylinder to
Peak
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
Assist Mode - Last Peaked Cylinder (Corvalis)
11
Corvalis TT
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 Turbine Inlet Temperature.
Peak TIT
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
Flight
Planning
Lean or Rich TIT Deviation
From Peak
from Peak
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Engine Leaning Assist Mode (Corvalis TT)
12
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
ADF TUNING (OPTIONAL)
EIS
1) Select the ADF/DME Softkey.
Nav/Com/
XPDR/Audio
2) Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
3) Turn the large FMS Knob to select the next desired field.
AFCS
4) Turn the small FMS Knob to enter the desired number.
5) Repeat steps 3 and 4 until the desired ADF frequency is entered.
GPS Nav
6) Press the ENT Key to accept the new frequency.
7) Press the ENT Key again to transfer the frequency to the active field.
Flight
Planning
8) Turn the large FMS Knob to select the MODE field.
9) Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
10) Press the ENT Key to complete the selection.
Procedures
DME TUNING (OPTIONAL)
Hazard
Avoidance
1) Select the ADF/DME or DME Softkey.
2) Turn the large FMS to select the DME source field.
Additional
Features
3) Turn the small FMS Knob to select the desired Nav radio.
4) Press the ENT Key to complete the selection.
Abnormal
Operation
ENTER A TRANSPONDER CODE
1) Select the XPDR Softkey to display the transponder mode selection
softkeys.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
13
Index
190-00567-05 Rev. A
Appendix
3) Select the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
Annun/
Alerts
2) Select the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
SELECTING A COM RADIO
Transmit/Receive
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
1) To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
Flight
Planning
2) Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
NAV/COM TUNING
1) Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.
Hazard
Avoidance
Procedures
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
SELECTING A NAV RADIO
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Receive Only
2) Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
3) Press the Frequency Transfer Key to place the frequency into the active
frequency field.
SPLIT COM
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.
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.
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
14
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Nav/Com/XPDR/Audio Panel
NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is
not recorded for COM3 MIC.
Passenger
Hears
Selected
radios; pilot;
copilot;
passengers;
music
Selected
radios; pilot;
copilot;
passengers;
music
Copilot;
passengers;
music
Copilot;
passengers;
music
PILOT
ON
OFF
Selected
radios; pilot
Copilot
Selected
radios; pilot;
passengers;
music
Selected
radios; pilot;
copilot
Passengers;
music
COPILOT
OFF
ON
Selected
radios; pilot;
passengers;
music
CREW
ON
ON
Selected
radios; pilot;
copilot
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
OFF
Appendix
OFF
Annun/
Alerts
ALL
Selected
radios; pilot;
copilot;
passengers;
music
Abnormal
Operation
Copilot
Hears
Additional
Features
Pilot Hears
Hazard
Avoidance
PILOT KEY
COPLT KEY
ANNUNCIATOR ANNUNCIATOR
Procedures
Mode
Flight
Planning
Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/
Com radios and music.
GPS Nav
INTERCOM SYSTEM (ICS) ISOLATION
AFCS
• Pressing the PLAY Key once plays the latest recorded memory block, then returns
to normal operation.
• Pressing the MKR/MUTE Key while playing a memory block stops play.
• Pressing the PLAY Key during play begins playing the previously recorded
memory block. Each subsequent press of the PLAY Key begins playing the next
previously recorded block.
Nav/Com/
XPDR/Audio
EIS
DIGITAL CLEARANCE RECORDER AND PLAYER
Flight
Instruments
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.
15
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Blank Page
16
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
AFCS
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
FLIGHT DIRECTOR ACTIVATION
GPS
VAPP
LOC
HDG Key
Heading Select
HDG
Appendix
Approach**
PIT
PIT
GP
GS
PIT
Annun/
Alerts
APR Key
Pitch Hold (default)
Pitch Hold (default)
Glidepath
Glideslope
Pitch Hold (default)
Abnormal
Operation
Backcourse***
PIT
Additional
Features
BC Key (GDU 1044B)
Pitch Hold (default)
Hazard
Avoidance
Navigation**
GA Switch
ROL
ROL
ROL
TO
GA
ROL
ROL
ROL
ROL
GPS
VOR
LOC
BC
Procedures
NAV Key
FD Key
AP Key
CWS Switch
Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Takeoff (on ground)
GA
Go Around (in air)
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Flight Level Change
FLC
Flight
Planning
ALT Key
VS Key
VNV Key
FLC 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)
GPS Nav
Modes Selected
Control Pressed
AFCS
An initial press of a key listed in the following table (when the flight director is not
active) activates the pilot-side flight director in the listed modes.
Nav/Com/
XPDR/Audio
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
EIS
Flight
Instruments
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
17
Index
**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.
VERTICAL MODES
Vertical Mode
Pitch Hold
Selected Altitude
Armed
Altitude Hold
Vertical Speed
Flight Level Change
Vertical Path Tracking
VNAV Target Altitude
Capture
Glidepath ***
Glideslope
Go Around
Description
Control
Holds the current aircraft pitch
attitude; may be used to climb/ (default)
descend to the Selected Altitude
Captures the Selected Altitude
Holds the current Altitude
Reference
Holds aircraft vertical speed; may
be used to climb/descend to the
Selected Altitude
Holds aircraft airspeed while aircraft
is climbing/descending to the
Selected Altitude
Captures and tracks descent legs of
an active vertical profile
Captures the Vertical Navigation
(VNV) Target Altitude
Captures and tracks the SBAS
glidepath on approach
Captures and tracks the ILS
glideslope on approach
Disengages the autopilot and
commands a constant pitch attitude
and wings level in the air
Annunciation
PIT
*
ALTS
ALT Key
ALT
nnnnn ft
VS Key
VS
nnnn fpm
FLC Key
FLC
nnn kt
VNV Key
VPTH
**
ALTV
GP
APR Key
GS
GA
Switch
GA
* ALTS armed automatically when PIT, VS, FLC, or GA active, and under VPTH when Selected Altitude
is to be captured instead of VNAV Target Altitude
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of
Selected Altitude
***GP is available in installations with GIA 63W IAUs when SBAS is available.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
AFCS
18
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
AFCS
Lateral Mode
BC
GPS
Disengages the autopilot
and commands a constant
pitch angle and wings level
GA
Switch
VAPP
LOC
GA
Annun/
Alerts
APR
Key
Abnormal
Operation
Captures and tracks the
selected navigation source
(GPS, VOR, LOC)
Additional
Features
Go Around
BC Key
(GDU
1044B
only)
Hazard
Avoidance
Approach, VOR Capture/Track
Approach, LOC (Glideslope
Mode automatically armed)
BC
Procedures
Approach, GPS
Flight
Planning
Backcourse (GDU 1044B only)
Captures and tracks
a localizer signal for
backcourse approaches
GPS Nav
Captures
and
tracks
Navigation, Backcourse
a localizer signal for
Capture/Track (GDU 1044 only)
backcourse approaches
AFCS
Navigation, GPS
Navigation, VOR Enroute
Capture/Track
Navigation, LOC Capture/Track
(No Glideslope)
Nav/Com/
XPDR/Audio
Heading Select
EIS
Roll Hold
Description
Control Annunciation
Holds the current aircraft roll
attitude or rolls the wings
(default)
ROL
level, depending on the
commanded bank angle
Captures and tracks the HDG
HDG
Selected Heading
Key
GPS
Captures and tracks the
VOR
selected navigation source
(GPS, VOR, LOC)
NAV
LOC
Key
Flight
Instruments
LATERAL MODES
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
19
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
AFCS
Blank Page
20
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
GPS Navigation
Flight
Instruments
GPS NAVIGATION
DIRECT-TO NAVIGATION
EIS
Direct-to Navigation from the MFD
2)
3)
6)
9)
12)
1) Press the Direct-to Key (
2)
5)
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
21
Index
6)
Appendix
4)
Annun/
Alerts
3)
).
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
Abnormal
Operation
Direct-to Navigation from the PFD
Additional
Features
11)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
7)
GPS Nav
5)
AFCS
4)
) Key.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
Enter the desired altitude.
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
Enter the desired offset distance before (-) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
Nav/Com/
XPDR/Audio
1) Press the Direct-to (
GPS Navigation
Flight
Instruments
7) Turn the small FMS Knob to enter the desired altitude.
EIS
8) Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Nav/Com/
XPDR/Audio
10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ field.
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
AFCS
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT again to activate the Direct-to.
ACTIVATE A STORED FLIGHT PLAN
1) Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
2) Press the FMS Knob to activate the cursor.
Hazard
Avoidance
3) Turn the large FMS Knob to highlight the desired flight plan.
4) Select the ACTIVE Softkey. The confirmation window is now displayed.
ACTIVATE A FLIGHT PLAN LEG
1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
Annun/
Alerts
Abnormal
Operation
Additional
Features
5) With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
Index
Appendix
2) On the MFD, select the ACT LEG Softkey.
Or:
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
3) With ‘Activate’ highlighted, press the ENT Key.
22
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
GPS Navigation
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
1) Press the FPL Key to display the Active Flight Plan Page.
2) Press the MENU Key to display the Page Menu Window.
GPS Nav
Flight
Planning
Procedures
Large White
Text
Insertion
Point
Indicator
AFCS
The navigation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.
Nav/Com/
XPDR/Audio
VERTICAL NAVIGATION (VNAV)
EIS
3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This does not delete the stored flight plan, only the active flight plan.
Large Light
Blue Text
Hazard
Avoidance
Small Light
Blue Text
Additional
Features
Small Light
Blue Subdued
Text
Abnormal
Operation
Small White Text
with Altitude
Restriction Bar
Annun/
Alerts
Cross AT or ABOVE 5,000 ft
Appendix
Cross AT 2,300 ft
Cross AT or BELOW 3,000 ft
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
23
Altitudes associated with approach procedures are “auto-designated”. This means
the system automatically uses the altitudes loaded with the approach for giving vertical
flight path guidance outside the FAF. Note these altitudes are displayed as small light
blue text.
Altitudes associated with arrival procedures are “manually-designated”. This means
the system does not use the altitudes loaded with the arrival for giving vertical flight
path guidance until designated to do so by the pilot. Note that these altitudes are
initially displayed as white text. These altitudes may be “designated” by placing the
cursor over the desired altitude and pressing the ENT Key. After designation, the text
changes to light blue.
Altitudes that have been designated for use in vertical navigation may also be
made “non-designated” by placing the cursor over the desired altitude and pressing
the CLR Key. The altitude is now displayed only as a reference. It will not be used
to give vertical flight path guidance. Other displayed altitudes may change due to
re-calculations or rendered invalid as a result of manually changing an altitude to a
non-designated altitude.
White Text
Light Blue Text
Large Text
Altitude calculated by the
system 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 flight path
guidance.
Altitude has been entered
by the pilot. Altitude is
designated for use in
giving vertical flight path
guidance.  Altitude does
not match the published
altitude in navigation
database or no published
altitude exists.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Small Text
Altitude is not designated
to be used in determining
vertical flight path
guidance.  Altitude has
been retrieved from the
navigation database and
is provided as a reference.
Altitude is designated
for use in giving vertical
flight path guidance. 
Altitude has been
retrieved from the
navigation database
or has been entered by
the pilot and matches a
published altitude in the
navigation database.
The system cannot
use this altitude in
determining vertical
flight path guidance.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
GPS Navigation
24
Light Blue
Subdued Text
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Planning
Flight
Instruments
FLIGHT PLANNING
TRIP PLANNING
EIS
1) Turn the large FMS Knob to select the ‘AUX’ page group.
3) The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, select the AUTO or MANUAL
Softkey.
AFCS
4) For Direct-to planning:
GPS Nav
a) Select the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
Flight
Planning
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
For point-to-point planning:
Hazard
Avoidance
Or:
Procedures
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
a) Enter the identifier of the starting waypoint.
Additional
Features
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
Abnormal
Operation
c) Again, enter the identifier of the ending waypoint.
d) Press the ENT Key to accept the waypoint.
Or:
For flight plan leg planning:
Annun/
Alerts
Nav/Com/
XPDR/Audio
2) Turn the small FMS Knob to select the Trip Planning page icon.
a) Press the FPL Softkey (at the bottom of the display).
Appendix
b) Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
25
Flight Planning
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
d) Turn the small FMS Knob to select the desired leg of the flight plan, or
select ‘CUM’ to apply trip planning calculations to the entire flight plan.
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ is an available option to display planning data for the
remainder of the flight plan.
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
AFCS
5) Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
GPS Nav
NOTE: The departure time on the Trip Planning Page is used for preflight
planning. Refer to the Utility Page for the actual flight departure time.
6) Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
Procedures
9) The flashing cursor moves to the fuel onboard field. Enter the fuel onboard.
Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel
onboard is provided by the fuel totalizer.
Additional
Features
8) The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow
is provided by the system.
Hazard
Avoidance
Flight
Planning
7) The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
Abnormal
Operation
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that
in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system.
Annun/
Alerts
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page
mode, altitude is provided by the system.
Index
Appendix
12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter
the desired baro setting. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered
on the PFD.
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.
26
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Planning
Flight
Instruments
CREATE A USER WAYPOINT DEFINED BY LATITUDE & LONGITUDE
1) Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
2) Turn the small FMS Knob to select the User WPT Information Page.
EIS
3) Press the NEW Softkey. A waypoint is created at the current aircraft
position.
Nav/Com/
XPDR/Audio
4) Enter the desired waypoint name.
5) Press the ENT Key.
AFCS
6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
GPS Nav
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
8) Turn the small FMS Knob to select LAT/LON (latitude and longitude).
9) Press the ENT Key.
1) Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
Additional
Features
2) Turn the small FMS Knob to select the User WPT Information Page.
Abnormal
Operation
3) Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4) Enter the desired waypoint name.
5) Press the ENT Key.
Annun/
Alerts
6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Appendix
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
190-00567-05 Rev. A
Hazard
Avoidance
CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS
Procedures
7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
Flight
Planning
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
27
Flight Planning
Flight
Instruments
7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
8) Turn the small FMS Knob to select RAD/RAD (radial/radial).
EIS
9) Press the ENT Key.
Nav/Com/
XPDR/Audio
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
AFCS
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
b) Turn the large FMS Knob to select the desired waypoint.
GPS Nav
c) Press the ENT Key.
Or:
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Procedures
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Hazard
Avoidance
Or:
Additional
Features
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Abnormal
Operation
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Annun/
Alerts
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Appendix
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
Index
d) Press the ENT Key.
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
28
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Planning
13) Repeat step 10 to enter the next waypoint name.
15) Press the ENT Key.
Nav/Com/
XPDR/Audio
16) Press the FMS Knob to remove the flashing cursor.
EIS
14) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field for the
second waypoint. Enter the desired radial from the reference waypoint.
Flight
Instruments
12) Press the ENT Key.
AFCS
CREATE A USER WAYPOINT DEFINED BY A RADIAL & DISTANCE FROM
ANOTHER WAYPOINT
1) Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
GPS Nav
2) Turn the small FMS Knob to select the User WPT Information Page.
3) Press the NEW Softkey. A waypoint is created at the current aircraft
position.
Flight
Planning
4) Enter the desired waypoint name.
5) Press the ENT Key.
Procedures
6) The cursor is now in the ‘WAYPOINT TYPE’ field. If desired, the waypoint
can be made temporary (deleted automatically when the system is turned
off). If the waypoint is to remain in the system, proceed to step 7.
Hazard
Avoidance
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
8) Turn the small FMS Knob to select RAD/DIS (radial/distance).
Abnormal
Operation
7) With the cursor in the ‘WAYPOINT TYPE’ field, turn the small FMS Knob to
display a list of waypoint types.
Additional
Features
b) Press the ENT Key to place a check-mark in the box. Turn the large
FMS Knob to place the cursor back in the ‘WAYPOINT TYPE’ field.
9) Press the ENT Key.
Annun/
Alerts
a) When a flight plan is active, turning the small FMS Knob to the left will
display a list of the flight plan waypoints.
Index
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Appendix
10) The cursor moves to the ‘REFERENCE WAYPOINTS’ field. With the first
waypoint name highlighted, use the FMS Knobs to enter the desired
waypoint name. Waypoints may also be selected as follows:
29
Flight Planning
Flight
Instruments
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
EIS
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Nav/Com/
XPDR/Audio
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
Flight
Planning
d) Press the ENT Key.
Or:
Procedures
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Hazard
Avoidance
b) Turn the small FMS Knob to the right to display the ‘USER’ waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Additional
Features
11) Press the ENT Key. The cursor is displayed in the ‘RAD’ (radial) field. Enter
the desired radial from the reference waypoint.
Abnormal
Operation
12) Press the ENT Key.
13) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Annun/
Alerts
14) Press the ENT Key.
15) Press the FMS Knob to remove the flashing cursor.
CREATE A USER WAYPOINT USING THE MAP POINTER
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.
Index
Appendix
Or:
30
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Planning
4) Press the ENT Key to accept the selected name.
AFCS
5) If desired, define the type and location (i.e., LAT/LON, RAD/RAD or RAD/
DIS) of the waypoint.
Nav/Com/
XPDR/Audio
3) Enter a user waypoint name (up to six characters).
EIS
NOTE: If the pointer has highlighted a map database feature, one of three
things happens upon pressing 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.
Flight
Instruments
8) Press the FMS Knob to remove the flashing cursor.
Procedures
9) Press the GO BACK Softkey to return to the map page
Flight
Planning
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.
GPS Nav
6) Press the ENT Key to accept the new waypoint.
DELETE A USER WAYPOINT
Hazard
Avoidance
1) Turn the large FMS Knob to select the ‘WPT’ page group.
2) Turn the small FMS Knob to select the User WPT Information Page.
5) Turn the small FMS Knob to highlight the desired waypoint.
6) Press the DELETE Softkey.
Annun/
Alerts
7) The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
Abnormal
Operation
4) Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
Additional
Features
3) Press the FMS Knob to activate the cursor.
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
31
CREATE A FLIGHT PLAN
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
EIS
Flight
Instruments
Flight Planning
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Creating an active flight plan:
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (only on MFD).
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).
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.
6) When all waypoints have been entered, press the FMS Knob to remove the
cursor.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
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).
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.
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.
32
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Planning
1) Insert the SD card containing the flight plan in the top card slot on the
MFD.
Nav/Com/
XPDR/Audio
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.
AFCS
6) Press the IMPORT Softkey.
Additional
Features
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
1) Press the FPL Key to display the active flight plan.
Appendix
4) Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
5) Enter the new flight plan waypoint by one of the following:
a) Enter the user waypoint identifier, facility, or city.
Index
b) Press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Annun/
Alerts
3) Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint (as indicated by
the insertion point indicator).
Abnormal
Operation
2) If necessary, press the FMS Knob to activate the cursor.
190-00567-05 Rev. A
Hazard
Avoidance
8) Press the ENT Key.
Procedures
7) Turn the small FMS Knob to highlight the desired flight plan for importing.
Flight
Planning
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 a list of the 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 existing or empty
flight plan, and again press the IMPORT Softkey.
GPS Nav
If an empty flight plan is selected, a list of the available flight plans on the
SD card will be displayed.
Or:
EIS
2) Press the FPL Key on the MFD to display the Active Flight Plan Page on the
MFD.
Flight
Instruments
IMPORT A FLIGHT PLAN FROM AN SD CARD
33
Flight Planning
Flight
Instruments
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
EIS
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Nav/Com/
XPDR/Audio
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
AFCS
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
GPS Nav
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
c) Turn the large FMS Knob to select the desired waypoint.
e) Press the ENT Key again to “accept” the waypoint.
ENTER AN AIRWAY IN A FLIGHT PLAN
1) Press the FPL Key.
2) Press the FMS Knob to activate the cursor (not required on the PFD).
Hazard
Avoidance
Procedures
Flight
Planning
d) Press the ENT Key.
Additional
Features
3) Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. The airway is inserted before the highlighted waypoint (as
indicated by the insertion point indicator). If this waypoint is not a valid
airway entry point, a valid entry point should be entered at this time.
Annun/
Alerts
Abnormal
Operation
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 an acceptable airway entry waypoint has
been chosen.
Appendix
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.
Index
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.
34
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Planning
Flight
Instruments
INVERT AN ACTIVE FLIGHT PLAN
1) Press the FPL Key to display the active flight plan.
2) Press the MENU Key to display the Page Menu.
EIS
3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
Nav/Com/
XPDR/Audio
4) Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.
5) With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
Or, for a stored flight plan:
Flight
Planning
GPS Nav
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
AFCS
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
a) Press the FPL Key on the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
Procedures
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
3) Press the CLR Key to display a confirmation window.
Abnormal
Operation
4) With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
Additional
Features
2) Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.
Hazard
Avoidance
d) Select the EDIT Softkey.
STORE A FLIGHT PLAN
3) With ‘OK’ highlighted, press the ENT Key to store the flight plan.
Appendix
2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
Annun/
Alerts
1) After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
35
EDIT A STORED FLIGHT PLAN
1) Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
2) Press the FMS Knob to activate the cursor.
EIS
Flight
Instruments
Flight Planning
Nav/Com/
XPDR/Audio
3) Turn the large FMS Knob to highlight the desired flight plan.
4) Select the EDIT Softkey.
5) Turn the large FMS Knob to place the cursor in the desired location.
7) Press the FMS Knob to return to the Flight Plan Catalog Page.
DELETE A WAYPOINT FROM THE FLIGHT PLAN
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Flight
Planning
GPS Nav
AFCS
6) Enter the changes, then press the ENT Key.
Or, for a stored flight plan:
Procedures
a) Press the FPL Key on the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
b) Press the FMS Knob to activate the cursor.
Hazard
Avoidance
c) Turn the large FMS Knob to highlight the desired flight plan.
d) Select the EDIT Softkey.
Additional
Features
2) Turn the large FMS Knob to highlight the waypoint to be deleted.
Abnormal
Operation
5) Once all changes have been made, press the FMS Knob to remove the
cursor.
INVERT AND ACTIVATE A STORED FLIGHT PLAN
1) Press the FPL Key on the MFD.
2) Turn the small FMS Knob to select the Flight Plan Catalog Page.
Index
Appendix
4) With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.
Annun/
Alerts
3) Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
3) Press the FMS Knob to activate the cursor.
36
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Flight Planning
5) Select the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
Nav/Com/
XPDR/Audio
COPY A FLIGHT PLAN
EIS
6) With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.
Flight
Instruments
4) Turn the large FMS Knob to highlight the desired flight plan.
1) Press the FPL Key on the MFD.
AFCS
2) Turn the small FMS Knob to select the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor.
6) With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Flight
Planning
5) Select the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
GPS Nav
4) Turn the large FMS Knob to highlight the flight plan to be copied.
Procedures
DELETE A FLIGHT PLAN
Hazard
Avoidance
1) Press the FPL Key on the MFD.
2) Turn the small FMS Knob to select the Flight Plan Catalog Page.
3) Press the FMS Knob to activate the cursor.
6) With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Abnormal
Operation
5) Select the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
Additional
Features
4) Turn the large FMS Knob to highlight the flight plan to be deleted.
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
37
GRAPHICAL FLIGHT PLAN CREATION
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
2) Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.
4) Select the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.
Nav/Com/
XPDR/Audio
AFCS
3) The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor (as indicated by the insertion point indicator). Turn the large FMS
Knob to select the desired insertion point.
GPS Nav
EIS
Flight
Instruments
Flight Planning
EXPORT 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 on the Contol Unit to display the Active Flight Plan Page
on the MFD.
Hazard
Avoidance
Procedures
Flight
Planning
5) To change the user waypoint name, follow the procedure for modifying a user
waypoint.
3) Turn the small FMS Knob to select the Flight Plan Catalog Page.
Additional
Features
4) Press the FMS Knob to activate the cursor.
5) Turn the large FMS Knob to highlight the flight plan to be exported.
Abnormal
Operation
6) Press the EXPORT Softkey.
Index
Appendix
Annun/
Alerts
7) Press the ENT Key to confirm the export.
38
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
EIS
1) Press the PROC Key.
3) Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
5) Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.
Flight
Planning
7) Turn the large FMS Knob to highlight the desired transition.
GPS Nav
6) Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
AFCS
4) Turn the large FMS Knob to highlight the desired departure.
Nav/Com/
XPDR/Audio
2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
8) Press the ENT Key.
Hazard
Avoidance
ACTIVATE A DEPARTURE LEG
Procedures
9) With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
1) Press the FPL Key on the MFD to display the active flight plan.
Additional
Features
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the desired waypoint within the
departure.
Abnormal
Operation
4) Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5) With ‘ACTIVATE’ highlighted, press the ENT Key.
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
39
Flight
Instruments
Procedures
LOAD AN ARRIVAL PROCEDURE
1) Press the PROC Key.
EIS
2) Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
Nav/Com/
XPDR/Audio
3) Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
4) Turn the large FMS Knob to highlight the desired arrival.
5) Press the ENT Key. A list of transitions is displayed for the selected arrival.
AFCS
6) Turn either FMS Knob to select the desired transition.
GPS Nav
7) Press the ENT Key. A list of runways may be displayed for the selected
arrival.
8) Turn the large FMS Knob to highlight the desired runway.
9) Press the ENT Key.
Flight
Planning
10) With ‘LOAD?’ highlighted, press the ENT Key.
11) The arrival becomes part of the active flight plan.
Procedures
12) If an altitude associated with a waypoint in an arrival procedure is to be
used to calculate vertical guidance perform the following steps:
a) Press the FMS Knob to activate the cursor.
c) Press the ENT Key to designate the altitude for use in giving vertical
guidance.
ACTIVATE AN ARRIVAL LEG
1) Press the FPL Key to display the active flight plan.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
b) Turn the large FMS Knob to highlight the desired waypoint altitude.
2) Press the FMS Knob to activate the cursor.
Annun/
Alerts
3) Turn the large FMS Knob to highlight the desired waypoint within the
arrival.
Appendix
4) Select the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
Index
5) With ‘ACTIVATE’ highlighted, press the ENT Key.
40
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Procedures
2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
4) Turn either FMS Knob to highlight the desired approach.
Flight
Planning
6) Turn either FMS Knob to select the desired transition. The “Vectors”
option assumes vectors will be received to the final course segment of
the approach and will provide navigation guidance relative to the final
approach course.
Procedures
7) Press the ENT Key. The cursor moves to the MINIMUMS field.
Hazard
Avoidance
8) If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO.
Additional
Features
9) Press the ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
Abnormal
Operation
10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.
Annun/
Alerts
GPS Nav
5) Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
AFCS
3) Press the ENT Key. A list of available approaches for the destination airport
is displayed.
Nav/Com/
XPDR/Audio
1) Press the PROC Key.
EIS
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
Instruments
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
Appendix
12) Press the ENT Key.
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
41
Flight
Instruments
Procedures
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
1) Press the PROC Key.
3) Press the ENT Key.
ACTIVATE A VECTOR TO FINAL APPROACH FIX
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3) Press the ENT Key.
4) The final approach course becomes the active leg.
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
1) Press the PROC Key.
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
2) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
Procedures
3) Press the ENT Key. A confirmation window is displayed.
Or:
Press the Go-around Switch.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
4) With ‘ACTIVATE’ highlighted, press the ENT Key.
42
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
EIS
1) With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
GPS Nav
STORMSCOPE® (OPTIONAL)
2) Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove
Stormscope Lightning Data from the Navigation Map Page.
Hazard
Avoidance
1) Press the MAP Softkey.
Procedures
Displaying Stormscope Lightning Data on the Navigation Map Page
Flight
Planning
WARNING: The Stormscope system is not intended to be used for hazardous
thunderstorm penetration. Weather information on the G1000 MFD is
approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for
detailed operation.
Additional
Features
Lightning Age
Strike is less than 6 seconds old
AFCS
3) Press the small FMS Knob to return to the Navigation Map Page.
Nav/Com/
XPDR/Audio
2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.
Symbol
Abnormal
Operation
Strike is between 6 and 60 seconds old
Annun/
Alerts
Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
1) Press the MENU Key (with the Navigation Map Page displayed).
2) Turn either FMS Knob to highlight ‘Map Setup’.
Index
3) Press the ENT Key.
4) Turn the small FMS Knob to highlight ‘Weather’.
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
43
Hazard Avoidance
Flight
Instruments
5) Press the ENT Key.
6) Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field.
7) Turn the small FMS Knob to display the ‘Cell/Strike’ window.
EIS
8) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
Nav/Com/
XPDR/Audio
9) Push the FMS Knob to return to the Navigation Map Page.
Clear Stormscope Lightning Data from the Navigation Map Page
1) Press the MENU Key (with the Navigation Map Page displayed).
AFCS
2) Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field
and press the ENT Key.
GPS Nav
NOTE: 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
Flight
Planning
positions are depicted accurately in relation to the nose of the aircraft.
Stormscope Page
Procedures
1) Turn the large FMS Knob until the Map Page group is selected.
2) Turn the small FMS Knob until the Stormscope Page is selected.
Hazard
Avoidance
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
1) Select the Stormscope Page.
Abnormal
Operation
Additional
Features
2) Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed.
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
located in the upper left corner of the Stormscope Page.
Annun/
Alerts
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Change the Viewing Mode Between 360˚ and 120˚
Appendix
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
44
Press the CLEAR Softkey to remove all Stormscope lightning data from the
display.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Hazard Avoidance
AFCS
1) Select the MAP Softkey.
2) Select the NEXRAD, XM LTNG, and METAR Softkey to display the desired
weather. Select the applicable softkey again to remove weather data from
the Navigation Map Page.
Nav/Com/
XPDR/Audio
Displaying SiriusXM Weather on the Navigation Map Page
EIS
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.
Flight
Instruments
SIRIUSXM WEATHER (OPTIONAL)
Display METAR and TAF information on the Airport Information Page
GPS Nav
1) Turn the large FMS Knob to select the WPT Page Group.
2) Turn the small FMS Knob to select the Airport Information Page.
Flight
Planning
3) Select the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
Procedures
Displaying Weather on the Weather Data Link 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 Page.
1) Push in the Joystick to display the panning arrow.
3) Press the ENT Key to display pertinent information for the selected product.
Note that pressing the ENT Key when panning over an AIRMET or a
SIGMET displays an information box that shows the text of the report.
Panning over an airport with METAR information does not display more
information but allows the user to press the ENT Key and select that
Airport’s Information Page to display the text of the report. Pressing the
ENT Key when panning over a TFR displays TFR specific information.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
190-00567-05 Rev. A
Appendix
Annun/
Alerts
2) Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
or SIGMETs.
Abnormal
Operation
Map Panning Information – Weather Data Link Page
Additional
Features
4) Select the LEGEND Softkey to view the legends for the selected products.
If necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.
Hazard
Avoidance
3) Select the available softkeys to select the desired XM weather product.
45
Hazard Avoidance
Flight
Instruments
SiriusXM Weather Products and Symbols
EIS
Wx Product
Status Icons
Description
Nav/Com/
XPDR/Audio
NEXRAD - Available for the US and Canada. The age of the displayed data
for each is shown at the right.
ECHO TOP - The age of the displayed data is shown at the right. Not
displayed when CLOUD TOP is displayed.
AFCS
CLOUD TOP - The age of the displayed data is shown at the right. Not
displayed when ECHO TOP is displayed.
GPS Nav
XM LIGHTNING - The age of the displayed data is shown at the right.
Flight
Planning
CELL MOVEMENT - The age of the displayed data is shown at the right.
Procedures
SIGMET & AIRMET - The age of the displayed data for each is shown at the
right.
Hazard
Avoidance
METAR - Available for the US and Canada. The age of the displayed data for
each is shown at the right.
Additional
Features
SURFACE ANALYSIS with CITY FORECAST - The upper symbol depicts
Surface Analysis. The lower symbol depicts City Forecast. The age of the
displayed data for each is shown at the right. The selected forecast period is
shown at the bottom.
Abnormal
Operation
FREEZING LEVEL - The age of the displayed data is shown at the right.
Annun/
Alerts
WINDS ALOFT - Available for the US and Canada. The age of the displayed
data for each is shown at the right. The altitude selection is shown at the
bottom.
Appendix
COUNTY WARNING - The age of the displayed data is shown at the right.
Index
CYCLONE WARNING - The age of the displayed data is shown at the right.
46
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Hazard Avoidance
Flight
Instruments
Wx Product
Status Icons
Description
AIREP - The age of the displayed data is shown at the right.
EIS
Nav/Com/
XPDR/Audio
PIREP - The age of the displayed data is shown at the right. Urgent Pireps
are displayed in yellow.
TURBULENCE - The age of the displayed data is shown at the right. The
altitude selection is shown at the bottom.
AFCS
ICING POTENTIAL - The age of the displayed data is shown at the right.
The altitude selection is shown at the bottom.
GPS Nav
No Status Icon
TFR- Depicted as an area outlined in yellow
Flight
Planning
TRAFFIC SYSTEMS
Description
Additional
Features
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Hazard
Avoidance
Traffic Symbol
Procedures
• If Traffic information Service (TIS) is configured, STANDBY, OPERATE, and
TNA MUTE softkeys are displayed.
• If a Traffic Advisory System (TAS) is configured, STANDBY, NORMAL, TEST,
and ALT MODE softkeys are displayed.
Abnormal
Operation
Proximity Advisory (PA) (Not available with TIS system)
(intruder is within 5 nm and less than 1200’ vertical separation)
Annun/
Alerts
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
Traffic Advisory Off Scale
Appendix
Traffic Symbol Description
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
47
Hazard Avoidance
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Traffic Information Service (TIS)
AFCS
Displaying Traffic on the Traffic Map Page
1) Turn the large FMS Knob to select the Map Page Group.
GPS Nav
2) Turn the small FMS Knob to select the Traffic Map Page.
3) Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
Flight
Planning
4) Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
Procedures
5) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Hazard
Avoidance
6) Select the TNA MUTE Softkey to mute the “Traffic Not Available” aural
alert.
Displaying Traffic on the Navigation Map
Additional
Features
1) Ensure TIS is operating. With the Navigation Map displayed, select the
MAP Softkey.
Abnormal
Operation
2) Select the TRAFFIC Softkey. Traffic is now displayed on the map.
Traffic Advisory System (TAS) (Optional)
Annun/
Alerts
Displaying Traffic on the Traffic Map Page
1) Turn the large FMS Knob to select the Map Page Group.
Index
Appendix
2) Turn the small FMS Knob to select the Traffic Map Page. ‘OPERATING’ is
displayed in the Traffic Mode field.
48
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Hazard Avoidance
Flight
Instruments
3) Select the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by selecting the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.
EIS
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Nav/Com/
XPDR/Audio
5) Select the MUTE Softkey to mute TAS voice alerts.
Displaying Traffic on the Navigation Map
AFCS
1) Ensure TAS is operating.
2) With the Navigation Map displayed, select the MAP Softkey.
GPS Nav
3) Select the TRAFFIC Softkey. Traffic is now displayed on the map.
TERRAIN AND OBSTACLE PROXIMITY
Displaying Terrain and Obstacles on the Terrain Proximity Page
Hazard
Avoidance
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Terrain Proximity Page.
Additional
Features
3) If desired, select the VIEW Softkey to access the ARC and 360 Softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.
Abnormal
Operation
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
Red
Appendix
Terrain/Obstacle Location
Annun/
Alerts
190-00567-05 Rev. A
Color
Procedures
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
Flight
Planning
49
Hazard Avoidance
Flight
Instruments
Displaying Terrain and Obstacles on the Navigation Map
1) With the Navigation Map displayed, select the MAP Softkey.
TERRAIN-SVS
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
2) Select the TERRAIN Softkey. Terrain and obstacle proximity will now be
displayed on the map.
NOTE: Terrain-SVS is only available when the Synthetic Vision System (SVS)
option is installed and the TAWS option has not been installed.
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
Flight
Planning
Display Terrain on the TERRAIN-SVS Page
1) Turn the large FMS Knob to select the Map Page Group.
Procedures
2) Turn the small FMS Knob to select the Terrain-SVS Page.
Hazard
Avoidance
3) If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.
Color
Terrain/Obstacle Location
Red
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
50
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Hazard Avoidance
Flight
Instruments
Enable/Disable Aviation Data
1) While the Terrain-SVS Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
EIS
3) Press the ENT Key.
Nav/Com/
XPDR/Audio
Terrain-SVS Inhibit
AFCS
Inhibit Terrain Alerting
While the Terrain-SVS Page is displayed, select the INHIBIT Softkey.
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit Terrain’.
3) Press the ENT Key.
GPS Nav
Flight
Planning
Hazard
Avoidance
Abnormal
Operation
NOTE: 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.
Additional
Features
Procedures
Enable Terrain Alerting
While the Terrain-SVS Page is displayed, select the INHIBIT Softkey.
Or:
1) While the Terrain-SVS Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable Terrain’.
3) Press the ENT Key.
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
51
TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL)
NOTE: Terrain data is not displayed when the aircraft is outside the installed
terrain database coverage area.
NOTE: TAWS operation is only available when the G1000 is configured for a
TAWS-B installation.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
Manual System Test
AFCS
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Test TAWS’.
GPS Nav
3) Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
Flight
Planning
When all is in working order, “TAWS System Test, OK” is heard.
Display Terrain on the TAWS-B Page
Procedures
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the TAWS-B Page.
Hazard
Avoidance
3) If desired, select the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Select the 360 Softkey to return to the 360° default display.
Color
Terrain/Obstacle Location
Red
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
52
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Hazard Avoidance
Flight
Instruments
Enable/Disable Aviation Data
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
EIS
3) Press the ENT Key.
NOTE: If TAWS 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.
AFCS
Nav/Com/
XPDR/Audio
TAWS Inhibit
GPS Nav
Flight
Planning
Inhibit TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit TAWS’.
3) Press the ENT Key.
Procedures
Hazard
Avoidance
Enable TAWS
While the TAWS-B Page is displayed, select the INHIBIT Softkey.
Or:
1) While the TAWS-B Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable TAWS’.
3) Press the ENT Key.
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
53
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
Blank Page
54
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION (OPTIONAL)
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
Additional
Features
Abnormal
Operation
•
•
•
•
•
•
•
AFCS
Synthetic Vision System (SVS) functionality is offered as an optional enhancement
to the G1000 system.
SVS is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVS information is shown on the primary flight display (PFD).
In addition to SVS enhancement to the PFD, the following features have been
added to the PFD:
Nav/Com/
XPDR/Audio
WARNING: Do not use SVS runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
EIS
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.
Displaying SVS Terrain
Annun/
Alerts
1) Select the PFD Softkey.
2) Select the SYN VIS Softkey.
Appendix
3) Select the SYN TERR Softkey.
4) Select the BACK Softkey to return to the previous page.
Index
190-00567-05 Rev. A
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55
Additional Features
Flight
Instruments
Displaying Pathways
1) Select the PFD Softkey.
2) Select the SYN VIS Softkey.
EIS
3) If not already enabled, select the SYN TERR Softkey.
Nav/Com/
XPDR/Audio
4) Select the PATHWAY Softkey.
5) Select the BACK Softkey to return to the previous page.
Displaying Heading on the Horizon
AFCS
1) Select the PFD Softkey.
2) Select the SYN VIS Softkey.
GPS Nav
3) If not already enabled, select the SYN TERR Softkey.
4) Select the HRZN HDG Softkey.
Flight
Planning
5) Select the BACK Softkey to return to the previous page.
Displaying Airport Signs
Procedures
1) Select the PFD Softkey.
2) Select the SYN VIS Softkey.
3) If not already enabled, select the SYN TERR Softkey.
5) Select the BACK Softkey to return to the previous page.
TERMINAL PROCEDURE CHARTS
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
4) Select the APTSIGNS Softkey.
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Selecting the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Selecting the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Selecting
56
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
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Additional Features
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Selecting the DCLTR Softkey again cycles
back to the original map detail.
The SafeTaxi database contains detailed airport diagrams for selected airports.
These diagrams provide the pilot with situational awareness by displaying the aircraft
position in relation to taxiways, ramps, runways, terminals, and services. This
information should not be used by the pilot as the basis for maneuvering the aircraft
on the ground. This database is updated on a 56-day cycle.
ChartView (Optional)
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
View Charts from the Navigation Map Page
Flight
Planning
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. Current aircraft position is not displayed on FliteCharts.
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.
GPS Nav
FliteCharts®
AFCS
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 plan view of most approach charts and
on airport diagrams.
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.
1) Select the SHW CHRT Softkey when displayed.
Or:
Move the map pointer to point to a desired point on the map and select the
SHW CHRT Softkey.
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
3) Select the GO BACK Softkey to return to the previous page.
Appendix
2) Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.
Annun/
Alerts
57
Additional Features
Flight
Instruments
View Charts from the Active Flight Plan Page
1) While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.
EIS
2) Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
Nav/Com/
XPDR/Audio
3) Select the SHW CHRT Softkey. The appropriate chart is displayed, if
available for the item selected.
4) Select the GO BACK Softkey to return to the previous page.
AFCS
Change Day/Night View
GPS Nav
1) While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
Flight
Planning
2) Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
Procedures
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.
Hazard
Avoidance
5) Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
Additional
Features
6) In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
7) Press the FMS Knob when finished to remove the Chart Setup Menu.
AIRPORT DIRECTORY
The Aircraft Owners and Pilots Association (AOPA) or AC-U-KWIK Airport
Directory database offers detailed information regarding services, hours of operation,
lodging options, and more for various airports. This information is viewed on the
WPT-Airport Information Page.
The Airport Directory databases are revised every 56 days. The Airport Directory is
always available for use after the expiration date. Check fly.garmin.com for the current
database.
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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
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Additional Features
Flight
Instruments
View Airport Directory Information
EIS
While viewing the WPT-Airport Information Page, if necessary, select the
INFO-1 Softkey to change the softkey label to display INFO-2. Airport
information is displayed on the right half of the display.
The XM Radio Page provides information and control of the audio entertainment
features of the SiriusXM Satellite Radio.
AFCS
Selecting the XM Radio Page
Nav/Com/
XPDR/Audio
SIRIUSXM RADIO ENTERTAINMENT
1) Turn the large FMS Knob to select the Auxiliary Page Group.
GPS Nav
2) Turn the small FMS Knob to select XM Radio.
Flight
Planning
3) Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Active Channel and Channel List
Appendix
59
Index
2) Select the CH + Softkey to go down through the list in the Channel Box, or
move up the list with the CH – Softkey.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Annun/
Alerts
1) While on the XM Radio Page, select the CHNL Softkey.
190-00567-05 Rev. A
Abnormal
Operation
Select an Available Channel within the Selected Category
Additional
Features
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Select the CATGRY Softkey on the XM Radio Page.
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.
3) Press the ENT Key.
Hazard
Avoidance
Selecting a Category
Procedures
The Active Channel Box on the XM Radio Page displays the currently selected
channel. The Channels List Box of the XM Radio Page shows a list of the available
channels for the selected category.
Additional Features
Flight
Instruments
Or:
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
EIS
3) With the desired channel highlighted, press the ENT Key.
Nav/Com/
XPDR/Audio
Entering a Channel Directly
1) While on the XM Radio Page, select the CHNL Softkey.
AFCS
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.
GPS Nav
4) Press the ENT Key to activate the selected channel.
Flight
Planning
Assigning Channel Presets
Additional
Features
Hazard
Avoidance
Procedures
Up to 15 channels from any category can be assigned a preset number.
1) On the XM Radio Page, with the desired channel active, select the
PRESETS Softkey to access the first five preset channels (PS1 - PS5).
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 the SET Softkey.
4) Select any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
Abnormal
Operation
Adjusting Volume
1) With the XM Radio Page displayed, select the VOL Softkey.
Annun/
Alerts
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
Appendix
3) Select the MUTE Softkey to mute the audio. Select the MUTE Softkey
again to unmute the audio.
60
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
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Additional Features
2) Turn the small FMS Knob to select VIDEO and display the AUX-VIDEO Page.
AFCS
The video display softkeys shown below appear on the AUX - VIDEO Page.
Control of the AUX - VIDEO Page can also be accessed through the Page Menu.
GPS Nav
Selecting video menu options:
1) While viewing the AUX - VIDEO Page press the MENU Key to display the
Page Menu OPTIONS.
Flight
Planning
2) Turn the large FMS Knob to highlight the desired video adjustment option
and press the ENT Key.
Appendix
Index
61
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Abnormal
Operation
Adjusting the video settings:
1) With the AUX-VIDEO Page displayed, press the SETUP Softkey.
2) Press the BRIGHT - or BRIGHT +, to adjust display brightness in five
percent increments from 0 to 100%.
3) Press the CNTRST- or CNTRST +, to adjust display contrast in five percent
increments from 0 to 100%.
4) Press the SAT - or SAT +, to adjust display saturation in five percent
increments from 0 to 100%.
5) If desired, return the display to the default settings by pressing the RESET
Softkey.
6) Press the BACK Softkey to return to the previous softkey level.
Additional
Features
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.
Hazard
Avoidance
Video Setup
Procedures
Once the ENT key is pressed on any option, the page menu closes and returns to
the AUX - VIDEO Page.
190-00567-05 Rev. A
Nav/Com/
XPDR/Audio
Displaying auxiliary video:
1) Turn the large FMS Knob to select the AUX page group.
EIS
There are four modes of operation of the optional auxiliary video display: FullScreen, Full-Screen with Digital Zoom, Split-Screen with Map, and Split-Screen with
Map and Digital Zoom.
Flight
Instruments
AUXILIARY VIDEO (OPTIONAL)
Display Selection
Pressing the HIDE MAP Softkey removes the map and displays video on the full
screen. The softkey label changes to grey with black characters. Pressing 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.
Input Selection
While on the AUX - VIDEO Page, press the INPUT Softkey to select the EVS or
AUX video source.
Zoom/Range
Pressing the VID ZM + or VID ZM - Softkeys increases or decreases video display
magnification between 1x and 10x.
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, pressing the MAP ACTV or VID ACTV Softkey determines which display the
RANGE Knob adjusts. Pressing the softkey to display MAP ACTV allows the RANGE
Knob to control the range setting of the map display. Pressing the softkey to display
VID ACTV allows the RANGE Knob to control the zoom setting of the video display.
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 the Joystick.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Additional Features
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Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
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Additional Features
Nav/Com/
XPDR/Audio
Accessing and Navigating Checklists
1) From any page on the MFD, press the CHKLIST Softkey.
AFCS
2) Turn the large FMS Knob to select the ‘GROUP’ field.
3) Turn the small FMS Knob to select the desired procedure and press the
ENT Key.
GPS Nav
4) Turn the large FMS Knob to select the ‘CHECKLIST’ field.
Flight
Planning
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.
Annun/
Alerts
8) Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the
cursor.
Abnormal
Operation
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 been checked, ‘*CHECKLIST NOT FINISHED*’
will be displayed in yellow text.
Additional
Features
Press the CLR Key or UNCHECK Softkey to remove a check mark from an
item.
Hazard
Avoidance
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
Procedures
6) Press the ENT Key or 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.
EIS
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.
Flight
Instruments
ELECTRONIC CHECKLISTS
9) Press the ENT Key to advance to the next checklist.
Appendix
10) Press the EXIT Softkey to exit the Checklist Page and return to the page
last viewed.
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
63
Additional Features
Flight
Instruments
Immediately Accessing Emergency Procedures
1) From any page on the MFD, press the CHKLIST Softkey.
2) Press the EMERGCY Softkey.
Nav/Com/
XPDR/Audio
EIS
3) Turn the FMS Knob to select the desired emergency checklist and press the
ENT Key.
GPS Nav
AFCS
4) Press the ENT Key or 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.
Press the CLR Key or UNCHECK Softkey to remove a check mark from an
item.
Procedures
Flight
Planning
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 been 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.
Hazard
Avoidance
7) Press the ENT Key to advance to the next checklist.
8) Press the RETURN Softkey to return to the previous checklist.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
9) Press the EXIT Softkey to exit the Checklist Page and return to the page
last viewed.
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Abnormal Operation
Flight
Instruments
ABNORMAL OPERATION
REVERSIONARY MODE
Nav/Com/
XPDR/Audio
Reversionary display mode can be manually activated by pressing the DISPLAY
BACKUP Button on the audio panel.
EIS
Should a system detected failure occur in either display, the G1000 automatically
enters reversionary mode. In reversionary mode, critical flight instrumentation is
combined with engine instrumentation on the remaining display.
AFCS
NOTE: The Cessna Corvalis/Corvalis TT Airplane Flight Manual (AFM) always
takes precedence over the information found in this section.
AUDIO PANEL FAIL-SAFE OPERATION
Abnormal
Operation
If GPS position is lost, or becomes invalid, selected hazards being displayed on the
Navigation Map Page are removed until GPS position is again established.
Additional
Features
HAZARD DISPLAYS WITH LOSS OF GPS POSITION
Hazard
Avoidance
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 is not available on the
speaker during Fail-safe operation.
Procedures
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected.
Flight
Planning
ABNORMAL COM OPERATION
GPS Nav
Annun/
Alerts
Appendix
Loss of Hazard Functions with Loss of GPS
Position
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
65
UNUSUAL ATTITUDES
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.
The following information is removed from the PFD (and corresponding softkeys
are disabled) when the aircraft experiences unusual attitudes:
• Traffic Annunciations
• AFCS Annunciations
• Flight director Command Bars
• Inset Map
• Temperatures
• DME Information
Window
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
• System Time
• PFD Setup Menu
• Windows displayed in
the lower right corner
of the PFD:
–Timer/References
– Nearest Airports
– Flight Plan
–Messages
–Procedures
– ADF/DME Tuning
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath, and Vertical
Deviation Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
Extreme Pitch Indication
DEAD RECKONING
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.
66
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Abnormal Operation
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
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 the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. The CDI deviation bar is displayed in yellow, but will be removed from the
display after 20 minutes. 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.
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 estimating your 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.
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 compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
EIS
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
navigating in GPS Mode.
Flight
Instruments
Annun/
Alerts
Appendix
CDI ‘DR’ Indication on PFD
Index
Symbolic Aircraft
(Map pages and Inset Map)
Dead Reckoning Indications
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
67
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. This data includes the following:
• Navigation Status Box fields except Active Leg, TAS, and DTK
• GPS Bearing Pointer
• Wind data and pointers in the Wind Data Box on the PFD
• Current Track Indicator
• All Bearing Pointer Distances
• Active Flight Plan distances, bearings, and ETE values
Also, while the G1000 is in DR Mode, the autopilot will couple to GPS for up to 20
minutes. Terrain Proximity, TERRAIN-SVS, and TAWS are also disabled. Additionally,
the accuracy of all nearest information (airports, airspaces, and waypoints) is
questionable. Finally, airspace alerts continue to function, but with degraded
accuracy.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
68
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
G1000 SYSTEM ANNUNCIATIONS
Nav/Com/
XPDR/Audio
System Annunciation
EIS
When an LRU or an LRU function fails, a large red “X” is typically displayed on windows associated with the failed data. Refer to the Corvalis Pilot’s Operating Handbook
(POH) for additional information regarding pilot responses to these annunciations
Comment
AFCS
Attitude and Heading Reference System is aligning.
GPS Nav
Flight
Planning
Procedures
Display system is not receiving attitude information from the
AHRS.
Hazard
Avoidance
Additional
Features
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 POH).
Abnormal
Operation
Display system is not receiving valid transponder information.
Annun/
Alerts
Display system is not receiving valid heading input from
AHRS.
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
69
G1000 SYSTEM ANNUNCIATIONS (CONT.)
System Annunciation
Comment
EIS
Flight
Instruments
Annunciations & Alerts
AFCS
Nav/Com/
XPDR/Audio
Display system is not receiving airspeed input from air data
computer.
Procedures
Flight
Planning
GPS Nav
Display system is not receiving altitude input from the air
data computer.
Additional
Features
Hazard
Avoidance
Display system is not receiving vertical speed input from the
air data computer.
A red ‘X’ through any other display field (such as engine
instrumentation display) indicates that the field is not
receiving valid data.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Other Various Red X
Indications
70
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
Annunciation Window
Text
FUEL PUMP
L-LOW FUEL
Fuel pump is operating
Low fuel in the left tank
R LOW FUEL
Low fuel in the right tank
Single Chime/None
STARTER ENGD
Starter relay has power applied
Single Chime/None
OXYGEN PRES
Single Chime/None
Single Chime/None
Annun/
Alerts
OXYGEN PRES†
Abnormal
Operation
Single Chime/None
OXYGEN QTY
RUDR LMTR *
Pressure above 12,000 ft and
oxygen off
Oxygen outlet pressure below 60
psi
Oxygen outlet pressure below
16.5 psi
Oxygen quantity below 250 psi.
Rudder limter is engaged
Additional
Features
Right Alternator offline
Appendix
Single Chime/None
Single Chime/None
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
*Corvalis only / High pressure oxygen outlet only / †Low pressure oxygen outlet only
190-00567-05 Rev. A
Hazard
Avoidance
R ALT OFF
Procedures
Left Alternator offline
Audio Alert/Voice
Message
Single Chime/”Left
Alternator Out”
Single Chime/”Right
Alternator Out”
Single Chime/”Fuel Pump”
Single Chime/None
OXYGEN
Alerts Window Message
Flight
Planning
Annunciation Window
Text
L ALT OFF
GPS Nav
CAUTION ALERTS
AFCS
Door not secured
Fuel tank is not correctly selected
or in OFF position
No power on the left bus
Chime
No power on the right bus
Chime
Carbon Monoxide level is too high Chime/”Carbon Monoxide”
Low oil pressure
Chime/”Oil Pressure Low”
Nav/Com/
XPDR/Audio
L BUS OFF
R BUS OFF
CO LVL HIGH
OIL PRES LOW
Audio Alert/Voice
Message
(Repeating)
Chime/”Door Open”
Chime/”Fuel Valve”
EIS
DOOR OPEN
FUEL VALVE
Alerts Window Message
Flight
Instruments
WARNING ALERTS
71
ANNUNCIATION ADVISORY
Annunciation Window
Text
AP/TRIM OFF
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Alerts Window Message
Audio Alert
AP/TRIM master switch is in the OFF position
None
OXYGEN ON
Reminder: Turn off oxygen
None
RUDR HOLD *
Rudder hold is engaged
None
SPEED BRAKES
Speed brakes are active
None
* Corvalis TT only
Alerts Window Message
PFD FAN FAIL – The cooling fan for the PFD is inoperative.
MFD FAN FAIL – The cooling fan for the MFD is inoperative.
AVIONICS FAN – The cooling fan for remote avionics is inoperative.
TIMER ZERO – Timer has counted down to zero.
FUEL IMBAL – Fuel imbalance is greater than 10 gallons.
LOW MAN PRES – Manifold pressure is below 15 in.
VAPOR SUPPR – Turn on Vapor Suppression.*
Audio Alert
None
None
None
“Timer Expired”
None
None
None
* Corvalis TT only
CO GUARDIAN MESSAGES
Alerts Window Message
CO DET SRVC – The carbon
monoxide detector needs
service.
CO DET FAIL – The carbon
monoxide detector is inoperative.
Comments
There is a problem within the CO Guardian that requires
services.
Loss of communication between the G1000 and the CO
Guardian.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
MESSAGE ADVISORY ALERTS
72
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
Condition
Flight
Instruments
AFCS ALERTS
Annunciation 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
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.
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, the aural alert will be heard.
Preflight system test has failed.
EIS
Pitch Failure
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Preflight Test
Procedures
Aileron Mistrim Right
Flight
Planning
Aileron Mistrim Left
GPS Nav
Elevator Mistrim Down
AFCS
Elevator Mistrim Up
Nav/Com/
XPDR/Audio
System Failure
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
73
Flight
Instruments
Annunciations & Alerts
TERRAIN-SVS ALERTS
Abnormal
Operation
Annun/
Alerts
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”
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”
TERRAIN-SVS SYSTEM STATUS ANNUNCIATIONS
TERRAIN-SVS Page
Annunciation
Aural
Message
TERRAIN TEST
None
None
“Terrain System
Test OK”
Terrain Alerting is disabled
None
None
Terrain System Test Fail
TERRAIN FAIL
“Terrain System
Failure”
NO GPS POSITION
“Terrain System
Not Available”
Alert Type
PFD/MFD Alert
Annunciation
System Test in Progress
System Test Pass
Appendix
MFD
Pop-Up Alert
Reduced Required Terrain
Clearance Warning (RTC)
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Alert Type
PFD/MFD
TERRAIN-SVS
Page
Annunciation
Index
No GPS position
None
74
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
TERRAIN FAIL
“Terrain System
Failure”
TERRAIN DATABASE FAILURE
None
None
“Terrain System
Not Available”
None
“Terrain System
Available”
Nav/Com/
XPDR/Audio
None
None
MFD
Pop-Up Alert
Excessive Descent
Rate Warning (EDR)
or
Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
Appendix
or
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
Annun/
Alerts
Imminent Terrain
Impact Warning (ITI)
“Pull Up”
Abnormal
Operation
Reduced Required
Terrain Clearance
Warning (RTC)
Aural Message
Additional
Features
PFD/MFD
TAWS-B Page
Annunciation
Hazard
Avoidance
Alert Type
Procedures
TAWS-B ALERTS
Flight
Planning
Sufficient GPS signal
received after loss or
database coverage area
entered
GPS Nav
Excessively degraded
GPS signal or out of
database coverage area
AFCS
MFD Terrain or Obstacle
database unavailable
or invalid. System
operating with PFD
Terrain or Obstacle
databases
Aural
Message
EIS
Terrain or Obstacle
database unavailable or
invalid, invalid software
configuration, system
audio fault
TERRAIN-SVS Page
Annunciation
Flight
Instruments
PFD/MFD Alert
Annunciation
Alert Type
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
75
Alert Type
PFD/MFD
TAWS-B Page
Annunciation
Reduced Required
Obstacle Clearance
Warning (ROC)
MFD
Pop-Up Alert
or
Imminent Obstacle
Impact Warning
(IOI)
or
Reduced Required
Terrain Clearance
Caution (RTC)
or
Imminent Terrain
Impact Caution (ITI)
or
Reduced Required
Obstacle Clearance
Caution (ROC)
or
Imminent Obstacle
Impact Caution (IOI)
or
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
Aural Message
“Obstacle, Obstacle; Pull
Up, Pull Up”
or
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
“Obstacle Ahead, Pull Up;
Obstacle Ahead, Pull Up”
or
“Obstacle, Obstacle; Pull
Up, Pull Up”
“Caution, Terrain; Caution,
Terrain”
or
“Terrain Ahead; Terrain
Ahead”
“Terrain Ahead; Terrain
Ahead”
or
“Caution, Terrain; Caution,
Terrain”
“Caution, Obstacle; Caution, Obstacle”
or
“Obstacle Ahead; Obstacle
Ahead”
“Obstacle Ahead; Obstacle
Ahead”
or
“Caution, Obstacle; Caution, Obstacle”
Premature Descent
Alert Caution (PDA)
Altitude Callout
“500”
“Too Low, Terrain”
None
None
Excessive Descent
Rate Caution (EDR)
76
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
“Five-Hundred”
“Sink Rate”
190-00567-05 Rev. A
Annunciations & Alerts
PFD/MFD
TAWS-B Page
Annunciation
Aural Message
or
“Don’t Sink”
or
“Too Low, Terrain”
Negative Climb
Rate Caution (NCR)
EIS
MFD
Pop-Up Alert
Flight
Instruments
Alert Type
Nav/Com/
XPDR/Audio
TAWS-B System Status Annunciations
TAWS-B Page
Annunciation
Aural
Message
TAWS TEST
None
None
“TAWS System
Test OK”
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”
TERRAIN DATABASE FAILURE
None
NO GPS POSITION
“TAWS Not
Available”
None
“TAWS Not
Available”
None
“TAWS Available”
System Test Pass
None
Procedures
Hazard
Avoidance
Appendix
77
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Annun/
Alerts
None
Abnormal
Operation
Excessively degraded
GPS signal or out of
database coverage
area
Additional
Features
None
No GPS position
190-00567-05 Rev. A
Flight
Planning
MFD Terrain or
Obstacle database
unavailable or invalid.
System operating
with PFD Terrain or
Obstacle databases
Sufficient GPS signal
received after loss or
database coverage
area entered
GPS Nav
System Test in
Progress
AFCS
PFD/MFD Alert
Annunciation
Alert Type
VOICE ALERTS
Voice Alert
“Minimums, minimums”
EIS
Flight
Instruments
Annunciations & Alerts
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
“Vertical track”
“Traffic”
“Traffic Not Available”
“Traffic, Traffic”
“Traffic Advisory System
Test Passed”
“Traffic Advisory System
Test Failed”
Description
The aircraft has descended below the preset barometric minimum
descent altitude.
The aircraft is one minute from Top of Descent. Issued only when
vertical navigation is enabled.
Played when a Traffic Advisory (TA) is issued.
The aircraft is outside the Traffic Information Service (TIS) coverage area.
Played when a Traffic Advisory (TA) is issued (TAS system).
Played when the TAS system passes a pilot-initiated self test.
Played when the TAS system fails a pilot-initiated self test.
MFD & PFD MESSAGE ADVISORIES
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 config error.
Config service req’d.
78
Comments
The pilot profile data was lost. System reverts
to default pilot profile and settings. The pilot
may reconfigure the MFD & PFDs with preferred
settings, if desired.
The MFD and PFDs are not communicating with
each other. The system should be serviced.
The PFD and/or MFD self-test has detected a
problem. The system should be serviced.
The PFD and/or MFD has incorrect software
installed. The system should be serviced.
The PFD configuration settings do not match
backup configuration memory. The system
should be serviced.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
AFCS
The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the system should
be serviced.
GPS Nav
Flight
Planning
A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The system should be serviced if
the problem persists.
Procedures
The PFD1 configuration module backup memory
has failed. The system should be serviced.
Hazard
Avoidance
The PFD1 voltage is low. The system should be
serviced.
The MFD voltage is low. The system should be
serviced.
Additional
Features
DATABASE MESSAGE ADVISORIES
Comments
The MFD and/or PFD detected a failure in the
navigation database. Attempt to reload the
aviation database. If problem persists, the
system should be serviced.
Annun/
Alerts
Appendix
The MFD and/or PFD detected a failure in the
basemap database.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index
190-00567-05 Rev. A
Abnormal
Operation
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.
Nav/Com/
XPDR/Audio
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 [key name]
Key is stuck.
MFD1 KEYSTK – MFD [key name]
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 configuration settings do not match
backup configuration memory. The system
should be serviced.
The MFD and PFDs have different software versions
installed. The system should be serviced.
EIS
Message
MFD1 CONFIG – MFD1 config
error. Config service req’d.
Flight
Instruments
MFD & PFD MESSAGE ADVISORIES (CONT.)
79
DATABASE MESSAGE ADVISORIES (CONT.)
Message
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.
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.
Comments
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.
The obstacle database is present on another LRU,
but is missing on the specified LRU.
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.
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
80
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
Flight
Instruments
DATABASE MESSAGE ADVISORIES (CONT.)
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
The MFD and/or PFD detected a failure in more
than one database. If problem persists, the
system should be serviced.
Hazard
Avoidance
System has updated the active navigation
database from the standby navigation database.
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.
Additional
Features
Abnormal
Operation
MFD1 DB ERR – MFD1 multiple
database errors exists.
PFD1 DB ERR – PFD1 multiple
database errors exists.
NAV DB UPDATED – Active
navigation database updated.
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
EIS
Message
Comments
MFD1 DB ERR – MFD1 Chartview The MFD detected a failure in the ChartView
database error exists.
database (optional feature). Ensure that the
data card is properly inserted. Replace data
card. If problem persists, the system should be
serviced.
MFD1 DB ERR – MFD1 FliteCharts The MFD detected a failure in the FliteCharts
database error exists.
database (optional feature). Ensure that the
data card is properly inserted. Replace data
card. If problem persists, the system should be
serviced.
MFD1 DB ERR – MFD1 Airport
The MFD and/or PFD detected a failure in the
Directory database error exists.
Airport Directory database. Ensure that the data
card is properly inserted. Replace data card. If
PFD1 DB ERR – PFD1 Airport
problem persists, the system should be serviced.
Directory database error exists.
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
81
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
DATABASE MESSAGE ADVISORIES (CONT.)
Message
DB MISMATCH – Standby
Navigation database mismatch.
Comments
The PFD and MFD have different standby
navigation 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 – Terrain database The PFD and MFD have different terrain
mismatch.
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 – Obstacle
The PFD and MFD have different obstacle
database mismatch.
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 mismatch.
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.
TERRAIN DSP – [PFD1, MFD1]
One of the terrain, airport terrain, or obstacle
Terrain awareness display
databases required for TAWS in the specified PFD
unavailable.
or MFD is missing or invalid.
82
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
Procedures
Comments
Hazard
Avoidance
The GIA1 and/or GIA2 configuration settings
do not match backup configuration memory.
The system should be serviced.
Additional
Features
Abnormal
Operation
The GIA1 and/or GIA2 have an error in the
audio configuration. The system should be
serviced.
Index
83
Appendix
The GIA1 and/or GIA2 temperature is too
high. If problem persists, the system should be
serviced.
Annun/
Alerts
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Flight
Planning
190-00567-05 Rev. A
GPS Nav
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.
AFCS
Message
Nav/Com/
XPDR/Audio
GIA 63 MESSAGE ADVISORIES
EIS
Message
Comments
GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.
The audio panel is unavailable. The system
should be serviced.
GMA1 CONFIG – GMA1 config
The audio panel configuration settings do not
error. Config service req’d.
match backup configuration memory. The system
should be serviced.
MANIFEST – GMA1 software
The audio panel has incorrect software installed.
mismatch, communication halted.
The system should be serviced.
GMA1 SERVICE – GMA1 needs
The audio panel self-test has detected a problem
service. Return unit for repair.
in the unit. Certain audio functions may still be
available, and the audio panel may still be usable.
The system should be serviced when possible.
Flight
Instruments
GMA 1347 MESSAGE ADVISORIES
GIA 63 MESSAGE ADVISORIES (CONT.)
Message
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
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.
Comments
The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be
serviced.
The GIA1 and/or GIA 2 has incorrect software
installed. The system should be serviced.
Incorrect servo software is installed, or gain
settings are incorrect.
COM1 and/or COM2 software mismatch. The
system should be serviced.
NAV1 and/or NAV2 software mismatch. The
system should be serviced.
The system has detected an over temperature condition in COM1 and/or COM2. The
transmitter is operating at reduced power. If
the problem persists, the system should be
serviced.
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
84
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
GPS Nav
Flight
Planning
The COM1 and/or COM2 configuration
settings do not match backup configuration
memory. The system should be serviced.
AFCS
Additional
Features
LOI – GPS integrity lost. Crosscheck
Loss of GPS integrity monitoring.
with other NAVS.
GPS NAV LOST – Loss of GPS naviga- Loss of GPS navigation due to insufficient
tion. Insufficient satellites.
satellites.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to position error.
navigation. Position error.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to GPS failure.
navigation. GPS fail.
ABORT APR – Loss of GPS navigation.
Abort approach due to loss of GPS navigation.
Abort approach.
TRUE APR – True north approach.
Displayed after passing the first waypoint of
Change hdg reference to TRUE.
a true north approach when the nav angle is
set to ‘AUTO’.
Hazard
Avoidance
GPS satellite coverage is insufficient to perform
Receiver Autonomous Integrity Monitoring
(RAIM) from the FAF to the MAP waypoints.
Procedures
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.
Nav/Com/
XPDR/Audio
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
Comments
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.
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.
EIS
Message
COM1 PTT – COM1 push-to-talk key
is stuck.
COM2 PTT – COM2 push-to-talk key
is stuck.
Flight
Instruments
GIA 63 MESSAGE ADVISORIES (CONT.)
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
85
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
GIA 63 MESSAGE ADVISORIES (CONT.)
Message
GPS1 FAIL – GPS1 is inoperative.
Comments
A failure has been detected in the GPS1 and/or
GPS2 receiver. The receiver is unavailable. The
system should be serviced.
GPS2 FAIL – GPS2 is inoperative.
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.
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 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.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver
may still be available. The system should be
serviced when possible.
GIA 63W MESSAGE ADVISORIES
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
86
Comments
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Annunciations & Alerts
Comments
The GIA1 and/or GIA2 have an error in the
audio configuration. The system should be
serviced.
EIS
Nav/Com/
XPDR/Audio
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
AFCS
GPS Nav
The GIA1 and/or GIA2 temperature is too
high. If problem persists, the system should be
serviced.
Flight
Planning
The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be
serviced.
Procedures
Hazard
Avoidance
A GIA mismatch has been detected, where only
one is SBAS capable.
Additional
Features
Abnormal
Operation
The GIA1 and/or GIA 2 has incorrect software
installed. The system should be serviced.
Annun/
Alerts
Incorrect servo software is installed, or gain
settings are incorrect.
Appendix
Message
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.
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.
Flight
Instruments
GIA 63W MESSAGE ADVISORIES (CONT.)
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
87
GIA 63W MESSAGE ADVISORIES (CONT.)
Message
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.
Comments
COM1 and/or COM2 software mismatch. The
system should be serviced.
NAV1 and/or NAV2 software mismatch. The
system should be serviced.
The system has detected an over temperature
condition in COM1 and/or COM2. The transmitter
is operating at reduced power. If the problem
persists, the system should be serviced.
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.
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.
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.
The COM1 and/or COM2 configuration settings
do not match backup configuration memory.
The system should be serviced.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
88
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190-00567-05 Rev. A
Annunciations & Alerts
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’.
Flight
Planning
Procedures
A failure has been detected in the GPS1 and/
or GPS2 receiver. The receiver may still be
available. The system should be serviced.
Hazard
Avoidance
Additional
Features
A failure has been detected in the NAV1 and/
or NAV2 receiver. The receiver may still be
available. The system should be serviced.
Abnormal
Operation
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.
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Annun/
Alerts
190-00567-05 Rev. A
Loss of GPS navigation due to GPS failure.
GPS Nav
G/S2 FAIL – G/S2 is inoperative.
AFCS
G/S1 FAIL – G/S1 is inoperative.
Loss of GPS navigation due to position error.
Nav/Com/
XPDR/Audio
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.
Comments
GPS integrity is insufficient for the current phase
of flight.
Loss of GPS navigation due to insufficient
satellites.
EIS
Message
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.
Flight
Instruments
GIA 63W MESSAGE ADVISORIES (CONT.)
89
GIA 63W MESSAGE ADVISORIES (CONT.)
Message
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
FAILED PATH – A data path has
failed.
Comments
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The system should be serviced
when possible.
A data path connected to the GDU or the GIA
63/W has failed
GEA 71 MESSAGE ADVISORIES
Message
Comments
GEA1 CONFIG – GEA1 config error. The GEA1 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
system should be serviced.
MANIFEST – GEA1 software
The #1 GEA 71 has incorrect software installed.
mismatch, communication halted. The system should be serviced.
GTX 33 MESSAGE ADVISORIES
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.
Comments
The transponder configuration settings do not
match those of backup configuration memory.
The system should be serviced.
The transponder has incorrect software installed.
The system should be serviced.
The #1 transponder should be serviced when
possible.
There is no communication with the #1
transponder.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
90
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190-00567-05 Rev. A
Annunciations & Alerts
Abnormal
Operation
Comments
A fault has occurred in the #1 GMU 44.
Heading is flagged as invalid. The AHRS uses
GPS for backup mode operation. The system
should be serviced.
The GMU 44 has incorrect software installed.
The system should be serviced.
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Annun/
Alerts
190-00567-05 Rev. A
Additional
Features
MANIFEST – GMU1 software
mismatch, communication halted.
Hazard
Avoidance
GMU 44 MESSAGE ADVISORIES
Message
HDG FAULT – AHRS1
magnetometer fault has occurred.
Procedures
MANIFEST – GRS1 software
mismatch, communication halted.
Flight
Planning
GEO LIMITS – AHRS1 too far
North/South, no magnetic compass.
GPS Nav
AHRS1 GPS – AHRS1 not receiving
backup GPS information.
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS1 SRVC – AHRS1 Magneticfield model needs update.
AFCS
AHRS1 GPS – AHRS1 not receiving
any GPS information.
Nav/Com/
XPDR/Audio
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 system should be serviced.
The #1 AHRS is using the backup GPS path.
Primary GPS path has failed. The system should
be serviced when possible.
The #1 AHRS is not receiving any or any useful
GPS information. Check AFMS limitations. The
system should be serviced.
The #1 AHRS is not receiving backup GPS
information. The system should be serviced.
The #1 AHRS is operating exclusively in no-GPS
mode. The 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 system should be serviced.
EIS
Message
AHRS1 TAS – AHRS1 not receiving
valid airspeed.
Flight
Instruments
GRS 77 MESSAGE ADVISORIES
91
GDL 69A MESSAGE ADVISORIES
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
GDL69 FAIL – GDL 69 has failed.
MANIFEST – GDL software
mismatch, communication halted.
Comments
GDL 69 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
A failure has been detected in the GDL 69. The
receiver is unavailable. The system should be
serviced
The GDL 69 has incorrect software installed.
The system should be serviced.
GDC 74A MESSAGE ADVISORIES
Message
MANIFEST – GDC1 software
mismatch, communication halted.
Comments
The GDC 74A has incorrect software installed.
The system should be serviced.
GCU 476 MESSAGE ADVISORIES
Message
GCU CNFG – GCU Config error.
Config service req’d.
Comments
GCU 476 configuration settings do not match
those of backup configuration memory. The
system should be serviced.
GCU FAIL – GCU is inoperative.
A failure has been detected in the GCU 476.
The GCU 476 is unavailable.
MANIFEST – GCU software
The GCU 476 has incorrect software installed.
mismatch, communication halted.
The G1000 system should be serviced.
GCU KEYSTK – GCU [key name] Key A key is stuck on the GCU 476 bezel. Attempt
is stuck.
to free the stuck key by pressing it several
times. The system should be serviced if the
problem persists.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
92
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190-00567-05 Rev. A
Annunciations & Alerts
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
Upon power-up, the system detects that a
stored flight plan waypoint is locked. This
occurs when an aviation 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
waypoint moved.
coordinate has changed due to a new aviation
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
Verify user modified procedures.
procedures that have been manually edited.
This alert is issued only after an aviation
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
Verify stored airways.
an airway that is no longer consistent with
the aviation database. This alert is issued only
after an aviation database update. Verify use
of airways in stored flight plans and reload
airways as needed.
EIS
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Flight
Instruments
MISCELLANEOUS MESSAGE ADVISORIES
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
93
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message
FPL TRUNC – Flight plan has been
truncated.
Comments
This occurs when a newly installed aviation
database eliminates an obsolete 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
locked flight plan.
a stored flight plan that contains locked
waypoint. Remove locked waypoint from flight
plan. Update flight plan with current waypoint.
WPT ARRIVAL – Arriving at
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint -[xxxx]
waypoint name.
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
Special use airspace is ahead of aircraft. The
less than 10 minutes.
aircraft will penetrate the airspace within 10
minutes.
ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the
ahead.
aircraft position.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the
than 2 nm.
aircraft position.
APR INACTV – Approach is not
The system notifies the pilot that the loaded
active.
approach is not active. Activate approach when
required.
SLCT FREQ – Select appropriate
The system notifies the pilot to load the
frequency for approach.
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.
SLCT NAV – Select NAV on CDI for The system notifies the pilot to set the CDI to
approach.
the correct NAV receiver. Set the CDI to the
correct NAV receiver.
94
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Annunciations & Alerts
Comments
Bad parallel track geometry.
EIS
Invalid leg type for parallel offset.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
95
Flight
Planning
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
GPS Nav
190-00567-05 Rev. A
AFCS
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.
VNV – Unavailable. Unsupported
The lateral flight plan contains a procedure
leg type in flight plan.
turn, vector, or other unsupported leg type
prior to the active vertical waypoint. This
prevents vertical guidance to the active vertical
waypoint.
VNV – Unavailable. Excessive track The current track angle error exceeds the limit,
angle error.
causing the vertical deviation to go invalid.
VNV – Unavailable. Excessive
The current crosstrack exceeds the limit,
crosstrack error.
causing vertical deviation to go invalid.
VNV – Unavailable. Parallel course A parallel course has been selected, causing
selected.
the vertical deviation to go invalid.
NON WGS84 WPT – Do not use GPS The position of the selected waypoint [xxxx]
navigation to [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.
TRAFFIC FAIL – Traffic device has
The system is no longer receiving data from
failed.
the traffic system. The traffic device should be
serviced.
FAILED PATH – A data path has
A data path connected to the GDU or the GIA
failed.
63/W has failed.
Nav/Com/
XPDR/Audio
Message
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.
Flight
Instruments
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message
SRMSCP FAIL – Stormscope has
failed
MAG VAR WARN – Large magnetic
variance. Verify all course angles.
Comments
Stormscope has failed. The system should be
serviced.
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
Synthetic Vision is disabled because the aircraft
available terrain region.
is not within the boundaries of the installed
terrain database.
SVS – SVS DISABLED: Terrain DB
Synthetic Vision is disabled because a terrain
resolution too low.
database of sufficient resolution (9 arc-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
LOC1 / [LOC ID] is [CRS]°.
localizer course by more than 10 degrees.
CHECK CRS – Database course for Selected course for LOC2 differs from published
LOC2 / [LOC ID] is [CRS]°.
localizer course by more than 10 degrees.
[PFD1 or MFD1] CARD 1 REM –
The SD card was removed from the top card
Card 1 was removed. Reinsert card. slot of the PFD or MFD. The SD card needs to
be reinserted.
[PFD1 or MFD1] CARD 2 REM –
The SD card was removed from the bottom
Card 2 was removed. Reinsert card. card slot of the PFD or MFD. The SD card
needs to be reinserted.
[PFD1 or MFD1] CARD 1 ERR –
The SD card in the top card slot of the PFD or
Card 1 is invalid.
MFD contains invalid data.
[PFD1 or MFD1] CARD 2 ERR –
The SD card in the bottom card slot of the PFD
Card 2 is invalid.
or MFD contains invalid data.
TRN AUD FAIL – Trn Awareness
The audio source for terrain awareness is
audio source unavailable.
offline. Check GIA 1 or GIA 2.
TERRAIN AUD CFG – Trn Awareness Terrain audio alerts are not configured properly.
audio config error. Service req’d.
The system should be serviced.
96
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Annunciations & Alerts
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Description
A flight plan file stored on the SD card was
successfully imported as a stored flight
plan.
‘File contained user waypoints only.
The file stored on the SD card did not
User waypoints imported successfully.
contain a flight plan, only user waypoints.
No stored flight plan data was modified.’ These waypoints have been saved to the
system user waypoints. No flight plans
stored in the system have been modified.
‘No flight plan files found to import.’
The SD card contains no flight plan data.
‘Flight plan import failed.’
Flight plan data was not successfully
imported from the SD card.
‘Flight plan partially imported.’
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.
‘File contained user waypoints only.’
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.
‘Too many points. Flight plan truncated.’ 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.
‘Some waypoints not loaded. Waypoints The flight plan on the SD card contains one
locked.’
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.
EIS
Flight Plan Import/Export Results
‘Flight plan successfully imported.’
Flight
Instruments
FLIGHT PLAN IMPORT/EXPORT MESSAGES
In some circumstances, some messages may appear in conjunction with others.
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
97
FLIGHT PLAN IMPORT/EXPORT MESSAGES (CONT.)
Flight Plan Import/Export Results
‘User waypoint database full. Not all
loaded.’
‘One or more user waypoints renamed.’
‘Flight plan successfully exported.’
‘Flight plan export failed.’
Description
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
98
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Appendix
Flight
Instruments
APPENDIX
PFD SOFTKEY MAP
EIS
ADF/DME
ALERTS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Top Level PFD Softkeys
ADF/DME
ALERTS
Flight
Planning
METAR
TRFC-1
ALERTS
Procedures
STRMSCP
WX LGND
Hazard
Avoidance
Press the BACK Softkey to return to
the top-level softkeys.
TRFC-2
Additional
Features
Inset Map Softkeys
Level 2
Level 3
Description
Displays Inset Map in PFD lower left corner
INSET
Selects desired amount of map detail; cycles
through declutter levels:
DCLTR (No Declutter): All map features
visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the
active flight plan
190-00567-05 Rev. A
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99
Index
DCLTR (3)
Appendix
Removes Inset Map
Annun/
Alerts
OFF
Abnormal
Operation
Level 1
Level 1
Level 2
WX LGND
TRAFFIC
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
AFCS
TOPO
TERRAIN
Flight
Planning
GPS Nav
STRMSCP
NEXRAD
Procedures
XM LTNG
Description
Displays icon and age on the Inset Map for
the selected weather products (optional)
Cycles through traffic display options:
TRFC-1: Traffic displayed on inset map
TRFC-2: Traffic Map Page is displayed in
the inset map window
Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation
scale on Inset Map
Displays terrain information on Inset Map
Displays Stormscope lightning data on the
Inset Map within a 200 nm radius of the
aircraft (optional)
Displays NEXRAD weather and coverage
information on Inset Map (optional feature)
Displays XM lightning information on Inset
Map (optional)
Displays METAR flags on airport symbols
shown on the Inset Map (optional)
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
METAR
Level 3
100
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Appendix
ADF/DME
ALERTS
ALT UNIT
HSI FMT
Flight
Instruments
SYN VIS
ALERTS
EIS
Select the BACK Softkey
to return to the top-level softkeys
Nav/Com/
XPDR/Audio
METERS
BACK
ARC HSI
IN
HPA
ALERTS
AFCS
360 HSI
GPS Nav
ALERTS
ALERTS
SYN TERR HRZN HDG APTSIGNS
Flight
Planning
PATHWAY
ALERTS
Procedures
PFD Configuration Softkeys
Level 2
Level 3
PFD
Appendix
HRZN HDG Displays compass heading along the
Zero-Pitch line
Annun/
Alerts
SYN TERR
Abnormal
Operation
PATHWAY
Displays second-level softkeys for
additional PFD configurations
Displays the softkeys for enabling or
disabling Synthetic Vision features
Displays rectangular boxes representing
the horizontal and vertical flight path of
the active flight plan
Enables synthetic terrain depiction
Additional
Features
SYN VIS
Description
Hazard
Avoidance
Level 1
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
101
Level 1
Level 2
Level 3
APTSIGNS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
DFLTS
AFCS
WIND
GPS Nav
OPTN 1
OPTN 2
Flight
Planning
OPTN 3
OFF
Hazard
Avoidance
Procedures
DME
BRG1
Additional
Features
HSI FRMT
Abnormal
Operation
360 HSI
ARC HSI
Annun/
Alerts
BRG2
Index
Appendix
ALT UNIT
102
Description
Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings, including changing units to standard
Displays softkeys to select wind data
parameters
Wind direction arrows with headwind
and crosswind components
Wind direction arrow and speed
Wind direction arrow with headwind/
tailwind and crosswind components
Information not displayed
Displays the DME Information Window
Cycles the Bearing 1 Information
Window through NAV1 or GPS/waypoint
identifier and GPS-derived distance
information, and ADF/frequency.
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree format
Displays the HSI in an arc format
Cycles the Bearing 2 Information Window through NAV2 or GPS/waypoint
identifier and GPS-derived distance
information, and ADF/frequency.
Displays softkeys for setting the altimeter
and BARO settings to metric units
METERS
When enabled, displays altimeter in
meters
IN
Select to display the BARO setting as
inches of mercury
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Appendix
Level 2
Level 3
HPA
Select to display the BARO setting as
hectopacals
Sets barometric pressure to 29.92 in Hg
(1013 hPa)
Nav/Com/
XPDR/Audio
ADF/DME
EIS
STD BARO
Description
Flight
Instruments
Level 1
ALERTS
AFCS
ALERTS
GPS Nav
Press the BACK Softkey to return
to the top-level softkeys.
ALERTS
Flight
Planning
Press the BACK Softkey to return
to the previous level softkeys.
Procedures
Transponder Softkeys
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
103
Flight
Instruments
Appendix
Level 1
Level 2
Level 3
Displays transponder mode selection softkeys
XPDR
0—7
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
interrogations)
Selects Mode C – Altitude Reporting Mode
(transponder replies to identification and
altitude interrogations)
Manually selects 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.
Automatically enters the VFR code (1200
in the U.S.A. only)
Displays transponder code selection softkeys 0-7
Use numbers to enter code
BKSP
Removes numbers entered, one at a time
EIS
STBY
Nav/Com/
XPDR/Audio
ON
AFCS
ALT
Flight
Planning
GPS Nav
GND
VFR
Additional
Features
Hazard
Avoidance
Procedures
CODE
TMR/REF
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
NRST
Displays Nearest Airports Window
ALERTS
Displays Alerts Window
IDENT
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Description
104
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Appendix
DCLTR
MAP
SYSTEM
SHW CHRT
CHKLIST
(optional)
(optional)
Flight
Instruments
MFD SOFTKEY MAP
DCLTR-1
EIS
DCLTR-2
TRAFFIC
PROFILE
TOPO
TERRAIN
AIRWAYS
Press the BACK Softkey on this
level to return to the top softkey level.
DCLTR-3
(optional)
STRMSCP
(optional)
NEXRAD
(optional)
XM LTNG
(optional)
METAR
(optional)
LEGEND
BACK
Nav/Com/
XPDR/Audio
(Default softkey
is dependant on
the selection made
in the map setup
options)
AIRWY ON
AFCS
AIRWY LO
Press the SYSTEM Softkey to
return to the default page level.
AIRWAY HI
(optional)
OXYGEN
DCLTR
ASSIST
CO RST
DEC FUEL
INC FUEL
RST FUEL
GPS Nav
SYSTEM
SYSTEM
CHECK
EXIT
Flight
Planning
The CHECK Softkey changes to UNCHECK when
the checklist item is already checked
EMERGCY
Procedures
MFD Softkeys
Level 1
Level 2
Description
Hazard
Avoidance
Access the EIS functions
SYSTEM
OXYGEN
Turns the oxygen system on or off (optional)
DCLTR
Cycles the EGT and CHT cylinder temperatures
on and off
Accesses the Engine Leaning Assist Mode
ASSIST
Abnormal
Operation
Returns to the top-level EIS display
Additional
Features
SYSTEM
Resets the CO Guardian and acknowledges an
alert
DEC FUEL Decreases the gallons of fuel remaining (GAL
REM) in 1-gallon increments
INC FUEL Increases the gallons of fuel remaining (GAL
REM) in 1-gallon increments
RST FUEL Resets the fuel remaining to 98 or 102 gallons
CO RST
Appendix
Index
TRAFFIC
190-00567-05 Rev. A
Annun/
Alerts
Enables second-level Navigation Map softkeys
MAP
Displays traffic information on Navigation Map
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
105
Appendix
Flight
Instruments
Level 1
PROFILE
Nav/Com/
XPDR/Audio
EIS
TOPO
TERRAIN
Description
Displays/removes Profile View on Navigation
Map Page
Displays topographical data (e.g., coastlines,
terrain, rivers, lakes) and elevation scale on
Navigation Map
Displays terrain information on Navigation Map
Displays airways on the map; cycles through the
following:
AIRWAYS: No airways are displayed
AIRWY ON: All airways are displayed
AIRWY LO: Only low altitude airways are
displayed
AIRWY HI: Only high altitude airways are
displayed
STRMSCP Press to display the Stormscope lightning data
on the Inset Map (within a 200 nm radius of the
aircraft)
NEXRAD Displays NEXRAD weather and coverage
information on Navigation Map (optional)
XM LTNG Displays XM lightning information on Navigation
Map (optional)
Displays METAR flags on airport symbols shown
METAR
on the Inset Map (optional)
LEGEND Displays the legend for the selected weather
products. Available only when NEXRAD, XM
LTNG, and/or METAR softkeys are selected.
Returns to top-level softkeys
BACK
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
AIRWAYS
DCLTR (3)
Index
Appendix
Annun/
Alerts
Level 2
106
Selects desired amount of map detail; cycles
through declutter levels:
DCLTR (No Declutter): All map features visible
DCLTR-1: Declutters land data
DCLTR-2: Declutters land and SUA data
DCLTR-3: Removes everything except the active
flight plan
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Appendix
Level 2
Description
Flight
Instruments
Level 1
CHKLIST
CHECK
Pressing this softkey checks off a checklist item.
If an item is already checked, an UNCHECK
Softkey is displayed.
Press to exit the checklist
Nav/Com/
XPDR/Audio
EXIT
EIS
When available, displays optional airport and
terminal procedure charts
When available, displays optional checklists
SHW CHRT
AFCS
EMERGCY Press to display the emergency checklist
LOADING UPDATED DATABASES
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
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.
If an error occurs during synchronization, an error message will be displayed,
followed by the affected display in the Sync Status section of the Database Window. If
synchronization completes on one display, but an error occurs on another, the error
message will be displayed with the affected displays listed after it. When an error
message is displayed, the problem must be corrected before synchronization can be
completed. A power cycle is required to restart synchronization when ‘Card Full’ or
‘Err’ is shown.
Procedures
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 AUXSYSTEM STATUS Page.
Flight
Planning
GPS Nav
CAUTION: Never disconnect power to the system when loading a database.
Power interruption during the database loading process could result in maintenance being required to reboot the system.
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
107
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
Loading Garmin Database Updates
1) With system power OFF, remove the MFD database card from the bottom
card slot of the MFD.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
2) Update the Garmin databases on the MFD card.
Flight
Planning
3) Insert the MFD database card into the bottom card slot of the MFD.
Procedures
4) Apply power to the system, check that the databases are initialized
and displayed on the power-up screen. 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.
Hazard
Avoidance
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.
Additional
Features
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.
Abnormal
Operation
9) Remove and reapply power to the system.
10) Turn the large FMS Knob to select the AUX Page group on the MFD.
Annun/
Alerts
11) Turn the small FMS Knob to select the System Status Page.
Index
Appendix
12) Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct
database cycle information is shown for each database for each display.
108
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Appendix
The Navigation Database that is loaded to internal memory as the active database
will be used by the system.
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
5) After the update completes, the display starts in normal mode.
Procedures
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.
Flight
Planning
2) Turn the system ON. A prompt is displayed in the upper left corner of the
display:
GPS Nav
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).
AFCS
Nav/Com/
XPDR/Audio
NOTE: Loading the Navigation Database as the active database prior to its
effective date will result in the expiration date on the power-up screen and
the effective date on the AUX-System Status Page being displayed in yellow.
EIS
Flight
Instruments
Loading the Active Navigation Database
Hazard
Avoidance
6) Turn the system OFF and remove the SD card from the top card slot.
7) Repeat steps 1 through 6 for the other displays (PFD1 or MFD).
Additional
Features
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.
Annun/
Alerts
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.
Abnormal
Operation
10) Turn the small FMS Knob to select the System Status Page.
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
109
Loading the Standby Navigation Database
The purpose of the Standby Navigation Database is to allow the loading of the
next cycle of the Navigation Database to the bottom SD card, prior to its effective
date. (The Navigation Database is available seven days prior to its effective date.)
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
NOTE: After the navigation database is loaded or copied, the top SD card
may be removed.
AFCS
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 each PFD and the
MFD.
GPS Nav
3) Turn the system ON. A prompt is displayed.
Flight
Planning
4) Press the YES Softkey. The navigation database is copied to the SD card in
the bottom card slot of the MFD.
Procedures
5) After the navigation database files are copied to the bottom SD card, press
any key to verify, as instructed.
6) After database verification is complete, press any key to continue as
instructed on the display.
Additional
Features
Hazard
Avoidance
7) 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.
8) Press the ENT Key to acknowledge the startup screen.
9) Turn the large FMS Knob to select the AUX Page group on the MFD.
Abnormal
Operation
10) Turn the small FMS Knob to select the System Status Page.
Appendix
Annun/
Alerts
11) The new database is copied to the SD card in the bottom card slot of each
PFD. Progress can be monitored in the SYNC STATUS field. When copying
is finished, ‘Complete’ is displayed.
NOTE: During the synchronization process, version differences between
standby navigation databases will exist. This will result in the system
displaying a ‘DB Mismatch’ alert for the standby navigation databases. This
alert will remain until the next power cycle.
Index
110
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Appendix
Flight
Instruments
12) Turn system power OFF.
13) Remove the SD card from the top card slot of the MFD.
14) Turn system power ON.
EIS
15) Press the ENT Key to acknowledge the startup screen.
16) Turn the large FMS Knob to select the AUX Page group on the MFD.
Nav/Com/
XPDR/Audio
17) Turn the small FMS Knob to select the System Status Page.
AFCS
18) 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.
Flight
Planning
Procedures
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 the
following figure. 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.
GPS Nav
Magnetic Field Variation Database Update
Hazard
Avoidance
Additional
Features
Abnormal
Operation
GRS1 Magnetic Field Variation Database Update Prompt
Annun/
Alerts
Appendix
Loading the magnetic field variation database update:
1) With ‘OK’ highlighted, as shown in the previous figure, press the ENT Key
on the MFD. A progress monitor is displayed as shown in the following
figure.
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
111
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
2) When the upload is complete, the prompt for the next GRS upload is
displayed, as seen in the following figure.
GRS2 Magnetic Field Variation Database Update Prompt
3) With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor
is displayed as shown in the following figure. When the upload is complete,
the system is ready for use.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Uploading Database to GRS1
Index
Uploading Database to GRS2
112
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Index
Appendix
Index
Index-1
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Abnormal
Operation
Fail-safe operation 65
FD 73
Flight Director 17
Flight path marker 55
Flight plan import/export messages 97,
98
FliteCharts® 56, 57
Frequency Transfer 14
Fuel calculations 8
Additional
Features
F
Hazard
Avoidance
Edit a flight plan 36
Electronic checklists 63, 64
Emergency checklist 64
Enable Terrain 51
Endurance, calculated (ENDUR) 8
Engine leaning assist 10–12
Engine Manifold Pressure (MAN IN HG)
5, 6
Exhaust Gas Temperature (EGT °F) 5, 9,
10–11
Procedures
190-00567-05 Rev. A
E
Flight
Planning
Carbon monoxide detection 7
CDI 2, 14, 94
Cell 43, 44
Cell mode 44
Channel Presets 60
ChartView 56, 57
Checklists 63–64
Clearance player 15
Clearance Recorder 15
GPS Nav
C
DB Mismatch 107, 110
DCLTR Softkey 56
Dead Reckoning 66
Declutter 66, 99, 106
Declutter EIS 9
Direct-to 21
DME 13, 14
DR mode 66, 67, 68
AFCS
Barometric Altitude Minimums 3
Barometric pressure 103
D
Nav/Com/
XPDR/Audio
B
EIS
Activate a flight plan 22
Active Channel 59
Active database 109
Active Navigation Database 109
AC-U-KWIK 58
ADF 13, 14, 66, 102
Advisory alerts 72
AHRS 69, 91, 92
Airport Directory 58
Airport Signs 55, 56
Airways 106
AOPA 58
AOPA’s Airport Directory 58
AP 73
Assist, engine leaning 10–12
Audio panel controls
NAV1, NAV2 14
Audio panel fail-safe operation 65
Autopilot 73
Auxiliary video 61
Code selection softkeys 13
COM 14, 15, 65
Cylinder Head Temperature (CHT °F) 5,
9
Flight
Instruments
A
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Index
Fuel Flow (FFLOW GPH) 5, 6, 10
Fuel flow totalizer 8
Fuel quantity (FUEL QTY GAL) 5, 6
Fuel remaining 105
Fuel remaining, calculated (GAL REM) 8
Fuel used, calculated (GAL USED) 8
H
Horizon heading 55
I
Inhibit TAWS 53
Inhibit Terrain 51
Insertion Point Indicator 23, 33, 34, 38
Inset Map 99, 100
IOI 74, 76
J
NAV 14
NAV1 2, 14
NAV2 2, 14
Navigation database 23, 24
NEXRAD 45, 100, 106
O
OBS 2
Obstacles 82, 87
Oil Pressure (OIL PSI) 5, 6
Oil Temperature (OIL °F) 5, 6
Overspeed Protection 18
Oxygen Outlet Pressure (OXY OUTLET
PSI) 6
Oxygen Quantity (OXY QTY PSI) 6
P
Jeppesen 57
L
Lightning 43, 44, 106
M
Magnetic Field Variation Database 111
Map panning 45
Message advisories 78–96
MET 73
METAR 45
Minimums 78
Mistrim 73
MKR/MUTE 15
Mode S 104
Mode selection softkeys 13
Multi Function Display (MFD)
Softkeys 105
Index-2
N
Pathways 55, 56
Power-up page 63
Profile View 106
R
Reversionary mode 65
ROC 74, 76
S
SafeTaxi® 56
Secure Digital (SD) card 63
Split COM operation 14
Standby Navigation Database 110
Store Flight Plan 35
Stormscope lightning data 43, 44, 106
Strike 43
Strike mode 44
SVS 55, 96
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Index
X
Nav/Com/
XPDR/Audio
XM lightning 100, 106
XM Radio 59
XM weather 45
AFCS
Z
Zoom Window 62
GPS Nav
Flight
Planning
Procedures
TA 78
Tachometer (RPM) 5, 6
TAF 45
TAS 48, 78, 91
TAWS 52, 53, 75
Terrain 49, 50, 52, 82, 100, 106
Terrain-SVS 50, 51
Timer 93
Topographical data 100, 106
Traffic 43, 48, 105
Traffic advisory 48, 78
Traffic map page 48, 49, 50
Transponder 13, 104
Trim 5, 6
Turbine Inlet Temperature (TIT °F) 5, 12
Waypoint Selection Submenu 32
Weather data link page 45
Wind data 102
EIS
T
W
Flight
Instruments
SVS Terrain 55
Synchronization 108
SYNC Status 110
Synthetic Vision System 55
Hazard
Avoidance
V
Additional
Features
Vertical speed guidance 24
Vertical track 78
Video 61
VNV 21, 66, 95
Vspeed 2
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00567-05 Rev. A
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
Index-3
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Index
Blank Page
Index-4
Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis/Corvalis TT
190-00567-05 Rev. A
Garmin International, Inc.
1200 East 151st Street
Olathe, KS 66062, U.S.A.
p: 913.397.8200 f: 913.397.8282
Garmin AT, Inc.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p: 503.391.3411 f: 503.364.2138
Garmin (Europe) Ltd
Liberty House, Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB, U.K.
p: 44/0870.8501241 f: 44/0870.8501251
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com
© 2006-2010, 2012 Garmin Ltd. or its subsidiaries
190-00567-05 Rev. A