Garmin | G1000: Beechcraft Baron G58 | Garmin G1000: Beechcraft Baron G58 G1000 Cockpit Reference Guide Beechcraft G58 - SSV 0857.08

Garmin G1000: Beechcraft Baron G58 G1000 Cockpit Reference Guide Beechcraft G58 - SSV 0857.08
G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Beechcraft 58/G58
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 © 2005, 2007-2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software 0857.08 or later for the Beechcraft 58/
G58. 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: 913/397.8200
Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411
Fax 503/364.2138
Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,
Southampton, SO40 9RB, U.K.
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,
transmitted, disseminated, downloaded or stored in any storage medium, for any purpose
without the express written permission of Garmin. Garmin hereby grants permission to
download a single copy of this manual and of any revision to this manual onto a hard drive or
other electronic storage medium to be viewed for personal use, provided that such electronic
or printed copy of this manual or revision must contain the complete text of this copyright
notice and provided further that any unauthorized commercial distribution of this manual or any
revision hereto is strictly prohibited.
Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH®,
FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks
may not be used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® and SkyWatch® are
registered trademarks of L-3 Communications; and XM® is a registered trademark of XM
Satellite Radio, Inc.;
April, 2010
190-00526-02 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 function. The G1000 Terrain Proximity 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 Proximity feature is only to be used as an aid for terrain
avoidance and is not certified for use in applications requiring a certified
terrain awareness system. 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: The altitude calculated by G1000 GPS receivers is geometric
height above Mean Sea Level and could vary significantly from the altitude
displayed by pressure altimeters, such as the GDC 74A Air Data Computer,
or other altimeters in the aircraft. GPS altitude should never be used for
vertical navigation. Always use pressure altitude displayed by the G1000
PFD or other pressure altimeters in aircraft.
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 the G1000 Multi Function Display
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: XM Weather should not be used for hazardous weather
penetration. Weather information provided by the GDL 69A is approved only
for weather avoidance, not penetration.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Warnings, Cautions & Notes
Warning: NEXRAD weather data is to be used for long-range planning
purposes only. Due to inherent delays in data transmission and the relative
age of the data, NEXRAD weather data should not be used for short-range
weather avoidance.
WARNING: Use of the Stormscope is not intended for hazardous weather
penetration (thunderstorm penetration). Stormscope information, as
displayed on the G1000 MFD, is to be used only for weather avoidance, not
penetration.
WARNING: The Garmin G1000, as installed in the Beechcraft 58/G58
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
Beechcraft 58/G58 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.
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
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: 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 the 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.
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Record of Revisions
Part Number
190-00526-00
190-00526-01
Rev A
Rev B
190-00526-02
Change Summary
Initial release.
Changed to smaller format
Added Airways, WAAS, VNAV, and Charts
Updated G1000 System Messages
Added other GDU 8.10 parameters
Removed FD Formatting feature
Added GDU 11.01 parameters
Added Synthetic Vision System
Added flight plan import/export
Updated procedure for entering User Waypoints
Updated XM weather products
Updated TAWS annunciations
Added CDI operation in Dead Reckoning mode
Added AOPA Airport Directory
Added temporary user waypoints
Added database synchronization
Added GTS 820 TAS
Removed support for non-WAAS systems
Various clerical corrections
Revision Date of Revision Affected Pages
A
April, 2010
All
190-00526-02 Rev. A
Description
Production release.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 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 Navigation Sources.................................................................................................... 1
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs Individually...................................................................................... 2
Set Barometric Minimum Descent Altitude......................................................................... 3
Displaying Wind Data............................................................................................................... 3
Changing HSI Format................................................................................................................ 3
Engine Indication System. ................................................................................................ 5
Engine Display............................................................................................................................ 5
Lean Engine Display.................................................................................................................. 6
Engine System Display............................................................................................................. 8
Nav/Com/Transponder/Audio Panel......................................................................... 9
ADF Tuning (Optional)............................................................................................................... 9
DME Tuning (Optional).............................................................................................................. 9
Enter a Transponder Code....................................................................................................... 9
Activate ADS-B Transmit.......................................................................................................... 9
Selecting a COM Radio........................................................................................................... 10
Selecting a NAV Radio............................................................................................................ 10
NAV/COM Tuning...................................................................................................................... 10
Digital Clearance Recorder and Player............................................................................... 11
Intercom System (ICS) Isolation........................................................................................... 11
Automatic Flight Control System........................................................................... 13
Flight Director Activation...................................................................................................... 13
Vertical Modes.......................................................................................................................... 14
Lateral Modes........................................................................................................................... 15
GPS Navigation......................................................................................................................... 17
Direct-to Navigation............................................................................................................... 17
Activate a Stored Flight Plan................................................................................................ 18
Activate a Flight Plan Leg...................................................................................................... 18
Stop Navigating a Flight Plan............................................................................................... 19
Vertical Navigation (VNAV)................................................................................................... 19
Flight Planning....................................................................................................................... 21
Trip Planning............................................................................................................................. 21
Create a New User Waypoint Defined by Latitude & Longitude.................................. 23
Create a New User Waypoint Defined by Radials from Other Waypoints.................. 23
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
i
Table of Contents
Create a New User Waypoint Defined by a Radial & Distance from Another
Waypoint.............................................................................................................................. 25
Delete a User Waypoint.......................................................................................................... 26
Create a New Flight Plan....................................................................................................... 27
Import a Flight Plan from an SD Card................................................................................. 28
Insert a Waypoint in the Active Flight Plan....................................................................... 29
Enter an Airway in a Flight Plan........................................................................................... 29
Invert An Active Flight Plan................................................................................................... 30
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 30
Store a Flight Plan................................................................................................................... 31
Edit a Stored Flight Plan........................................................................................................ 31
Delete a Waypoint from the Flight Plan............................................................................. 31
Invert and Activate a Stored Flight Plan............................................................................ 32
Copy a Flight Plan.................................................................................................................... 32
Delete a Flight Plan................................................................................................................. 32
Graphical Flight Plan Creation.............................................................................................. 33
Export a Flight Plan to an SD Card...................................................................................... 33
Procedures................................................................................................................................. 35
Load and Activate a Departure Procedure........................................................................ 35
Activate A Departure Leg...................................................................................................... 35
Load An Arrival Procedure..................................................................................................... 35
Activate An Arrival Leg.......................................................................................................... 36
Load and/or Activate an Approach Procedure.................................................................. 36
Activate An Approach in the Active Flight Plan................................................................ 37
Activate a Vector to Final Approach Fix............................................................................. 38
Activate A Missed Approach in the Active Flight Plan.................................................... 38
Hazard Avoidance................................................................................................................. 39
Customizing the Hazard Displays on the Navigation Map............................................. 39
STORMSCOPE® (Optional)..................................................................................................... 39
XM Weather (Optional)........................................................................................................... 41
Traffic Systems......................................................................................................................... 42
Terrain Awareness & Warning System (TAWS-B) Display................................................ 44
Airborne Color Weather Radar............................................................................................. 46
Additional Features............................................................................................................ 51
Synthetic Vision........................................................................................................................ 51
Terminal Procedure Charts.................................................................................................... 52
AOPA Airport Directory.......................................................................................................... 54
XM® Radio Entertainment..................................................................................................... 55
ii
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Table of Contents
Abnormal Operation.......................................................................................................... 57
Reversionary Mode................................................................................................................. 57
Abnormal COM Operation..................................................................................................... 57
Hazard Displays with Loss of GPS Position........................................................................ 57
Unusual Attitudes.................................................................................................................... 58
Dead Reckoning....................................................................................................................... 59
Annunciations & Alerts................................................................................................... 61
WARNING Annunciation......................................................................................................... 61
CAUTION Annunciation........................................................................................................... 61
ADVISORY Annunciation........................................................................................................ 62
Alert Message........................................................................................................................... 62
AFCS ALERTS............................................................................................................................. 62
TAWS-B Alerts........................................................................................................................... 63
TAWS-B System Status Annunciations................................................................................ 65
Voice Alerts............................................................................................................................... 66
MFD & PFD Message Advisories........................................................................................... 67
Database Message Advisories.............................................................................................. 68
GMA 1347 Message Advisories............................................................................................. 70
GIA 63W Message Advisories................................................................................................ 71
GEA 71 Message Advisories................................................................................................... 73
GTX 33 Message Advisories................................................................................................... 74
GRS 77 Message Advisories................................................................................................... 74
GMU 44 Message Advisories................................................................................................. 75
GDL 69/69A Message Advisories.......................................................................................... 75
GDC 74A Message Advisories................................................................................................ 75
GWX 68 Message Advisories................................................................................................. 76
GTS 820 Message Advisories................................................................................................. 76
Miscellaneous Message Advisories...................................................................................... 77
Flight Plan Import/Export Messages................................................................................... 80
Appendix........................................................................................................................................ 83
PFD Softkey Map..................................................................................................................... 83
MFD Softkey Map.................................................................................................................... 88
Database Updates................................................................................................................... 90
Index..........................................................................................................................................Index-1
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
iii
Table of Contents
Blank Page
iv
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Flight Instruments
Flight
Instruments
Flight Instruments
Selecting the Altimeter Barometric Pressure Setting
Turn the BARO Knob to select the desired setting.
EIS
Press the PFD Softkey.
2)
Press the STD BARO Softkey to set standard barometric pressure.
AFCS
1)
Nav/Com/
XPDR/Audio
Selecting Standard Barometric Pressure (29.92 in Hg)
Change Altimeter Barometric Pressure Setting Units
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Flight
Planning
Press the PFD Softkey to display the second-level softkeys.
GPS Nav
1)
Procedures
Or:
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Press the BACK Softkey to return to the top-level softkeys.
Hazard
Avoidance
4)
Change Navigation Sources
Press 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)
Press the CDI Softkey a third time to return to GPS.
Annun/
Alerts
2)
Abnormal
Operation
Press 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.
Additional
Features
1)
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
1
Enable/Disable OBS Mode While Navigating with GPS
1)
Press the OBS Softkey to select OBS Mode.
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.
3)
Press the OBS Softkey again to disable OBS Mode.
1)
Press 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.
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.
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.
Additional
Features
Configure Vspeed Bugs Individually
1) Press 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
Abnormal
Operation
Hazard
Avoidance
Procedures
Flight
Planning
AFCS
Generic Timer
GPS Nav
Nav/Com/
XPDR/Audio
EIS
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.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Index
Appendix
Annun/
Alerts
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Flight Instruments
Flight
Instruments
Set Barometric Minimum Descent Altitude
1) Press the TMR/REF Softkey.
Turn the small FMS Knob clockwise to BARO.
4)
Press the ENT Key.
5)
Use the small FMS Knob to enter the desired altitude.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
AFCS
3)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘Minimums’.
EIS
2)
2)
Press the WIND Softkey to display wind data to the left of the HSI.
3)
Press one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, press the OFF Softkey.
Procedures
Press the PFD Softkey.
Flight
Planning
1)
GPS Nav
Displaying Wind Data
Changing HSI Format
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI Softkey to display the full size HSI.
Additional
Features
Press the PFD Softkey.
Hazard
Avoidance
1)
Or:
Abnormal
Operation
Press the ARC HSI Softkey to display the arc style HSI.
Annun/
Alerts
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
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 Beechcraft 58/G58
190-00526-02 Rev. A
Engine Indication System
Flight
Instruments
Engine Indication System
Engine Display
EIS
Nav/Com/
XPDR/Audio
In all cases green indicates normal operation, yellow indicates caution, and red
indicates warning.
Pressing the ENGINE Softkey makes available the LEAN and SYSTEM softkeys
which in turn provide access to the Lean Page and the System Page, respectively.
AFCS
GPS Nav
Manifold
Pressure
Gauge
(Left Engine)
Flight
Planning
RPM Gauge
(Left Engine)
Propeller Sync
Indicator
Fuel Flow
Indicator
Procedures
Fuel Flow
Numeric
Readout
Hazard
Avoidance
Cylinder Head
Temperature
Indicator
Additional
Features
Oil Temperature
Indicator
Oil Pressure
Indicator
Abnormal
Operation
Ammeter
Fuel Quantity
Indicator
Annun/
Alerts
Default Engine Page
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
5
Lean Engine Display
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
AFCS
Fuel Flow Leaning
Marker
Difference between peak
and current temperature
of selected cylinder
(Right Engine)
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
EGT peak
temperature
(Left Engine)
Exhaust Gas
Temperature
Bar Graphs
(Left Engine)
Cylinder Head
Temperature
Bar Graphs
(Left Engine)
Additional
Features
Abnormal
Operation
CHT Readout
For Selected
Cylinder
(Right Engine)
LEAN Engine Page
1)
Press the ENGINE Softkey.
2)
Press the LEAN Softkey to display the LEAN Engine Page.
From the Lean Display, the CYL SLCT and ASSIST Softkeys can be utilized to
obtain information about specific cylinders on both the EGT and CHT graphs. Pressing
the CYL SLCT Softkey cycles through the cylinders; the selected cylinder number is
displayed in light blue. The CYL SLCT Softkey is disabled during warning or caution
conditions or when the ASSIST Softkey is pressed.
Monitoring the desired cylinder’s EGT and CHT:
From the Lean Display, press the CYL SLCT Softkey to cycle through each
cylinder and view its EGT and CHT. The selected cylinder is shown in light
blue.
Index
Appendix
Annun/
Alerts
EGT Readout
For Selected
Cylinder
(Right Engine)
6
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Engine Indication System
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
When the ASSIST Softkey is selected, the system initially highlights and selects
the cylinder number with the hottest EGT and displays its temperature below the EGT
bar graph. A readout showing the difference between peak (DPEAK) and the current
temperature for the selected cylinder is displayed above the EGT bar graph.
As the mixture is leaned, a light blue line will appear above each cylinder to indicate
EGT peak.
When the system detects the first cylinder to peak, the cylinder numbers below the
EGT graph disappear, and the letter “R” is annunciated below the first peaked cylinder
to indicate the other cylinders are rich of peak. As the mixture is further leaned, the
letter “L” is annunciated below the last peaked cylinder indicating all cylinders are
lean of peak. Refer to the POH and AFM for the recommended mixture adjustment
procedures.
Monitoring of the cylinder continues until the ASSIST Softkey is pressed again
which disables lean assist and removes the peak lines from the bar graph and the
temperature deviation from peak (DPEAK). The system then returns to seeking the
hottest cylinder.
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
7
Engine System Display
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
1)
Press the ENGINE Softkey, then the SYSTEM Softkey to display the
SYSTEM Engine Page.
2)
If desired, use the DEC FUEL, INC FUEL, 166 GAL, and 194 GAL
softkeys to adjust the amount of fuel remaining for totalizer calculations.
Procedures
Flight
Planning
GPS Nav
AFCS
NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and
are calculated from the last time the fuel was reset.
Hazard
Avoidance
System
Information
Additional
Features
Fuel Calculation
Information
Annun/
Alerts
Abnormal
Operation
Electrical
Information
Index
Appendix
SYSTEM Engine Page
8
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
Nav/Com/Transponder/Audio Panel
ADF Tuning (Optional)
EIS
Tune the ADF using the remote ADF control head.
Nav/Com/
XPDR/Audio
DME Tuning (Optional)
2)
Turn the large FMS to select the DME source field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
GPS Nav
Press the DME Softkey.
AFCS
1)
Enter a Transponder Code
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
Press 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.
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the ADS-B TX Softkey to enable transmission of three-dimensional
aircraft position and aircraft heading.
3)
Press the ADS-B TX Softkey again to disable transmission.
Abnormal
Operation
1)
Additional
Features
Activate ADS-B Transmit
Hazard
Avoidance
2)
Procedures
Press the XPDR Softkey to display the transponder mode selection softkeys.
Flight
Planning
1)
Annun/
Alerts
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
9
Selecting a COM Radio
Transmit/Receive
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
Selecting a NAV Radio
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
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.
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.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Receive Only
10
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Nav/Com/XPDR/Audio Panel
GPS Nav
Selected
radios; pilot;
copilot;
passengers;
music
Copilot;
passengers;
music
Copilot;
passengers;
music
OFF
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
Appendix
OFF
Annun/
Alerts
ALL
Abnormal
Operation
Selected
radios; pilot;
copilot;
passengers;
music
Selected
radios; pilot;
copilot;
passengers;
music
Additional
Features
Passenger
Hears
Hazard
Avoidance
Copilot
Hears
Procedures
Pilot Hears
Flight
Planning
Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/
Com radios and music.
PILOT KEY
COPLT KEY
ANNUNCIATOR ANNUNCIATOR
AFCS
Intercom System (ICS) Isolation
Mode
Nav/Com/
XPDR/Audio
• Pressing PLAY once plays the latest recorded memory block, then returns to
normal operation.
• Pressing MKR/MUTE 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.
EIS
NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is
not recorded for COM3 MIC.
Flight
Instruments
Digital Clearance Recorder and Player
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
11
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
12
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
AFCS
AFCS
Flight Director Activation
Modes Selected
Heading Select
HDG
PIT
GP
GS
PIT
Annun/
Alerts
HDG Key
Pitch Hold (default)
Glidepath
Glideslope
Pitch Hold (default)
Abnormal
Operation
Approach**
PIT
Additional
Features
APR Key
GPS
VAPP
LOC
Pitch Hold (default)
Hazard
Avoidance
Navigation**
Procedures
NAV Key
ROL
ROL
ROL
GA
ROL
ROL
ROL
GPS
VOR
LOC
Vertical
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Pitch Hold (default)
PIT
Go Around (in air)
GA
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Flight
Planning
FD Key
AP Key
CWS Switch
GA Switch
ALT Key
VS Key
VNV Key
Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Go Around (in air)
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
GPS Nav
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.
Control Pressed
Nav/Com/
XPDR/Audio
Note: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
EIS
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.
Flight
Instruments
Automatic Flight Control System
**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.
Appendix
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
13
Vertical Modes
Vertical Mode
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
AFCS
Pitch Hold
Selected Altitude
Armed
Vertical Speed
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Altitude Hold
Flight Level Change
VNAV
VNAV Target Altitude
Armed (GDU 1045
only)
Glidepath
Glideslope
Go Around
Description
Holds the current aircraft pitch
attitude; may be used to climb/
descend to the Selected Altitude
AFCS armed to capture the altitude
displayed in the Selected Altitude
window
Holds the current Altitude
Reference
Maintains the current aircraft
vertical speed; may be used to climb/
descend to the Selected Altitude
Maintains the current aircraft
airspeed in IAS while the aircraft is
climbing/descending to the Selected
Altitude
Captures and tracks the VNAV flight
path
AFCS armed to capture the altitude
displayed in the VNAV Target
Altitude window
Captures and tracks the WAAS
glidepath on approach
Captures and tracks the ILS
glideslope on approach
Disengages the autopilot and
commands a constant pitch attitude
and wings level
Control
Annunciation
(default)
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
14
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
AFCS
Lateral Mode
Flight
Planning
BC
Procedures
GPS
APR
Key
Hazard
Avoidance
VAPP
LOC
GA
Abnormal
Operation
GA
Switch
Additional
Features
Approach, GPS (Glidepath
mode automatically armed if
vertical guidance is available) Captures and tracks the
selected navigation source
Approach, VOR
(GPS, VOR, LOC)
Approach, LOC (Glideslope
Mode automatically armed)
Disengages the autopilot and
Go Around
commands a constant pitch
angle and wings level
GPS Nav
Navigation, Backcourse
Captures and tracks a
localizer signal for backcourse
approaches
AFCS
Navigation, GPS
Navigation, VOR (Enroute
Mode)
Navigation, LOC (Glideslope
will not arm or capture)
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
Annun/
Alerts
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
15
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
16
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
GPS Navigation
Flight
Instruments
GPS Navigation
Direct-to Navigation
2)
3)
6)
9)
12)
1)
2)
5)
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
17
Index
6)
Appendix
4)
).
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.
Annun/
Alerts
3)
Press the Direct-to Key (
Abnormal
Operation
Direct-to Navigation from the PFD
Additional
Features
11)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
7)
GPS Nav
5)
) 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.
AFCS
4)
Press the Direct-to (
Nav/Com/
XPDR/Audio
1)
EIS
Direct-to Navigation from the MFD
EIS
Flight
Instruments
GPS Navigation
7)
Turn the small FMS Knob to enter the desired altitude.
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 distance 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.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Press the ACTIVE Softkey. The confirmation window is now displayed.
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.
Activate a Flight Plan Leg
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
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.
2)
Press the ACT LEG Softkey on the MFD.
3)
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.
4)
With ‘Activate’ highlighted, press the ENT Key.
Index
Appendix
or
18
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
GPS Navigation
Flight
Instruments
Stop Navigating a Flight Plan
2)
Press the MENU Key to display the Page Menu Window.
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.
Vertical Navigation (VNAV)
AFCS
GPS Nav
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
Press the FPL Key to display the Active Flight Plan Page.
EIS
1)
Flight
Planning
Procedures
Large White
Text
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
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
19
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
20
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Light Blue
Subdued Text
190-00526-02 Rev. A
Flight Planning
Flight
Instruments
Flight Planning
Trip Planning
Turn the large FMS Knob to select the ‘AUX’ page group.
2)
Turn the small FMS Knob to select the first rectangular page icon.
3)
The current ‘page mode’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL
Softkey.
4)
For Direct-to planning:
EIS
1)
AFCS
GPS Nav
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.
Procedures
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
Hazard
Avoidance
For point-to-point planning:
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:
Annun/
Alerts
For flight plan leg planning:
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
21
Index
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.
190-00526-02 Rev. A
Nav/Com/
XPDR/Audio
a) Press the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
Flight
Instruments
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.
EIS
Flight Planning
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
Nav/Com/
XPDR/Audio
5)
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
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.
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.
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
6)
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.
Abnormal
Operation
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
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.
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.
Appendix
Annun/
Alerts
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.
Index
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.
22
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Flight Planning
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.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
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.
AFCS
2)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
EIS
1)
Flight
Instruments
Create a New User Waypoint Defined by Latitude & Longitude
GPS Nav
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
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 LAT/LON (latitude and longitude).
9)
Press the ENT Key.
Hazard
Avoidance
Create a New User Waypoint Defined by Radials from Other
Waypoints
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.
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
Turn the small FMS Knob to select the User WPT Information Page.
Annun/
Alerts
2)
Abnormal
Operation
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
Additional
Features
1)
Index
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
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.
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Procedures
7)
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.
23
EIS
Flight
Instruments
Flight Planning
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).
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.
24
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Flight Planning
13) Repeat step 10 to enter the next waypoint name.
15) Press the ENT Key.
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.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
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.
Procedures
2)
Flight
Planning
Turn the large FMS Knob on the MFD to select the ‘WPT’ page group.
GPS Nav
1)
Hazard
Avoidance
a) Turn the large FMS Knob one click to the left to highlight
‘TEMPORARY’.
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/DIS (radial/distance).
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.
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:
c) Press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Abnormal
Operation
7)
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.
190-00526-02 Rev. A
AFCS
Create a New User Waypoint Defined by a Radial & Distance from
Another Waypoint
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.
25
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.
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.
15) Press the FMS Knob to remove the flashing cursor.
Delete a User Waypoint
Index
Appendix
Annun/
Alerts
14) Press the ENT Key.
26
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.
3)
Press the FMS Knob to activate the cursor.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Flight Planning
Turn the small FMS Knob to highlight the desired waypoint.
6)
Press the DELETE Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
Create a New Flight Plan
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
27
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Procedures
190-00526-02 Rev. A
Flight
Planning
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
GPS Nav
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.
AFCS
NOTE: When creating a new flight plan in the Active Flight Plan Window,
the first leg is activated automatically after it is created.
Nav/Com/
XPDR/Audio
5)
EIS
Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
Flight
Instruments
4)
Flight Planning
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.
Import a Flight Plan from an SD Card
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
NOTE: See the Annunciations & Alerts section for flight plan import message
descriptions.
1)
Insert the SD card containing the flight plan in the top card slot on the
MFD.
2)
Press the FPL Key on the MFD to display the Active Flight Plan Page.
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.
6)
Press the IMPORT Softkey.
Additional
Features
If an empty flight plan is selected, a list of the available flight plans on
the SD card will be displayed.
Or:
7)
Turn the small FMS Knob to highlight the desired flight plan for importing.
8)
Press the ENT Key.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
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.
28
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Flight Planning
1)
Press the FPL Key to display the active flight plan.
2)
If required, press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
EIS
4)
Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
Nav/Com/
XPDR/Audio
Flight
Instruments
Insert a Waypoint in the Active Flight Plan
5)
Enter the new flight plan waypoint by one of the following:
AFCS
a) Enter the user waypoint identifier, facility, or city.
b) Press the ENT Key.
b) Turn the small FMS Knob to the right to display the ‘NRST’ airport
waypoints to the aircraft’s current position.
Flight
Planning
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
GPS Nav
Or:
Procedures
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Hazard
Avoidance
Or:
Additional
Features
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.
e) Press the ENT Key again to accept the waypoint.
Annun/
Alerts
Enter an Airway in a Flight Plan
Press the FPL Key.
2)
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
29
Index
190-00526-02 Rev. A
Appendix
1)
4)
Turn the small FMS Knob one click clockwise and press 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 (the waypoint ahead of the cursor position).
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.
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.
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.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
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.
Remove a Departure, Arrival, Approach, or Airway from a Flight
Plan
1)
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or, for a stored flight plan:
Annun/
Alerts
a) Press the FPL Key on the MFD.
b) Turn the small FMS Knob to select the Flight Plan Catalog Page.
Appendix
c) Press the FMS Knob to activate the cursor.
d) Turn the large FMS Knob to highlight the desired flight plan.
e) Press the EDIT Softkey.
Index
2)
30
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.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Flight Planning
Press the CLR Key to display a confirmation window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
EIS
Store a Flight Plan
Flight
Instruments
3)
2)
Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key.
3)
With ‘OK’ highlighted, press the ENT Key to store the flight plan.
AFCS
After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
Nav/Com/
XPDR/Audio
1)
Edit a Stored Flight Plan
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan.
4)
Press the EDIT Softkey.
5)
Turn the large FMS Knob to place the cursor in the desired location.
6)
Enter the changes, then press the ENT Key.
7)
Press the FMS Knob to return to the Flight Plan Catalog Page.
Flight
Planning
Press the FPL Key on the MFD, then turn the small FMS Knob to display the
Flight Plan Catalog Page.
Procedures
Hazard
Avoidance
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Abnormal
Operation
Or, for a stored flight plan:
a) Press the FPL Key on the MFD.
Annun/
Alerts
b) Turn the small FMS Knob to select the Flight Plan Catalog Page.
c) Press the FMS Knob to activate the cursor.
Appendix
d) Turn the large FMS Knob to highlight the desired flight plan.
e) Press the EDIT Softkey.
Turn the large FMS Knob to highlight the waypoint to be deleted.
3)
Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
31
Index
2)
190-00526-02 Rev. A
Additional
Features
Delete a Waypoint from the Flight Plan
1)
GPS Nav
1)
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.
5)
Once all changes have been made, press the FMS Knob to remove the
cursor.
Invert and Activate a Stored Flight Plan
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.
4)
Turn the large FMS Knob to highlight the desired flight plan.
5)
Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
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.
Additional
Features
Abnormal
Operation
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.
4)
Turn the large FMS Knob to highlight the flight plan to be copied.
5)
Press the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
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.
Delete a Flight Plan
Index
Appendix
Annun/
Alerts
1)
Copy a Flight Plan
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
32
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.
4)
Turn the large FMS Knob to highlight the flight plan to be deleted.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Flight Planning
Press the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
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.
Flight
Instruments
5)
EIS
Graphical Flight Plan Creation
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. Turn the large FMS Knob to select the desired insertion point.
4)
Press 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.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
Hazard
Avoidance
Export a Flight Plan to an SD Card
3)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
4)
Press the FMS Knob to activate the cursor.
5)
Turn the large FMS Knob to highlight the flight plan to be exported.
6)
Press the EXPORT Softkey.
7)
Press the ENT Key to confirm the export.
Appendix
Press the FPL Key to display the Active Flight Plan Page on the MFD.
Annun/
Alerts
2)
Abnormal
Operation
Insert the SD card into the top card slot on the MFD.
Additional
Features
NOTE: See the Annunciations & Alerts section for flight plan export message
descriptions.
1)
Procedures
3)
Flight
Planning
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.
GPS Nav
2)
AFCS
Press the FPL Key on the MFD to display the Active Flight Plan Page.
Nav/Com/
XPDR/Audio
1)
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
33
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
Blank Page
34
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Procedures
Flight
Instruments
Procedures
Load and Activate a Departure Procedure
EIS
3)
Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
4)
Turn the large FMS Knob to highlight the desired departure.
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.
6)
Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
7)
Turn the large FMS Knob to highlight the desired transition.
8)
Press the ENT Key.
9)
With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
Hazard
Avoidance
Press the FPL Key on the MFD to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
departure.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Additional
Features
1)
Abnormal
Operation
Annun/
Alerts
Load An Arrival Procedure
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
3)
Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
Appendix
1)
35
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Procedures
Activate A Departure Leg
190-00526-02 Rev. A
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
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.
6)
Turn either FMS Knob to select the desired transition.
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.
10) With ‘LOAD?’ highlighted, press the ENT Key.
AFCS
11) The arrival becomes part of the active flight plan.
GPS Nav
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.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
arrival.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Load and/or Activate an Approach Procedure
NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
b) Turn the large FMS Knob to highlight the desired waypoint altitude.
36
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Procedures
Press the ENT Key. A list of available approaches for the destination airport
is displayed.
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
EIS
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.
Nav/Com/
XPDR/Audio
7)
Press the ENT Key. The cursor moves to the MINIMUMS field.
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.
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.
AFCS
GPS Nav
Flight
Planning
Procedures
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?’.
Hazard
Avoidance
Additional
Features
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.
12) Press the ENT Key.
Abnormal
Operation
Activate An Approach in the Active Flight Plan
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
Annun/
Alerts
1)
Flight
Instruments
3)
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
37
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
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Flight
Planning
Or:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Press the Go-around Button.
38
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Hazard Avoidance
Flight
Instruments
Hazard Avoidance
Customizing the Hazard Displays on the Navigation Map
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.
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.
3)
Press the small FMS Knob to return to the Navigation Map Page.
EIS
1)
AFCS
Procedures
Press the MAP Softkey.
2)
Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove
Stormscope Lightning Data from the Navigation Map Page.
Additional
Features
Symbol
Abnormal
Operation
Strike is between 6 and 60 seconds old
Strike is between 1 and 2 minutes old
Annun/
Alerts
Strike is between 2 and 3 minutes old
3)
Press the ENT Key.
4)
Turn the small FMS Knob to highlight ‘Weather’.
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
Turn either FMS Knob to highlight ‘Map Setup’.
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
2)
Hazard
Avoidance
1)
Press the MENU Key (with the Navigation Map Page displayed).
Flight
Planning
Displaying Stormscope Lightning Data on the Navigation Map Page
1)
GPS Nav
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.
Lightning Age
Strike is less than 6 seconds old
Nav/Com/
XPDR/Audio
STORMSCOPE® (Optional)
39
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
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.
8)
Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
9)
Push the FMS Knob to return to the Navigation Map Page.
AFCS
Clear Stormscope Lightning Data from the Navigation Map Page
1)
Press the MENU Key (with the Navigation Map Page displayed).
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
Flight
Planning
after the execution of each turn. This is to ensure that the strike and/or cell
positions are depicted accurately in relation to the nose of the aircraft.
Procedures
Stormscope Page
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.
1)
Select the Stormscope Page.
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.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
Annun/
Alerts
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Appendix
Change the Viewing Mode Between 360˚ and 120˚
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
Press the CLEAR Softkey to remove all Stormscope lightning data from the
display.
40
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Hazard Avoidance
Press the MAP Softkey.
2)
Press the NEXRAD or XM LTNG Softkey to display the desired weather.
Press the applicable softkey again to remove weather data from the
Navigation Map Page.
AFCS
1)
Nav/Com/
XPDR/Audio
Displaying XM Weather on the Navigation Map Page
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Press the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
Flight
Planning
Turn the large FMS Knob to select the WPT Page Group.
GPS Nav
Display METAR and TAF information on the Airport Information Page
1)
Procedures
Displaying Weather on the Weather Data Link Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link Page.
3)
Press the available softkeys to select the desired XM weather product.
4)
Press 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
1)
Abnormal
Operation
Push in the Joystick to display the panning arrow.
2)
Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
or SIGMETs.
3)
Press the ENT Key to display pertinent information for the selected product.
Annun/
Alerts
1)
Appendix
Index
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 Beechcraft 58/G58
Additional
Features
Map Panning Information – Weather Data Link Page
190-00526-02 Rev. A
EIS
WARNING: Use of XM weather for hazardous weather penetration is not
recommended. Weather information provided by XM Radio Service is
approved only for weather avoidance, not penetration.
Flight
Instruments
XM Weather (Optional)
41
Hazard Avoidance
Flight
Instruments
Weather Products and Symbols
Turbulence
NEXRAD XM Lightning
METARs Surface Analysis
SIGMETs/AIRMETs
County Warnings
Winds Aloft
Traffic Systems
• 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.
Traffic Symbol
Procedures
Flight
Planning
PIREPs
Cloud Top
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Echo Top (Cloud Top and Echo Top Mutually Exclusive)
Cyclone Warnings
City Forecast
AIREPs
Cell Movement
Icing Potential
Freezing Levels
Description
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Hazard
Avoidance
Proximity Advisory (PA) (Not available with TIS system)
(intruder is within 5 nm and less than 1200’ vertical separation)
Additional
Features
Traffic Advisory (TA)
(closing rate, distance, and vertical separation meet TA criteria)
Abnormal
Operation
Traffic Advisory Off Scale
Traffic Symbol Description
Annun/
Alerts
Traffic Information Service (TIS)
Appendix
NOTE: If the G1000 is configured to use a Traffic Advisory System (TAS), TIS
is not available for use.
Index
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
42
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Hazard Avoidance
3)
Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
6)
Press the TNA MUTE Softkey to mute the “Traffic Not Available” aural
alert.
GPS Nav
Turn the small FMS Knob to select the Traffic Map Page.
AFCS
2)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob to select the Map Page Group.
EIS
1)
Flight
Instruments
Displaying Traffic on the Traffic Map Page
Displaying Traffic on the Navigation Map
Ensure TIS is operating. With the Navigation Map displayed, press the
MAP Softkey.
2)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
Flight
Planning
1)
Procedures
Traffic Advisory System (TAS)(If Installed)
Select the OPERATE or NORMAL Softkey to begin displaying traffic.
‘OPERATING’ is displayed in the Traffic Mode field.
4)
Select the ALT MODE Softkey to change the altitude volume. Select the
desired altitude volume by pressing the BELOW, NORMAL, ABOVE, or
UNREST (unrestricted) Softkey. The selection is displayed in the Altitude
Mode field.
5)
Select the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
6)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
7)
Select the FLT ID Softkey to enable or disable Flight ID displayed with the
intruder information (GTS 820 only).
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
3)
Appendix
Turn the small FMS Knob to select the Traffic Map Page.
Annun/
Alerts
2)
Abnormal
Operation
Turn the large FMS Knob to select the Map Page Group.
Additional
Features
1)
Hazard
Avoidance
Displaying Traffic on the Traffic Map Page
43
Hazard Avoidance
1)
With the Traffic Map Page displayed, set the range to 2/6 nm.
2)
Select the STANDBY Softkey.
3)
Select the TEST Softkey.
4)
Self test takes approximately eight seconds to complete. When completed
successfully, traffic symbols are displayed and a voice alert is heard (see
Alerts and Annunciations section). If the self test fails, the system reverts to
Standby Mode and a voice alert is heard.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
System Self Test
1)
Ensure TAS is operating.
2)
With the Navigation Map displayed, select the MAP Softkey.
3)
Select the TRAFFIC Softkey. Traffic is now displayed on the map.
Terrain Awareness & Warning System (TAWS-B) Display
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Procedures
Flight
Planning
GPS Nav
AFCS
Displaying Traffic on the Navigation Map
1)
While the TAWS-B Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select ‘Test TAWS’.
3)
Press the ENT Key. During the test ‘TAWS TEST’ is displayed in the center
of the TAWS-B Page.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Manual System Test
When all is in working order, “TAWS System Test, OK” is heard.
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Appendix
Turn the small FMS Knob to select the TAWS-B Page.
3)
If desired, press the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Press the 360 Softkey to return to the 360° default display.
Index
Annun/
Alerts
Display Terrain on the TAWS-B Page
4)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
44
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Hazard Avoidance
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.
Nav/Com/
XPDR/Audio
Red
EIS
Terrain/Obstacle Location
Flight
Instruments
Color
Enable/Disable Aviation Data
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
GPS Nav
While the TAWS-B Page is displayed, press the MENU Key.
AFCS
1)
TAWS Inhibit
Flight
Planning
Procedures
Inhibit TAWS
While the TAWS-B Page is displayed, press the INHIBIT Softkey.
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit TAWS’.
3) Press the ENT Key.
Hazard
Avoidance
Additional
Features
Enable TAWS
While the TAWS-B Page is displayed, press 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.
Abnormal
Operation
Annun/
Alerts
Appendix
NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active
waypoint in a GPS WAAS 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.
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
45
Airborne Color Weather Radar
WARNING: Begin transmitting only when it is safe to do so. If it is desired to
transmit while the aircraft is on the ground, no personnel or objects should
be within 11 feet of the antenna.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
AFCS
CAUTION: In Standby Mode, the antenna is parked at the center line. It
is always a good idea to put the radar in Standby Mode before taxiing the
aircraft to prevent the antenna from bouncing on the bottom stop and possibly
causing damage to the radar assembly.
1)
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Radar Page.
3)
Press the MODE Softkey.
4)
If the aircraft is on the ground, press the STANDBY Softkey to initiate the
one minute warm-up period. After the warm-up is complete, the radar
enters Standby Mode. After the aircraft is airborne, press the WEATHER
Softkey.
Procedures
Flight
Planning
GPS Nav
Displaying Weather on the Weather Radar Page
Hazard
Avoidance
Or:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
If the aircraft is already airborne, press the WEATHER or GROUND Softkey.
The one-minute warm-up period is initiated, after which the radar begins
transmitting. The horizontal scan is initially displayed.
5)
Turn the Joystick to select the desired range.
6)
If desired, press the VERTICAL Softkey for vertical scanning.
Adjusting Antenna Tilt
Move the Joystick up or down to adjust the tilt of the antenna up or down. Monitor the displayed tilt value in the TILT field.
When scanning vertically, a Tilt Line may be displayed to aid in positioning the tilt
of the antenna. If the Tilt Line is not displayed, perform the following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Tilt Line’.
3) Press the ENT Key.
46
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Hazard Avoidance
EIS
Nav/Com/
XPDR/Audio
AFCS
Move the Joystick right or left to adjust the azimuth position of the antenna right
or left. Monitor the displayed bearing value in the BEARING field.
When scanning horizontally, a Bearing Line may be displayed to aid in positioning
the antenna for the vertical scan. If the Bearing Line is not displayed, perform the
following steps:
1) Press the MENU Key
2) Turn the large FMS Knob to select ‘Show Bearing Line’.
3) Press the ENT Key.
Flight
Instruments
Adjusting Antenna Bearing
Vertically Scan a Storm Cell
Move the Joystick right or left to move the scanned “slice” a few degrees
right or left.
4)
Turn the Joystick to adjust the range.
5)
To select a new area to be vertically scanned, press the HORIZON Softkey
to return to the Horizontal Scan view and repeat the previous steps.
Adjusting Gain
3)
Press the FMS Knob to remove the cursor.
4)
Press the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ is
displayed in the ‘GAIN’ field.
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
Turn the small FMS Knob to adjust the gain for the desirable level. The
gain setting is visible in the gain field as a movable horizontal bar in
a flashing box. The line pointer is a reference depicting the calibrated
position.
Appendix
2)
Annun/
Alerts
Press the GAIN Softkey to activate the cursor in the ‘GAIN’ field.
Abnormal
Operation
1)
Additional
Features
WARNING: Changing the gain in Weather Mode causes precipitation intensity
to be displayed as a color not representative of the true intensity. Remember
to return the gain setting to ‘Calibrated’ for viewing the actual intensity of
precipitation.
Hazard
Avoidance
3)
Procedures
Press the VERTICAL Softkey. A vertical ‘slice’ of the selected area is now
displayed.
Flight
Planning
2)
GPS Nav
1) While in the Horizontal Scan view, move the Joystick to place the Bearing
Line on the desired storm cell, or other area, to be vertically scanned.
47
Hazard Avoidance
Press the MODE Softkey.
2)
Press the GROUND Softkey to place the radar in Ground Map Mode.
3)
Press the BACK Softkey.
4)
Press the FMS Knob to activate the cursor.
Nav/Com/
XPDR/Audio
5)
Turn the large FMS Knob to place the cursor in the ‘TILT’ field.
6)
Adjust the antenna tilt angle by turning the small FMS Knob to position the
ground returns as desired.
7)
Press the FMS Knob to remove the cursor.
EIS
1)
AFCS
Flight
Instruments
Ground Mapping
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Sector Scan
2)
Press the FMS Knob to display the cursor.
3)
Turn the large FMS Knob to place the cursor in the SECTOR SCAN field.
4)
Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan.
5)
If desired, readjust the Bearing Line with the Joystick to change the center
of the Sector Scan.
6)
Press the FMS Knob to remove the cursor.
Additional
Features
Antenna Stabilization
Abnormal
Operation
Annun/
Alerts
While in the Horizontal Scan Mode, move the Joystick right or left to place
the Bearing Line in the desired position. The location of the Bearing Line
becomes the center point of the Sector Scan.
1)
To activate or deactivate the antenna stabilization, press the MODE
Softkey.
2)
Press the STAB ON Softkey to activate antenna stabilization or press the
STAB OFF Softkey to deactivate. The current stabilization condition is
shown in the upper right of the weather radar display.
Weather Attenuated Color Highlight (WATCH®)
To activate or deactivate the Watch® feature, press the WATCH Softkey. This
feature is only available in the Horizontal Scan Mode.
Index
Appendix
1)
48
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Hazard Avoidance
EIS
Nav/Com/
XPDR/Audio
Automatic Standby
When the weather radar system is in the Weather or Ground Map Mode, upon
landing the system automatically switches to Standby Mode.
Flight
Instruments
Weather Alert
To activate or deactivate Weather Alert, press the WX ALRT Softkey. Activating and
deactivating also enables or inhibits the alert on the PFD.
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
49
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
50
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Additional Features
Flight
Instruments
Additional Features
Synthetic Vision
EIS
Nav/Com/
XPDR/Audio
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 the accuracy and/or fidelity upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or
traffic.
AFCS
Abnormal
Operation
Annun/
Alerts
Press the SYN VIS Softkey.
3)
Press the SYN TERR Softkey.
4)
Press the BACK Softkey to return to the previous page.
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
2)
Appendix
Press the PFD Softkey.
Additional
Features
Displaying SVS Terrain
1)
Hazard
Avoidance
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
Procedures
•
•
•
•
•
•
•
Flight
Planning
Synthetic Vision System (SVS) functionality is offered as an optional enhancement
to the G1000 Integrated Flight Deck 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).
SVS offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
In addition to SVS enhancement to the PFD, the following feature enhancements
have been added to the PFD:
GPS Nav
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.
51
Additional Features
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Displaying Pathways
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the PATHWAY Softkey.
5)
Press the BACK Softkey to return to the previous page.
AFCS
GPS Nav
Flight
Planning
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the HRZN HDG Softkey.
5)
Press the BACK Softkey to return to the previous page.
Procedures
Displaying Airport Signs
Hazard
Avoidance
Additional
Features
Press the PFD Softkey.
Displaying Heading on the Horizon
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the APTSIGNS Softkey.
5)
Press the BACK Softkey to return to the previous page.
Terminal Procedure Charts
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts® in
electronic form, it is still advisable to carry another source of charts on-board
the aircraft.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
1)
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.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
52
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Additional Features
AFCS
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
View Charts from the Navigation Map Page
Press the SHW CHRT Softkey when displayed.
Press 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.
3)
Press the GO BACK Softkey to return to the previous page.
53
Index
2)
Appendix
Move the map pointer to point to a desired point on the map and press the
SHW CHRT Softkey.
Annun/
Alerts
Or:
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
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®
190-00526-02 Rev. A
Nav/Com/
XPDR/Audio
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)
EIS
ChartView (Optional)
Flight
Instruments
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. Pressing 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.
Additional Features
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
View Charts from the Active Flight Plan Page
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.
2)
Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
3)
Press the SHW CHRT Softkey. The appropriate chart is displayed, if
available for the item selected.
4)
Press the GO BACK Softkey to return to the previous page.
Change Day/Night View
1)
While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
2)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
3)
Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR
SCHEME’ Options.
4)
Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.
5)
Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
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.
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.
AOPA Airport Directory
AOPA Airport Directory adds enhanced airport information when viewing airports
on the WPT-Airport Information Page.
This database is updated four times per year. Check fly.garmin.com for the current
database.
View Airport Directory Information
While viewing the WPT-Airport Information Page, if necessary, press the
INFO-1 Softkey to change the softkey label to display INFO-2. AOPA
airport information is displayed on the right half of the display.
Index
Appendix
1)
54
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Additional Features
The XM® Radio Page provides information and control of the audio entertainment
features of the XM Satellite Radio.
2)
Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
3)
Press the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
AFCS
Turn the large FMS Knob to select the Auxiliary Page Group.
Nav/Com/
XPDR/Audio
1)
EIS
Selecting the XM Radio Page
Selecting a Category
Annun/
Alerts
Appendix
Press the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.
Or:
Index
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
3)
With the desired channel highlighted, press the ENT Key.
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Abnormal
Operation
2)
Additional
Features
While on the XM Radio Page, press the CHNL Softkey.
Hazard
Avoidance
Select an Available Channel within the Selected Category
Procedures
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Press the CATGRY Softkey on the XM Radio Page.
2) Press 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.
Flight
Planning
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.
GPS Nav
Active Channel and Channel List
1)
Flight
Instruments
XM® Radio Entertainment
55
Additional Features
1)
While on the XM Radio Page, press the CHNL Softkey.
2)
Press the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
3)
Press the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
4)
Press the ENT Key to activate the selected channel.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Entering a Channel Directly
AFCS
Assigning Channel Presets
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
Up to 15 channels from any category can be assigned a preset number.
1) On the XM Radio Page, while listening to an Active Channel that is wanted
for a preset, press the PRESETS Softkey to access the first five preset
channels (PS1 - PS5).
2) Press the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Pressing the
MORE Softkey repeatedly cycles through the preset channels.
3) Press the SET Softkey.
4) Press any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
1)
On the XM Radio Page, press the RADIO Softkey.
2)
Press the VOL Softkey to access the volume control softkeys.
3)
Press VOL + or VOL - softkeys to adjust the volume level.
4)
Press the MUTE Softkey to mute the radio audio.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Adjusting Volume
56
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
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
Abnormal COM Operation
Flight
Planning
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. In the event of a failure of both PFDs,
the emergency frequency (121.500 MHz) automatically becomes the active frequency
on both COM radios.
GPS Nav
NOTE: The Beechcraft 58/G58 Pilot’s Operating Handbook (POH) always takes
precedence over the information found in this section.
Hazard
Avoidance
Hazard Displays with Loss of GPS Position
Additional
Features
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.
Abnormal
Operation
Annun/
Alerts
Loss of Hazard Functions with Loss of GPS
Position
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
57
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
– DME Tuning
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath,
and Vertical Deviation
Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Extreme Pitch Indication
58
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Abnormal Operation
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
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/WAAS 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/WAAS 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.
Nav/Com/
XPDR/Audio
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.
EIS
While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
Flight
Instruments
Dead Reckoning
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
59
EIS
Flight
Instruments
Abnormal Operation
Symbolic Aircraft
(Map pages and Inset Map)
Dead Reckoning Indications
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. 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
CDI ‘DR’ Indication on PFD
60
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
Flight
Instruments
Annunciations & Alerts
WARNING Annunciation
Gear up with power below 13 in Hg or flaps
down.
Continuous Tone
(received through the
G1000 audio from
another source)
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
Repeating Tone
AFCS
GPS Nav
Flight
Planning
Procedures
Left alternator offline.
Right alternator offline.
Right and Left alternators offline.
L or R fuel flow is greater than 27.4 gph
L or R CHT is greater than 238 deg C.
L or R oil temp is greater than 116 deg C.
L or R oil press is greater than 100 psi.
L or R oil press is less than 10 psi.
L or R fuel qty is at zero.
Audio Alert
Nav/Com/
XPDR/Audio
L ALT INOP
R ALT INOP
L-R ALT INOP
FUEL FLOW HI
CHT HI
OIL TEMP HI
OIL PRESS HI
OIL PRESS LO
FUEL QTY LO
Alerts Window Message
EIS
Annunciation
Text
GEAR UP
Hazard
Avoidance
CAUTION Annunciation
Single Chime
Single Chime
Single Chime
Single Chime
Single Chime
Single Chime
Single Chime
Single Chime
Annun/
Alerts
Appendix
Single Chime
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
190-00526-02 Rev. A
Left starter relay has power applied.
Right starter relay has power applied.
Left bus voltage greater than 30 VDC.
Right bus voltage greater than 30 VDC.
Left bus voltage less than 24 V.
Right bus voltage less than 24 V.
Aft door not latched.
Press Low — Ops in icing conditions not
approved.
Press Low — Ops in icing conditions not
approved.
Audio Alert
Abnormal
Operation
R AIR PUMP
Alerts Window Message
Additional
Features
Annunciation
Text
L START ENGD
R START ENGD
LBUS VOLT HI
RBUS VOLT HI
LBUS VOLT LO
RBUS VOLT LO
AFT DOOR
L AIR PUMP
61
Annunciation
Text
OIL PRESS LO
FUEL QTY LO
ALT LOAD
Annunciation
Text
BUSES TIED
Audio Alert
L or R oil press is between 30 and 10 psi.
L or R fuel qty is less than or equal to 13 gal.
L or R alternator load exceeds 100 amps.
Single Chime
Single Chime
Single Chime
Alerts Window Message
Audio Alert
Right Bus is tied to Left Bus.
None
Alert Message
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.
Audio Alert
None
None
None
AFCS ALERTS
Condition
Annunciation
Description
Pitch Failure
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.
Yaw Damper Failure
YD control failure; AP also inoperative
System Failure
AP and MET are unavailable. FD may still be
available.
Elevator Mistrim Up
A condition has developed causing the pitch
servo to provide a sustained force. Be prepared
to apply nose up control wheel force upon
autopilot disconnect.
Index
Appendix
Alerts Window Message
ADVISORY Annunciation
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
62
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
Annunciation
Description
Flight
Instruments
Condition
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.
Aileron Mistrim Left
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.
Aileron Mistrim Right
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.
Rudder Mistrim Left
A condition has developed causing the yaw servo
to provide a sustained force. Ensure the slip/skid
indicator is centered and observe any maximum
fuel imbalance limits.
Rudder Mistrim Right
A condition has developed causing the yaw
servo to provide a sustained force. Ensure the
slip/skid indicator is centered and observe any
maximum fuel imbalance limits.
Preflight Test
Performing preflight system test. Upon
completion of the test, the aural alert will be
heard.
EIS
Elevator Mistrim Down
Procedures
Hazard
Avoidance
Additional
Features
“Pull Up”
or
Appendix
“Terrain, Terrain; Pull Up,
Pull Up”
or
“Terrain Ahead, Pull Up;
Terrain Ahead, Pull Up”
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
190-00526-02 Rev. A
Aural Message
Annun/
Alerts
Reduced Required
Terrain Clearance
Warning (RTC)
Abnormal
Operation
Excessive Descent
Rate Warning (EDR)
Flight
Planning
MFD
Pop-Up Alert
GPS Nav
Alert Type
AFCS
TAWS-B Alerts
PFD/MFD
TAWS-B Page
Annunciation
Nav/Com/
XPDR/Audio
Preflight system test has failed.
63
Alert Type
Imminent Terrain
Impact Warning (ITI)
Reduced Required
Obstacle Clearance
Warning (ROC)
Imminent Obstacle
Impact Warning
(IOI)
Reduced Required
Terrain Clearance
Caution (RTC)
Imminent Terrain
Impact Caution (ITI)
Reduced Required
Obstacle Clearance
Caution (ROC)
PFD/MFD
TAWS-B Page
Annunciation
MFD
Pop-Up Alert
or
or
or
or
or
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
Imminent Obstacle
Impact Caution (IOI)
or
Premature Descent
Alert Caution (PDA)
64
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Aural Message
Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”
or
“Terrain, Terrain; Pull Up,
Pull Up”
“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”
“Too Low, Terrain”
190-00526-02 Rev. A
Annunciations & Alerts
MFD
Pop-Up Alert
Aural Message
None
None
“Five-Hundred”
Altitude Callout
“500”
Negative Climb
Rate Caution (NCR)
“Don’t Sink”
or
“Too Low, Terrain”
or
AFCS
“Sink Rate”
Nav/Com/
XPDR/Audio
Excessive Descent
Rate Caution (EDR)
EIS
PFD/MFD
TAWS-B Page
Annunciation
Flight
Instruments
Alert Type
PFD/MFD
Alert
Annunciation
GPS Nav
TAWS-B System Status Annunciations
Aural
Message
TAWS TEST
None
None
“TAWS System
Test OK”
None
None
TERRAIN DATABASE FAILURE
None
TAWS-B System Test Fail
TAWS FAIL
“TAWS System
Failure”
Terrain or Obstacle database
unavailable or invalid, invalid
software configuration, system
audio fault
TAWS FAIL
“TAWS System
Failure”
NO GPS POSITION
“TAWS Not
Available”
None
“TAWS Not
Available”
None
“TAWS
Available”
System Test in Progress
None
TAWS Alerting is disabled
None
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Appendix
190-00526-02 Rev. A
None
Annun/
Alerts
Sufficient GPS signal received
after loss
Abnormal
Operation
Excessively degraded GPS
signal, Out of database
coverage area
Additional
Features
No GPS position
Hazard
Avoidance
MFD Terrain or Obstacle
database unavailable or invalid.
TAWS operating with PFD
Terrain or Obstacle databases
Procedures
System Test Pass
Flight
Planning
TAWS-B Page
Annunciation
Alert Type
65
Voice Alerts
Voice Alert
“Minimums, minimums”
EIS
Flight
Instruments
Annunciations & Alerts
“Traffic”
“TIS Not Available”
“Traffic, Traffic”
“Traffic Advisory System
Test Passed”
“Traffic Advisory System
Test Failed”
“TAS System Test
Passed”
“TAS System Test
Failed”
“One o’clock” through
“Twelve o’clock”
or “No Bearing”
“High”, “Low”, “Same
Altitude” (if within 200
feet of own altitude), or
“Altitude not available”
“Less than one mile”,
“One Mile” through
“Ten Miles”, or “More
than ten miles”
Played when the GTS 820 TAS system passes a pilot-initiated self
test.
Played when the GTS 820 TAS system fails a pilot-initiated self test.
Intruder bearing (GTS 820 only)
Intruder relative altitude (GTS 820 only)
Intruder distance (GTS 820 only)
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
“Vertical track”
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 (TIS and GTS 820).
The aircraft is outside the Traffic Information Service (TIS) coverage
area.
Played when a Traffic Advisory (TA) is issued (Skywatch TAS system).
Played when the Skywatch TAS system passes a pilot-initiated self
test.
Played when the Skywatch TAS system fails a pilot-initiated self test.
66
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
The PFD and/or MFD has incorrect software
installed. The system should be serviced.
Flight
Planning
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Annun/
Alerts
The PFD1 configuration module backup memory
has failed. The system should be serviced.
Abnormal
Operation
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.
Additional
Features
The PFD and/or MFD is overheating and is reducing
power consumption by dimming the display. If
problem persists, the system should be serviced.
Hazard
Avoidance
The PFD configuration settings do not match
backup configuration memory. The system should
be serviced.
The MFD configuration settings do not match
backup configuration memory. The system should
be serviced.
The MFD and PFD have different software versions
installed. The system should be serviced.
Procedures
190-00526-02 Rev. A
The PFD and/or MFD self-test has detected a
problem. The system should be serviced.
GPS Nav
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.
AFCS
MFD1 CONFIG – MFD1 config
error. Config service req’d.
Nav/Com/
XPDR/Audio
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.
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 PFD are not communicating with
each other. The system should be serviced.
EIS
Message
DATA LOST – Pilot stored data was
lost. Recheck settings.
Flight
Instruments
MFD & PFD Message Advisories
67
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
MFD & PFD Message Advisories (Cont.)
Message
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
Comments
The PFD1 voltage is low. The system should be
serviced.
The MFD voltage is low. The system should be
serviced.
Database Message Advisories
Message
MFD1 DB ERR – MFD1 navigation
database error exists.
PFD1 DB ERR – PFD1 navigation
database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
68
Comments
The MFD and/or PFD detected a failure in the
navigation database. Attempt to reload the
navigation database. If problem persists, the
system should be serviced.
The MFD and/or PFD detected a failure in the
basemap database.
The MFD and/or PFD detected a failure in the
terrain database. Ensure that the terrain card is
properly inserted in display. Replace terrain card. If
problem persists, the system should be serviced.
The terrain database is present on another LRU, but
is missing on the specified LRU.
The MFD and/or PFD detected a failure in the
obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, the system should be serviced.
The obstacle database is present on another LRU,
but is missing on the specified LRU.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
The MFD detected a failure in the ChartView
database (optional feature). Ensure the data card
is properly inserted. Replace data card. If problem
persists, system should be serviced.
The MFD detected a failure in the FliteCharts
database (optional feature). Ensure the data card
is properly inserted. Replace data card. If problem
persists, system should be serviced.
The MFD detected a failure in the Airport Directory
database. Ensure that the data card is properly
inserted. Replace data card. If problem persists, the
system should be serviced.
The PFD and MFD have different navigation
database versions or types (Americas, European,
etc.) installed. Crossfill is off. Install correct
navigation database version or type in all displays.
The PFD and MFD have different terrain database
versions or types installed. Install correct terrain
database version or type in all displays.
Flight
Planning
DB MISMATCH – Terrain database
mismatch.
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.
GPS Nav
DB MISMATCH – Navigation
database mismatch. Xtalk is off.
The airport terrain database is present on another
LRU, but is missing on the specified LRU.
AFCS
MFD1 DB ERR – MFD1 Airport
Directory database error exists.
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.
Nav/Com/
XPDR/Audio
MFD1 DB ERR – MFD1 FliteCharts
database error exists.
Comments
EIS
Message
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.
MFD1 DB ERR – MFD1 Chartview
database error exists.
Flight
Instruments
Database Message Advisories (Cont.)
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
69
Database Message Advisories (Cont.)
Message
DB MISMATCH – Obstacle
database mismatch.
DB MISMATCH – Airport Terrain
database mismatch.
NAV DB UPDATED – Active
navigation database updated.
TERRAIN DSP – [PFD1 or
MFD1] Terrain awareness display
unavailable.
Comments
The PFD and MFD have different obstacle database
installed. Install correct obstacle database in all
displays.
The PFD and MFD have different airport terrrain
databases installed. Install correct airport terrain
database in all displays.
System has updated the active navigation database
from the standby navigation database.
One of the terrain, airport terrain, or obstacle
databases required for TAWS in the specified PFD or
MFD is missing or invalid.
GMA 1347 Message Advisories
Message
GMA1 FAIL – GMA1 is inoperative.
GMA1 CONFIG – GMA1 config
error. Config service req’d.
MANIFEST – GMA1 software
mismatch, communication halted.
GMA1 SERVICE – GMA1 needs
service. Return unit for repair.
Comments
The audio panel self-test has detected a failure.
The audio panel is unavailable. The system should
be serviced.
The audio panel configuration settings do not
match backup configuration memory. The system
should be serviced.
The audio panel has incorrect software installed. The
system should be serviced.
The audio panel self-test has detected a problem in
the unit. Certain audio functions may still be available, and the audio panel may still be usable. The
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
70
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
system should be serviced.
Nav/Com/
XPDR/Audio
The GIA1 and/or GIA2 have an error in the audio
configuration. The system should be serviced.
AFCS
GPS Nav
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Flight
Planning
The GIA1 and/or GIA2 temperature is too high. If
problem persists, the system should be serviced.
Procedures
Hazard
Avoidance
The GIA1 and/or GIA2 self-test has detected
a problem in the unit. The system should be
serviced.
Additional
Features
Abnormal
Operation
A GIA mismatch has been detected, where only
one is WAAS capable.
Annun/
Alerts
Appendix
The GIA1 and/or GIA 2 has incorrect software
installed. The system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
190-00526-02 Rev. A
Comments
EIS
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs
service. Return the unit for repair.
GIA2 SERVICE – GIA2 needs
service. Return the unit for repair.
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.
Flight
Instruments
GIA 63W Message Advisories
71
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 63W Message Advisories (Cont.)
Message
MANIFEST – GFC 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.
Comments
Incorrect servo software is installed, or gain
settings are incorrect.
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
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.
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.
72
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.
GPS integrity is insufficient for the current phase
of flight.
Loss of GPS navigation due to insufficient
satellites.
Loss of GPS navigation due to position error.
Loss of GPS navigation due to GPS failure.
Abort approach due to loss of GPS navigation.
Vertical guidance generated by WAAS is
unavailable, use LNAV only minimums.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
A failure has been detected in the GPS1 and/or
GPS2 receiver. The receiver may still be available.
The system should be serviced.
AFCS
A failure has been detected in the NAV1 and/or
NAV2 receiver. The receiver may still be available.
The system should be serviced.
GPS Nav
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.
Flight
Planning
Procedures
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 glideslope receiver
1 and/or receiver 2. The receiver may still be
available. The system should be serviced when
possible.
Additional
Features
G/S2 FAIL – G/S2 is inoperative.
A failure has been detected in glideslope receiver 1
and/or receiver 2. The system should be serviced.
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
190-00526-02 Rev. A
Comments
The GEA1 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
The #1 GEA 71 has incorrect software installed.
The G1000 system should be serviced.
Appendix
MANIFEST – GEA1 software
mismatch, communication halted.
Annun/
Alerts
GEA 71 Message Advisories
Message
GEA1 CONFIG – GEA1 config error.
Config service req’d.
Hazard
Avoidance
G/S1 FAIL – G/S1 is inoperative.
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
Displayed after passing the first waypoint of a
true north approach when the nav angle is set to
‘AUTO’.
EIS
Message
TRUE APR – True north approach.
Change HDG reference to TRUE.
Flight
Instruments
GIA 63W Message Advisories (Cont.)
73
GTX 33 Message Advisories
Message
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
Comments
The transponder configuration settings do not
match those of backup configuration memory. The
system should be serviced.
The transponder has incorrect software installed.
MANIFEST – GTX1 software
The system should be serviced.
mismatch, communication halted.
The #1 transponder should be serviced when
XPDR1 SRVC – XPDR1 needs
possible.
service. Return unit for repair.
XPDR1 FAIL – XPDR1 is inoperative. There is no communication with the #1
transponder.
GRS 77 Message Advisories
Message
AHRS1 TAS – AHRS1 not receiving
airspeed.
AHRS1 GPS – AHRS1 not receiving
any GPS information.
AHRS1 GPS – AHRS1 not receiving
backup GPS information.
AHRS1 GPS – AHRS1 operating
exclusively in no-GPS mode.
AHRS MAG DB – AHRS magnetic
model database version mismatch.
AHRS1 SRVC – AHRS1 Magneticfield model needs update.
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 and #2 AHRS magnetic model
database versions do not match.
The #1 AHRS earth magnetic field model is out of
date. Update magnetic field model when practical.
Index
Appendix
Annun/
Alerts
Additional
Features
AHRS1 GPS – AHRS1 using backup
GPS source.
Abnormal
Operation
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
74
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
Appendix
Comments
The GDC 74A has incorrect software installed.
The G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
190-00526-02 Rev. A
Annun/
Alerts
Message
MANIFEST – GDC1 software
mismatch, communication halted.
Abnormal
Operation
GDC 74A Message Advisories
Additional
Features
Comments
GDL 69 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
A failure has been detected in the GDL 69.
GDL69 FAIL – GDL 69 has failed.
The receiver is unavailable. The G1000 system
should be serviced
MANIFEST – GDL software mismatch, The GDL 69 has incorrect software installed. The
G1000 system should be serviced.
communication halted.
Hazard
Avoidance
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
Procedures
GDL 69/69A Message Advisories
Flight
Planning
Comments
A fault has occurred in the #1 GMU 44. Heading
is flagged as invalid. The AHRS uses GPS for
backup mode operation. The G1000 system
should be serviced.
The GMU 44 has incorrect software installed.
The G1000 system should be serviced.
GPS Nav
MANIFEST – GMU1 software
mismatch, communication halted.
AFCS
Message
HDG FAULT – AHRS1 magnetometer
fault has occurred.
Nav/Com/
XPDR/Audio
GMU 44 Message Advisories
EIS
Message
Comments
GEO LIMITS – AHRS1 too far North/ The aircraft is outside geographical limits for
approved AHRS operation. Heading is flagged as
South, no magnetic compass.
invalid.
The #1 AHRS has incorrect software installed. The
MANIFEST – GRS1 software
system should be serviced.
mismatch, communication halted.
Flight
Instruments
GRS 77 Message Advisories (Cont.)
75
GWX 68 Message Advisories
Message
GWX CONFIG – GWX config error.
Config service req’d.
Comments
GWX 68 configuration settings do not match
those of the GDU configuration. The G1000
system should be serviced.
The GDU is not receiving status packet from the
GWX FAIL – GWX is inoperative.
GWX 68 or the GWX 68 is reporting a fault. The
GWX 68 radar system should be serviced.
GWX SERVICE – GWX needs service. A failure has been detected in the GWX 68. The
GWX 68 may still be usable.
Return unit for repair.
The GWX 68 has incorrect software installed. The
MANIFEST – GWX software
G1000 system should be serviced.
mismatch, communication halted.
WX ALERT – Possible severe weather The GWX 68 indicates severe weather within
±10 degrees of the aircraft heading at a range of
ahead.
80 to 320 nm.
GTS 820 Message Advisories
Message
GTS CONFIG – GTS config error.
Config service req’d.
MANIFEST – GTS software
mismatch, communication halted.
Comments
The GTS and GDU have incompatible
configurations. This alert is also set when the GTS
has an invalid mode S address configured or the
mode S address does not match both XPDR mode
S addresses.
The GTS has incorrect software installed. The
G1000 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
76
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
Abnormal
Operation
Annun/
Alerts
Appendix
Index
77
Additional
Features
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Hazard
Avoidance
190-00526-02 Rev. A
Procedures
FPL TRUNC – Flight plan has been
truncated.
Flight
Planning
DB CHANGE – Database changed.
Verify stored airways.
GPS Nav
DB CHANGE – Database changed.
Verify user modified procedures.
AFCS
TIMER EXPIRD – Timer has expired.
Nav/Com/
XPDR/Audio
FPL WPT MOVE – Flight plan
waypoint moved.
Comments
Upon power-up, the system detects that a stored
flight plan waypoint is locked. This occurs when
an navigation database update eliminates an
obsolete waypoint. The flight plan cannot find
the specified waypoint and flags this message.
This can also occur with user waypoints in a flight
plan that is deleted.
Remove the waypoint from the flight plan if it no
longer exists in any database,
Or
update the waypoint name/identifier to reflect
the new information.
The system has detected that a waypoint coordinate
has changed due to a new navigation database
update. Verify that stored flight plans contain
correct waypoint locations.
The system notifies the pilot that the timer has
expired.
This occurs when a stored flight plan contains
procedures that have been manually edited. This
alert is issued only after an navigation database
update. Verify that the user-modified procedures
in stored flight plans are correct and up to date.
This occurs when a stored flight plan contains
an airway that is no longer consistent with the
navigation database. This alert is issued only
after an navigation database update. Verify
use of airways in stored flight plans and reload
airways as needed.
This occurs when a newly installed navigation
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.
EIS
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Flight
Instruments
Miscellaneous Message Advisories
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
LOCKED FPL – Cannot navigate
locked flight plan.
Comments
This occurs when the pilot attempts to activate a
stored flight plan that contains locked waypoint.
Remove locked waypoint from flight plan.
Update flight plan with current waypoint.
WPT ARRIVAL – Arriving at waypoint Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
-[xxxx]
A steep turn is 15 seconds ahead. Prepare to turn.
STEEP TURN – Steep turn ahead.
The aircraft is inside the airspace.
INSIDE ARSPC – Inside airspace.
ARSPC AHEAD – Airspace ahead less Special use airspace is ahead of aircraft. The
aircraft will penetrate the airspace within 10
than 10 minutes.
minutes.
Special use airspace is near and ahead of the
ARSPC NEAR – Airspace near and
aircraft position.
ahead.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft
position.
than 2 nm.
The system notifies the pilot that the loaded approach
APR INACTV – Approach is not
is not active. Activate approach when required.
active.
The system notifies the pilot to load the approach
SLCT FREQ – Select appropriate
frequency for the appropriate NAV receiver.
frequency for approach.
Select the correct frequency for the approach.
The system notifies the pilot to set the CDI to the
SLCT NAV – Select NAV on CDI for
correct NAV receiver. Set the CDI to the correct
approach.
NAV receiver.
PTK FAIL – Parallel track unavailable:
Bad parallel track geometry.
bad geometry.
PTK FAIL – Parallel track unavailable:
IAF waypoint for parallel offset has been passed.
past IAF.
PTK FAIL – Parallel track unavailable:
IAF waypoint for parallel offset has been passed.
past IAF.
UNABLE V WPT – Can’t reach current The current vertical waypoint can not be reached
within the maximum flight path angle and vertical
vertical waypoint.
speed constraints. The system automatically
transitions to the next vertical waypoint.
78
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
The lateral flight plan contains a procedure turn,
vector, or other unsupported leg type prior to the
active vertical waypoint. This prevents vertical
guidance to the active vertical waypoint.
The current crosstrack exceeds the limit, causing
VNV – Unavailable. Excessive
vertical deviation to go invalid.
crosstrack error.
A parallel course has been selected, causing the
VNV – Unavailable. Parallel course
vertical deviation to go invalid.
selected.
The position of the selected waypoint [xxxx]
NO WGS84 WPT – Non WGS 84
is not calculated based on the WGS84 map
waypoint for navigation -[xxxx]
reference datum and may be positioned in error
as displayed. Do not use GPS to navigate to the
selected non-WGS84 waypoint.
The system is no longer receiving data from the
TRAFFIC FAIL – Traffic device has
traffic system. The traffic device should be serviced.
failed.
FAILED PATH – A data path has failed. A data path connected to the GDU, GSD 41, or
the GIA 63/W has failed.
MAG VAR WARN – Large magnetic The GDU’s internal model cannot determine the
exact magnetic variance for geographic locations
variance. Verify all course angles.
near the magnetic poles. Displayed magnetic
course angles may differ from the actual
magnetic heading by more than 2°.
SVS – SVS DISABLED: Out of available Synthetic Vision is disabled because the aircraft is
not within the boundaries of the installed terrain
terrain region.
database.
Synthetic Vision is disabled because a terrain
SVS – SVS DISABLED: Terrain DB
database of sufficient resolution (9 arc-second or
resolution too low.
better) is not currently installed.
Message criteria entered by the user.
SCHEDULER [#] – <message>.
EIS
Message
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Unsupported leg
type in flight plan.
Flight
Instruments
Miscellaneous Message Advisories (Cont.)
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
79
Miscellaneous Message Advisories (Cont.)
Message
CHECK CRS – Database course for
LOC1 / [LOC ID] is [CRS]°.
CHECK CRS – Database course for
LOC2 / [LOC ID] is [CRS]°.
[PFD1 or MFD1] CARD 1 REM –
Card 1 was removed. Reinsert card.
[PFD1 or MFD1] CARD 2 REM –
Card 2 was removed. Reinsert card.
[PFD1 or MFD1] CARD 1 ERR –
Card 1 is invalid.
[PFD1 or MFD1] CARD 2 ERR –
Card 2 is invalid.
Comments
Selected course for LOC1 differs from published
localizer course by more than 10 degrees.
Selected course for LOC2 differs from published
localizer course by more than 10 degrees.
The SD card was removed from the top card slot
of the PFD or MFD. The SD card needs to be
reinserted.
The SD card was removed from the bottom card
slot of the PFD or MFD. The SD card needs to be
reinserted.
The SD card in the top card slot of the PFD or
MFD contains invalid data.
The SD card in the bottom card slot of the PFD or
MFD contains invalid data.
Flight Plan Import/Export Messages
In some circumstances, some messages may appear in conjunction with others.
Flight Plan Import/Export Results
‘Flight plan successfully imported.’
‘File contained user waypoints only. User
waypoints imported successfully. No
stored flight plan data was modified.’
‘No flight plan files found to import.’
‘Flight plan import failed.’
‘Flight plan partially imported.’
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
Description
A flight plan file stored on the SD card was
successfully imported as a stored flight plan.
The file stored on the SD card did not contain
a flight plan, only user waypoints. These
waypoints have been saved to the system
user waypoints. No flight plans stored in the
system have been modified.
The SD card contains no flight plan data.
Flight plan data was not successfully
imported from the SD card.
Some flight plan waypoints were successfully
imported from the SD card, however others
had errors and were not imported. A partial
stored flight plan now exists in the system.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Annunciations & Alerts
Flight Plan Import/Export Results
‘File contained user waypoints only.’
Abnormal
Operation
Annun/
Alerts
Appendix
Index
81
Additional
Features
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Hazard
Avoidance
190-00526-02 Rev. A
Procedures
‘Flight plan export failed.’
Flight
Planning
‘Flight plan successfully exported.’
GPS Nav
‘One or more user waypoints renamed.’
AFCS
‘User waypoint database full. Not all
loaded.’
Nav/Com/
XPDR/Audio
‘Some waypoints not loaded. Waypoints
locked.’
EIS
‘Too many points. Flight plan truncated.’
Description
The file stored on the SD card did not contain
a flight plan, only user waypoints. One or
more of these waypoints did not import
successfully.
The flight plan on the SD card contains more
waypoints than the system can support.
The flight plan was imported with as many
waypoints as possible.
The flight plan on the SD card contains one
or more waypoints that the system cannot
find in the navigation database. The flight
plan has been imported, but must be edited
within the system before it can be activated
for use.
The flight plan file on the SD card contains
user waypoints. The quantity of stored user
waypoints has exceeded system capacity,
therefore not all the user waypoints on the
SD card have been imported. Any flight plan
user waypoints that were not imported are
locked in the flight plan. The flight plan must
be edited within the system before it can be
activated for use.
One or more imported user waypoints were
renamed when imported due to naming
conflicts with waypoints already existing in
the system.
The stored flight plan was successfully
exported to the SD card.
The stored flight plan was not successfully
exported to the SD card. The SD card may
not have sufficient available memory or the
card may have been removed prematurely.
Flight
Instruments
Flight Plan Import/Export Messages (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
Blank Page
82
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Appendix
Flight
Instruments
Appendix
PFD Softkey Map
EIS
ALERTS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Top Level PFD Softkeys
ALERTS
Flight
Planning
Additional
Features
Inset Map Softkeys
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
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
83
Index
DCLTR (3)
Appendix
Removes Inset Map
Annun/
Alerts
OFF
Abnormal
Operation
Displays Inset Map in PFD lower left corner
INSET
Hazard
Avoidance
Press the BACK Softkey to return to
the top-level softkeys.
Procedures
ALERTS
STRMSCP
EIS
Flight
Instruments
Appendix
TRAFFIC
Displays traffic information on Inset Map
TOPO
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Inset Map
Displays terrain information on Inset Map
TERRAIN
Press to display the Stormscope lightning
data on the Inset Map (within a 200 nm
radius of the aircraft)
Displays NEXRAD weather and coverage
information on Inset Map (optional feature)
Displays XM lightning information on Inset
Map (optional feature)
Nav/Com/
XPDR/Audio
STRMSCP
AFCS
NEXRAD
GPS Nav
XM LTNG
Flight
Planning
(optional)
ALERTS
HSI FRMT
Procedures
SYN VIS
ALT UNIT
ALERTS
Additional
Features
Hazard
Avoidance
Press the BACK Softkey to
return to the top-level softkeys
Abnormal
Operation
METERS
360 HSI
IN
HPA
ARC HSI
ALERTS
ALERTS
Annun/
Alerts
ALERTS
Appendix
PATHWAY
SYN TERR HRZN HDG APTSIGNS
ALERTS
Index
PFD Configuration Softkeys
84
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Appendix
SYN VIS
Annun/
Alerts
Appendix
Index
85
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Additional
Features
190-00526-02 Rev. A
Hazard
Avoidance
360 HSI
ARC HSI
Procedures
HSI FRMT
Displays the DME Information Window
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree format
Displays the HSI in an arc format
Flight
Planning
DME
BRG1
GPS Nav
WIND
AFCS
DFLTS
HRZN HDG Displays compass heading along the
Zero-Pitch line
APTSIGNS Displays position markers for airports
within approximately 15 nm of the
current aircraft position. Airport
identifiers are displayed when the
airport is within approximately 9 nm.
Resets PFD to default settings,
including changing units to standard
Displays softkeys to select wind data
parameters
Headwind/tailwind and crosswind
OPTN 1
arrows with numeric speed components
Wind direction arrow and numeric
OPTN 2
speed
Wind direction arrow with numeric
OPTN 3
direction and speed
Information not displayed
OFF
Nav/Com/
XPDR/Audio
SYN TERR
EIS
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
Flight
Instruments
PFD
Appendix
Cycles the Bearing 2 Information
Window through NAV2 or GPS/
waypoint identifier and GPS-derived
distance information.
Displays softkeys for setting the altimeter
and BARO settings to metric units
EIS
Flight
Instruments
BRG2
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
ALT UNIT
Flight
Planning
STD BARO
METERS
When enabled, displays altimeter in
meters
IN
Press to display the BARO setting as
inches of mercury
HPA
Press to display the BARO setting as
hectopacals
Sets barometric pressure to 29.92 in Hg
(1013 hPa)
Procedures
ALERTS
Hazard
Avoidance
ADS-B TX
Additional
Features
Press the BACK Softkey to return
to the top-level softkeys.
ALERTS
Abnormal
Operation
Press the BACK Softkey to return
to the previous level softkeys.
Transponder Softkeys
XPDR
Appendix
Annun/
Alerts
ALERTS
STBY
Index
ON
86
Displays transponder mode selection
softkeys
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
interrogations)
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Appendix
Displays Alerts Window
Abnormal
Operation
ALERTS
Additional
Features
Displays Nearest Airports Window
Hazard
Avoidance
NRST
Procedures
TMR/REF
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Displays Timer/References Window
IDENT
Flight
Planning
ADS-B TX
GPS Nav
IDENT
AFCS
CODE
Nav/Com/
XPDR/Audio
Removes numbers entered, one at a time
VFR
EIS
BKSP
GND
Flight
Instruments
0—7
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
Activates the Special Position Identification
(SPI) pulse for 18 seconds, identifying the
transponder return on the ATC screen
Activates/deactivates transmission of the
aircraft’s three-dimensional position and
aircraft heading for reception by ADS-B
systems.
Use numbers to enter code
ALT
Annun/
Alerts
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
87
MFD Softkey Map
DCLTR
MAP
EIS
Flight
Instruments
Appendix
(optional)
SHW CHRT
CHKLIST
DCLTR-1
Press the BACK Softkey on
this level to return to the top
softkey level.
DCLTR-2
DCLTR-3
Nav/Com/
XPDR/Audio
(optional)
TRAFFIC
TOPO
TERRAIN
AIRWAYS
STRMSCP
Press the BACK Softkey on
this level to return to the top
softkey level.
(optional)
(optional)
NEXRAD
XM LTNG
BACK
AFCS
AIRWY ON
AIRWY LO
194 GAL
BACK
AIRWAY HI
MFD Softkeys
ENGINE
Displays the LEAN and SYSTEM
softkeys
Displays the engine leaning softkeys
LEAN
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
166 GAL
Abnormal
Operation
Additional
Features
CYL SLCT Selects the desired cylinder for
monitoring
Highlights the first cylinder that peaks
ASSIST
and displays information for that
cylinder
Press to return to the top level softkeys
BACK
Displays fuel system softkeys
Annun/
Alerts
SYSTEM
Index
Appendix
DEC FUEL Press to decrease fuel quantity in 1gallon increments
INC FUEL Press to increase fuel quantity in 1gallon increments
166 GAL Press to reset fuel to 166 gallons
88
194 GAL
Press to reset fuel to 194 gallons
BACK
Press to return to the top level softkeys
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Appendix
TRAFFIC
Annun/
Alerts
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Abnormal
Operation
190-00526-02 Rev. A
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
Additional
Features
DCLTR
Hazard
Avoidance
BACK
Procedures
XM LTNG
Flight
Planning
NEXRAD
GPS Nav
STRMSCP
AFCS
AIRWAYS
Nav/Com/
XPDR/Audio
TERRAIN
EIS
TOPO
Enables second-level Navigation Map
softkeys
Displays traffic information on
Navigation Map
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
Displays Stormscope weather and
coverage information on Navigation
Map (optional feature)
Displays NEXRAD weather and
coverage information on Navigation
Map (optional feature)
Displays XM lightning information on
Navigation Map (optional feature)
Returns to top-level softkeys
Flight
Instruments
MAP
89
When available, displays optional
airport and terminal procedure charts
When available, displays optional
checklists
SHW CHRT
CHKLIST
Database Updates
The system uses Secure Digital (SD) cards to load and store various types of data.
For basic flight operations, SD cards are required for database storage as well as
Jeppesen navigation and Jeppesen ChartView database updates. Not all SD cards are
compatible with the G1000. Use only SD cards supplied by Garmin or the aircraft
manufacturer.
Information regarding the various databases may be viewed on the AUX-System
Status Page.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
Index
Display Database
Selection Softkey
AUX-System Status Page
90
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Appendix
AFCS
PFD1 DB Selected
GPS Nav
Display Database Selection Softkey
The following databases are stored on Supplemental Data Cards provided by
Garmin:
Procedures
• Airport Directory
(AOPA)
Abnormal
Operation
Annun/
Alerts
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.
Additional
Features
After subscribing to the desired database product updates, these updated databases
are copied to each Supplemental Data Card for each display (the card that contains the
FliteCharts or ChartView database resides in the MFD). Since these databases are not
stored internally in the displays, these Supplemental Data Cards must remain in the
bottom card slot of each display.
Hazard
Avoidance
• Obstacle
• SafeTaxi
• FliteCharts
Flight
Planning
Garmin Databases
• Expanded basemap
• Terrain
• Airport terrain
Nav/Com/
XPDR/Audio
MFD1 DB Selected
EIS
Unselected
Flight
Instruments
The Display Database Selection Softkey is used to place the cursor in the Database
Window. Upon first press of the Display Database Selection Softkey, the softkey will
change to a selected state (black text on gray background) and the cursor will appear
in the Database Window. At this point the user can scroll through all databases in
the Database Window to view status information. If the Display Database Selection
Softkey is pressed repeatedly, the softkey will switch between PFD1 and MFD1.
Database status information in the Database Window will reflect the database of the
PFD or MFD.
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
91
Obtaining Garmin Database Updates
The Garmin database updates can be obtained by following the instructions
detailed in the ‘Aviation Databases’ section of the Garmin website (fly.garmin.com).
Once the updated files have been downloaded from the website, a PC equipped with
an appropriate SD card reader is used to unpack and copy the new databases onto the
appropriate Supplemental Data Cards. Equipment required to perform the update is
as follows:
• Windows-compatible PC computer (Windows 2000 or XP recommended)
• SD Card Reader: SanDisk SDDR-93, SanDisk SDDR-99, Verbatim #96504, or
equivalent
• Updated database obtained from the Garmin website
• Existing Supplemental Database SD Card (010-00330-41, -42, or -43) from the
MFD. The supplemental data card from the MFD should be used because all
databases (except the active navigation database) are required to reside on this
card.
Jeppesen Databases
Note: The Jeppesen aviation navigation database is now referred to as the
‘navigation database’. Previously this database had been referred to as the
‘aviation database’.
The ChartView database should be copied to the Supplemental Data Card which
will reside in the bottom card slot on the MFD. The navigation database is be loaded
from the Jeppesen or user supplied SD data card. Contact Jeppesen (www.jeppesen.
com) for subscription and update information.
The navigation database is loaded from an SD card inserted into the top card slot
of each displayed. The database is copied from the SD card in the top card slot to the
display’s internal memory.
Loading Updated Databases
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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
92
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Appendix
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
AFCS
Loading the Garmin database updates:
1) With system power OFF, remove the MFD database card from the bottom
card slot of the MFD.
2) Update the Garmin databases on the MFD card.
3) Insert the MFD database card into the bottom card slot of the MFD.
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.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Database Information on the Power-up Screen
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.
7)
Turn the small FMS Knob to select the System Status Page.
8)
Make sure the SYNC DBS Softkey is in the enabled state.
9)
Monitor the Sync Status in the Database Window. Wait for all databases to
complete synching, indicated by ‘Complete’ being displayed.
Abnormal
Operation
5)
Annun/
Alerts
Appendix
10) Remove and reapply power to the system.
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Index
11) Turn the large FMS Knob to select the AUX Page group on the MFD.
93
Appendix
Flight
Instruments
12) Turn the small FMS Knob to select the System Status Page.
EIS
13) Press the Display Database Selection Softkey to show database information
for each display (MFD1 DB, PFD1 DB). Verify the correct database cycle
information is shown for each database for each display.
AFCS
Nav/Com/
XPDR/Audio
Canceling an automatic database synchronization:
1) While synchronization is in progress, press the SYNC DBS Softkey to
disable automatic database synchronization.
2) Acknowledge the cancelation by pressing the ENT Key.
Loading the Jeppesen navigation database:
Procedures
Copy the new navigation database to an SD card obtained from Garmin, or
the aircraft manufacturer.
2)
3)
With the G1000 system OFF, insert the SD card containing the new
navigation database version into the top card slot of the MFD (label of SD
card facing left).
Turn the G1000 system ON. A prompt similar to the following illustration is
displayed:
Abnormal
Operation
Additional
Features
1)
Hazard
Avoidance
Flight
Planning
GPS Nav
NOTE: Loading the Jeppesen navigation 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.
Index
Appendix
Annun/
Alerts
Navigation Database Load Prompt
94
4)
Press the YES Softkey to update the navigation database in the MFD.
5)
After the update completes, the display starts in normal mode.
6)
Turn the G1000 system OFF and remove the SD card from the top card slot.
7)
Repeat steps 2 through 6 for the PFD.
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Appendix
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.
Flight
Instruments
8)
Nav/Com/
XPDR/Audio
11) Press the Display Database Selection Softkey to show navigation database
information for each display (MFD1 DB, PFD1 DB).
EIS
10) Turn the small FMS Knob to select the System Status Page.
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Check Database Cycle Number (MFD shown)
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
95
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Appendix
Blank Page
96
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Index
E
Edit a flight plan 31
F
Hazard
Avoidance
D
J
Databases 90
Database synchronization 94
Jeppesen 53
Abnormal
Operation
HF 10
Horizon heading 51
Horizontal scan 47
Additional
Features
CDI 1, 10, 78
Cell 39, 40
Cell mode 40
Channel Presets 56
ChartView 52, 53
Clearance player 11
Clearance Recorder 11
Code selection softkeys 9
COM 10, 11, 57
I
Annun/
Alerts
Appendix
Inhibit 45
Inhibit TAWS 45
Inset Map 83, 84
IOI 64
Index
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
Procedures
Gain 47
Ground mapping 48
H
Flight
Planning
G
GPS Nav
FD 62
Flight Director 13
Flight path marker 51
Flight plan import/export messages 80,
81
FliteCharts® 52, 53
Frequency Transfer 10
C
190-00526-02 Rev. A
AFCS
Barometric Altitude Minimums 3
Barometric pressure 86
Bearing line 47, 48
Nav/Com/
XPDR/Audio
B
EIS
Activate a flight plan 18
Active Channel 55
ADF 9, 10, 58
ADS-B 87
AHRS 74, 75
Airport Signs 51, 52
Airways 89
ALT 43
Altitude mode 43
Altitude volume 43
Antenna stabilization 48
Antenna tilt 46
AOPA’s Airport Directory 54
AP 62
Audio panel controls
NAV1, NAV2 10
Autopilot 62, 63
Database updates 90, 92, 93
DCLTR Softkey 52
Dead Reckoning 59
Declutter 58, 83, 89
Direct-to 17
DME 9, 10
DR mode 59, 60
Flight
Instruments
A
Index-1
Flight
Instruments
Index
L
S
Lightning 39, 40, 84
SafeTaxi® 52
Sector scan 48
Secure Digital (SD) cards 90
STAB 48
Standby 46
Store Flight Plan 31
Stormscope lightning data 39, 40, 84
Strike 39
Strike mode 40
Supplemental Data Card 91, 92
SVS 51, 79
Synthetic Vision System 51
Map panning 41
Message advisories 67–70, 72–80
MET 62
METAR 41
Minimums 66
Mistrim 62, 63
MKR/MUTE 11
Mode S 87
Mode selection softkeys 9
Multi Function Display (MFD)
Softkeys 88
N
NAV 10
NAV1 1, 10
NAV2 1, 10
Navigation database 19, 20, 69
NEXRAD 41, 42, 84, 89
O
OBS 2
Obstacles 70, 71
Overspeed Protection 14
P
Pathways 51, 52
R
Reversionary mode 57
ROC 64
T
TA 66
TAF 41
TAS 43, 66, 74
TAWS 44, 45, 63
Terrain 44, 69, 84, 89
Tilt line 46
Timer 77
Topographical data 84, 89
Traffic 39, 43, 84, 89
Traffic Advisory 66
Traffic advisory 42
Traffic map page 43, 44
Transponder 9, 86, 87
V
Vertical speed guidance 20
Vertical track 66
VNV 17, 58, 79
Vspeed 2
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
M
Index-2
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
190-00526-02 Rev. A
Index
Flight
Instruments
W
EIS
WAAS 71
WATCH® 48
Waypoint Selection Submenu 27, 28
Weather Attenuated Color Highlight 48
Weather data link page 41
Weather radar 46
Wind data 85
Nav/Com/
XPDR/Audio
AFCS
X
GPS Nav
XM lightning 84, 89
XM weather 41
XPDR Softkey 9
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00526-02 Rev. A
Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
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 Beechcraft 58/G58
190-00526-02 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
© 2005, 2007-2010 Garmin Ltd. or its subsidiaries
190-00526-02 Rev. A
Was this manual useful for you? yes no
Thank you for your participation!

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

Download PDF

advertising