Garmin DA42-L360 GPS Receiver User Manual

G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Diamond DA42-L360
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 © 2004-2010 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 1054.01 or later for the Diamond
DA42-L360. 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
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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. FliteCharts®,
and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be
used without the express permission of Garmin.
NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® is a registered trademark
of L-3 Communications; and XM® is a registered trademark of XM Satellite Radio, Inc.
August, 2010
190-01062-01 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 DA42-L360
190-01062-01 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 Diamond DA42-L360
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
Diamond DA42-L360 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.
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
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 DA42-L360
190-01062-01 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.
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Record of Revisions
Part Number
190-01062-00
190-01062-01
Change Summary
Initial release
Added Synthetic Vision System
Added Terrain-SVS
Added other GDU 9.05 parameters
Revision Date of Revision
A
190-01062-01 Rev. A
August, 2010
Affected Pages
All
Description
Production release
Garmin G1000 Cockpit Reference Guide for the DA42-L360
RR-1
Record of Revisions
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RR-2
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Table of Contents
Flight Instruments. ............................................................................................................... 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure.............................................................................. 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............................................................................................................. 2
Set Barometric Minimum Descent Altitude......................................................................... 3
Displaying Wind Data............................................................................................................... 3
Changing HSI Format................................................................................................................ 3
Engine Indication System. ................................................................................................ 5
Engine Display............................................................................................................................ 5
System Display........................................................................................................................... 6
Lean Display................................................................................................................................ 8
Nav/Com/Transponder/Audio Panel......................................................................... 9
Enter or Change Flight ID........................................................................................................ 9
Enter a Transponder Code....................................................................................................... 9
ADF Tuning (Optional)............................................................................................................... 9
DME Tuning (Optional)............................................................................................................ 10
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
GFC 700 Automatic Flight Control System (Optional)............................. 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................................................................................................ 23
Delete a User Waypoint.......................................................................................................... 24
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
i
Table of Contents
Create a New Flight Plan....................................................................................................... 24
Insert a Waypoint in the Active Flight Plan....................................................................... 25
Enter an Airway in a Flight Plan........................................................................................... 26
Invert An Active Flight Plan................................................................................................... 26
Remove a Departure, Arrival, Approach, or Airway from a Flight Plan...................... 27
Store a Flight Plan................................................................................................................... 27
Edit a Stored Flight Plan........................................................................................................ 27
Delete a Waypoint from the Flight Plan............................................................................. 28
Invert and Activate a Stored Flight Plan............................................................................ 28
Copy a Flight Plan.................................................................................................................... 29
Delete a Flight Plan................................................................................................................. 29
Graphical Flight Plan Creation.............................................................................................. 29
Procedures................................................................................................................................. 31
Load and Activate a Departure Procedure........................................................................ 31
Activate A Departure Leg...................................................................................................... 31
Load An Arrival Procedure..................................................................................................... 31
Activate An Arrival Leg.......................................................................................................... 32
Load and/or Activate an Approach Procedure.................................................................. 32
Activate An Approach in the Active Flight Plan................................................................ 33
Activate a Vector to Final Approach Fix............................................................................. 33
Activate A Missed Approach in the Active Flight Plan.................................................... 34
Hazard Avoidance................................................................................................................. 35
Customizing the Hazard Displays on the Navigation Map............................................. 35
STORMSCOPE® (Optional)...................................................................................................... 35
XM Weather (Optional)........................................................................................................... 37
Traffic Systems......................................................................................................................... 38
Terrain And Obstacle Proximity............................................................................................ 41
Terrain-SVS................................................................................................................................ 41
Additional Features............................................................................................................ 45
Synthetic Vision (Optional).................................................................................................... 45
Terminal Procedure Charts.................................................................................................... 46
XM® Radio Entertainment..................................................................................................... 48
Abnormal Operation.......................................................................................................... 51
Reversionary Mode................................................................................................................. 51
Abnormal COM Operation..................................................................................................... 51
Hazard Displays with Loss of GPS Position........................................................................ 51
Unusual Attitudes.................................................................................................................... 52
Dead Reckoning....................................................................................................................... 53
ii
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Table of Contents
Annunciations & Alerts................................................................................................... 55
WARNING Annunciation......................................................................................................... 55
CAUTION Annunciation........................................................................................................... 55
Annunciation Advisory Alerts............................................................................................... 56
Alert Message........................................................................................................................... 56
AFCS Alerts................................................................................................................................ 56
Terrain-SVS Alerts.................................................................................................................... 57
Voice Alerts............................................................................................................................... 59
MFD & PFD Message Advisories........................................................................................... 59
Database Message Advisories.............................................................................................. 60
GMA 1347 Message Advisories............................................................................................. 63
GIA 63 Message Advisories.................................................................................................... 63
GIA 63W Message Advisories................................................................................................ 66
GEA 71 Message Advisories................................................................................................... 68
GTX 33 Message Advisories................................................................................................... 69
GRS 77 Message Advisories................................................................................................... 69
GMU 44 Message Advisories................................................................................................. 70
GDC 74A Message Advisories................................................................................................ 70
GDL 69A Message Advisories................................................................................................ 71
Miscellaneous Message Advisories...................................................................................... 71
Appendix........................................................................................................................................ 75
PFD Softkey Map..................................................................................................................... 75
MFD Softkey Map.................................................................................................................... 80
Index..........................................................................................................................................Index-1
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
iii
Table of Contents
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iv
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Flight Instruments
Flight
Instruments
Flight Instruments
Selecting the Altimeter Barometric Pressure Setting
EIS
Turn the BARO Knob to select the desired setting.
Nav/Com/
XPDR/Audio
Selecting Standard Barometric Pressure
1) Press the PFD Softkey.
AFCS
2) Press the STD BARO Softkey to set standard barometric pressure.
Change Altimeter Barometric Pressure Setting Units
GPS Nav
1) Press the PFD Softkey to display the second-level softkeys.
2) Press the ALT UNIT Softkey.
Flight
Planning
3) Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Procedures
Or:
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Hazard
Avoidance
4) Press the BACK Softkey to return to the top-level softkeys.
Change Navigation Sources
Abnormal
Operation
Annun/
Alerts
2) 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.
Additional
Features
1) 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.
3) Press the CDI Softkey a third time to return to GPS.
Appendix
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
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.
Generic Timer
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Instruments
GPS Nav
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.
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.
Configure Vspeed Bugs
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
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
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.
Abnormal
Operation
speed has been changed from a default value, an asterisk appears next to
the speed).
Annun/
Alerts
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.
Index
Appendix
6) To remove the window, press the CLR Key or the TMR/REF Softkey.
2
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Flight Instruments
Flight
Instruments
Set Barometric Minimum Descent Altitude
1) Press the TMR/REF Softkey.
EIS
2) Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘Minimums’.
Nav/Com/
XPDR/Audio
3) Turn the small FMS Knob clockwise to BARO.
4) Press the ENT Key.
5) Use the small FMS Knob to enter the desired altitude.
AFCS
6) Press the ENT Key.
7) To remove the window, press the CLR Key or the TMR/REF Softkey.
GPS Nav
Displaying Wind Data
1) Press the PFD Softkey.
Flight
Planning
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.
Procedures
4) To remove the Wind Data Window, press the OFF Softkey.
Changing HSI Format
Hazard
Avoidance
1) Press the PFD Softkey.
2) Press the HSI FRMT Softkey.
Additional
Features
3) Press the 360 HSI Softkey to display the full size HSI.
Or:
Press the ARC HSI Softkey to display the arc style HSI.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
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
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4
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Engine Indication System
Flight
Instruments
Engine Indication System
Engine Display
EIS
Nav/Com/
XPDR/Audio
Manifold Pressure
Indicator
AFCS
Tachometer
GPS Nav
Flight
Planning
Fuel Flow
Indicator
Procedures
Cylinder Head
Temperature
Indicator
Hazard
Avoidance
Oil Temperature
Indicator
Oil Pressure
Indicator
Additional
Features
Ammeter
Abnormal
Operation
Voltmeter
Annun/
Alerts
Fuel Quantity
Indicator
ENGINE Display
Appendix
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
5
System Display
Pressing the ENGINE Softkey displays the SYSTEM and LEAN softkeys. Press the
SYSTEM Softkey to show the System Display.
Fuel used (GAL USED), endurance (ENDUR), and range (RANGE NM) are all
calculated based on the last manual adjustment of the fuel remaining (GAL REM).
Measured fuel quantity has no effect on fuel calculations. Fuel calculations are
based on sensed fuel flow and the last manual adjustment of the fuel remaining.
- DEC FUEL – Allows the pilot to decrease the gallons of fuel remaining (GAL
REM) in 1-gallon increments
- INC FUEL – Allows the pilot to increase the gallons of fuel remaining in
1-gallon increments
- RST FUEL – Resets the fuel remaining to 76.4 gallons with auxilliary fuel
tanks.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
6
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Engine Indication System
Flight
Instruments
Manifold Pressure
Indicator
EIS
Tachometer
Nav/Com/
XPDR/Audio
AFCS
Voltmeter
Ammeter
GPS Nav
Flight Timer
Oil Temperature
Indicator
Flight
Planning
Oil Pressure
Indicator
Fuel Quantity
Procedures
Fuel Flow
Fuel Remaining
Fuel Range
Hazard
Avoidance
Fuel Used
Fuel Endurance
Additional
Features
Deice Fluid
Quantity
Abnormal
Operation
SYSTEM Display
Annun/
Alerts
Appendix
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
7
Lean Display
Pressing the ENGINE Softkey displays the SYSTEM and LEAN softkeys. Press the
LEAN Softkey to show the Lean Display.
Pressing the CYL SLCT Softkey selects the desired cylinder’s EGT to be shown in
the digital display. The selected cylinder is also highlighted as a light blue bar graph.
To lean each engine, press the ASSIST Softkey. Lean the fuel mixture for the desired
engine until the first cylinder peaks, indicated by the cylinder bar graph displayed as
light blue and a light blue box being displayed above the bar. Enrich the mixture until
the ∆PEAK displays the desired value. This process is performed for each engine.
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
GPS Nav
Manifold Pressure
Indicator
Hazard
Avoidance
Procedures
Flight
Planning
Tachometer
Fuel Flow
Indicator
Peak Temperature
Indicator
Abnormal
Operation
Additional
Features
Exhaust Gas
Temperature
Bar Graph
Annun/
Alerts
Exhaust Gas
Temperature
Digital Display
Peak Temperature
Difference
Appendix
Cylinder Head
Temperature
Bar Graph
Index
Cylinder Head
Temperature
Digital Display
LEAN Display
8
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
Nav/Com/Transponder/Audio Panel
Enter or Change Flight ID
EIS
1) Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.
Nav/Com/
XPDR/Audio
2) Turn the small FMS Knob to enter the first character.
3) Turn the large FMS Knob to select the next field.
AFCS
4) Turn the small FMS Knob to enter the next desired character.
5) Repeat steps 3 and 4 until the desired Flight ID is entered.
GPS Nav
6) Press the ENT Key to update the Flight ID.
Enter a Transponder Code
Additional
Features
ADF Tuning (Optional)
Hazard
Avoidance
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.
Procedures
2) Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
Flight
Planning
1) Press the XPDR Softkey to display the transponder mode selection softkeys.
1) Press the ADF/DME Softkey.
Abnormal
Operation
2) Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
3) Turn the large FMS Knob to select the next desired field.
Annun/
Alerts
4) Turn the small FMS Knob to enter the desired number.
5) Repeat steps 3 and 4 until the desired ADF frequency is entered.
Appendix
6) Press the ENT Key to accept the new frequency.
7) Press the ENT Key again to transfer the frequency to the active field.
8) Turn the large FMS Knob to select the MODE field.
Index
9) Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
10) Press the ENT Key to complete the selection.
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
9
Flight
Instruments
Nav/Com/XPDR/Audio Panel
DME Tuning (Optional)
1) Press the ADF/DME or DME Softkey.
3) Turn the small FMS Knob to select the desired Nav radio.
4) Press the ENT Key to complete the selection.
Selecting a COM Radio
Transmit/Receive
AFCS
Nav/Com/
XPDR/Audio
EIS
2) Turn the large FMS to select the DME source field.
GPS Nav
Receive Only
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).
Hazard
Avoidance
Procedures
Flight
Planning
2) Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
NAV/COM Tuning
Abnormal
Operation
Additional
Features
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
1) Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.
Appendix
Annun/
Alerts
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.
Index
3) Press the Frequency Transfer Key to place the frequency into the active
frequency field.
10
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 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 the PLAY Key once plays the latest recorded memory block, then returns
to normal operation.
• Pressing the MKR/MUTE Key while playing a memory block stops play.
• Pressing the PLAY Key during play begins playing the previously recorded
memory block. Each subsequent press of the PLAY Key begins playing the next
previously recorded block.
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
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
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 DA42-L360
190-01062-01 Rev. A
AFCS
Flight
Instruments
GFC 700 Automatic Flight Control System
(Optional)
Note: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
Nav/Com/
XPDR/Audio
Note: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
EIS
AFCS
Flight Director Activation
Flight
Planning
Control Pressed
Modes Selected
HDG Key
Heading Select
HDG
Pitch Hold (default)
Glidepath
Glideslope
Pitch Hold (default)
PIT
GP
GS
PIT
Appendix
GPS
VAPP
LOC
Annun/
Alerts
Approach**
PIT
Abnormal
Operation
APR Key
Pitch Hold (default)
Additional
Features
Navigation**
Hazard
Avoidance
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
GA
Altitude Hold
ALT
Vertical Speed
VS
Vertical Path Tracking* VPTH
Procedures
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
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
13
Index
**The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before
NAV or APR Key press activates flight director.
190-01062-01 Rev. A
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.
Vertical Modes
Vertical Mode
Pitch Hold
Selected Altitude
Armed
Altitude Hold
Vertical Speed
Flight Level Change
VNAV
(GDU 1044 only)
VNAV Target Altitude
Armed (GDU 1044
only)
Glidepath (SBAS only)
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 SBAS
glidepath on approach
Captures and tracks the ILS
glideslope on approach
Disengages the autopilot and
commands a constant pitch attitude
and wings level in the air
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
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
AFCS
14
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 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
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
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 DA42-L360
190-01062-01 Rev. A
GPS Navigation
Flight
Instruments
GPS Navigation
Direct-to Navigation
EIS
Direct-to Navigation from the MFD
2)
3)
6)
9)
12)
1) Press the Direct-to Key (
2)
5)
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
17
Index
6)
Appendix
4)
Annun/
Alerts
3)
).
Turn the large FMS Knob to place the cursor in the desired selection field.
Turn the small FMS Knob to begin selecting the desired identifier, location,
etc.
Press the ENT Key.
The cursor is now flashing on ‘ACTIVATE?’. If no altitude constraint or
course is desired, press the ENT Key to activate. To enter an altitude
constraint, proceed to step 6.
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
Abnormal
Operation
Direct-to Navigation from the PFD
Additional
Features
11)
Hazard
Avoidance
10)
Procedures
8)
Flight
Planning
7)
GPS Nav
5)
AFCS
4)
) Key.
Enter the waypoint identifier.
Press the ENT Key to confirm the identifier. The ‘Activate?’ field is
highlighted.
If no altitude constraint or course is desired, press the ENT Key to activate.
To enter an altitude constraint, proceed to step 5.
Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field.
Enter the desired altitude.
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 9.
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Press the ENT Key. The cursor is now flashing in the VNV offset distance
field.
Enter the desired offset distance before (-) the waypoint.
Press the ENT Key. The ‘Activate?’ field is highlighted.
Press the ENT Key to activate.
Nav/Com/
XPDR/Audio
1) Press the Direct-to (
GPS Navigation
Flight
Instruments
7) Turn the small FMS Knob to enter the desired altitude.
EIS
8) Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Nav/Com/
XPDR/Audio
10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ field.
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
AFCS
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
15) Press the ENT again to activate the Direct-to.
Activate a Stored Flight Plan
1) Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
Procedures
Flight
Planning
GPS Nav
13) Turn the small FMS Knob to enter the desired course to the waypoint.
2) Press the FMS Knob to activate the cursor.
Hazard
Avoidance
3) Turn the large FMS Knob to highlight the desired flight plan
4) Press the ACTIVE Softkey. The confirmation window is now displayed.
Activate a Flight Plan Leg
1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
Annun/
Alerts
Abnormal
Operation
Additional
Features
5) With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
Index
Appendix
2) On the MFD, press the ACT LEG Softkey.
or
Press the MENU Key, select the ‘Activate Leg’ option from the page menu
and press the ENT Key. This step must be used when activating a leg from
the PFD.
3) With ‘Activate’ highlighted, press the ENT Key.
18
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
GPS Navigation
Flight
Instruments
Stop Navigating a Flight Plan
1) Press the FPL Key to display the Active Flight Plan Page.
2) Press the MENU Key to display the Page Menu Window.
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
Vertical Navigation (VNAV)
EIS
3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This does not delete the stored flight plan, only the active flight plan.
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
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
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 DA42-L360
Light Blue
Subdued Text
190-01062-01 Rev. A
Flight Planning
Flight
Instruments
Flight Planning
Trip Planning
EIS
1) Turn the large FMS Knob to select the ‘AUX’ page group.
3) The current ‘page mode’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL
Softkey.
AFCS
4) For Direct-to planning:
GPS Nav
a) Press the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
Flight
Planning
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
For point-to-point planning:
Hazard
Avoidance
Or:
Procedures
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
a) Enter the identifier of the starting waypoint.
Additional
Features
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
Abnormal
Operation
c) Again, enter the identifier of the ending waypoint.
d) Press the ENT Key to accept the waypoint.
Or:
For flight plan leg planning:
Annun/
Alerts
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 DA42-L360
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.
190-01062-01 Rev. A
Nav/Com/
XPDR/Audio
2) Turn the small FMS Knob to select the first rectangular page icon.
Flight Planning
EIS
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.
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.
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.
GPS Nav
6) Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
Flight
Planning
7) The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
Procedures
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.
Additional
Features
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
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.
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 DA42-L360
190-01062-01 Rev. A
Flight Planning
Flight
Instruments
Create a New User Waypoint
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.
EIS
3) Press the NEW Softkey. A waypoint is created at the current aircraft
position.
Nav/Com/
XPDR/Audio
4) Enter the desired waypoint name.
5) Press the ENT Key.
GPS Nav
a) Turn the small FMS Knob to the left to display a list of flight plan
waypoints. This list is populated only when there is an active flight
plan.
Flight
Planning
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
Or:
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Additional
Features
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Or:
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Annun/
Alerts
b) Turn the small FMS Knob to the right to display the ‘RECENT’
waypoints.
Appendix
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Index
7) After pressing the ENT Key, the cursor is displayed in the ‘RAD’ (radial)
field. Enter the desired radial from the reference waypoint.
8) Press the ENT Key.
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Abnormal
Operation
Hazard
Avoidance
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Procedures
AFCS
6) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the
waypoint can be defined by a reference waypoint. Use one of the following
methods to enter the reference waypoint:
23
Flight Planning
Flight
Instruments
9) The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Nav/Com/
XPDR/Audio
EIS
10) Press the ENT Key. The cursor is now placed for entering another reference
waypoint, if desired.
11) Press the FMS Knob to remove the flashing cursor.
Delete a User Waypoint
1) Turn the large FMS Knob to select the ‘WPT’ page group.
AFCS
2) Turn the small FMS Knob to select the User WPT Information Page.
3) Press the FMS Knob to activate the cursor.
GPS Nav
4) Turn the large FMS Knob to the place the cursor in the ‘USER WAYPOINT LIST’
field.
5) Turn the small FMS Knob to highlight the desired waypoint.
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
Hazard
Avoidance
Procedures
Flight
Planning
6) Press the DELETE Softkey.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
24
NOTE: When creating a new flight plan in the Active Flight Plan Window,
the first leg is activated automatically after it is created.
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.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Flight Planning
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
1) Press the FPL Key to display the active flight plan.
4) Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
Additional
Features
3) Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
Hazard
Avoidance
2) If necessary, press the FMS Knob to activate the cursor.
Abnormal
Operation
5) Enter the new flight plan waypoint by one of the following:
a) Enter the user waypoint identifier, facility, or city.
Annun/
Alerts
b) Press the ENT Key.
Or:
Index
b) Turn the small FMS Knob to the right to display the ‘NRST’ airports to
the aircraft’s current position.
Appendix
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
EIS
Insert a Waypoint in the Active Flight Plan
190-01062-01 Rev. A
Flight
Instruments
Creating a stored flight plan:
1) Press the FPL Key.
2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page.
3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New
Flight Plan’, and press the ENT Key to display a blank flight plan for the
first empty storage location.
4) Turn the small FMS Knob to display the Waypoint Information Window.
(Turning it clockwise displays a blank Waypoint Information Window,
turning it counter-clockwise displays the Waypoint Information Window
with a waypoint selection submenu allowing selection of active flight plan,
nearest, recent, user, or airway waypoints).
5) Enter the identifier, facility, or city name of the departure waypoint or select
a waypoint from the submenu of waypoints and press the ENT Key.
6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint.
7) When all waypoints have been entered, press the FMS Knob to return to
the Flight Plan Catalog Page. The new flight plan is now in the list.
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 ‘RECENT’
waypoints.
d) Press the ENT Key.
e) Press the ENT Key again to “accept” the waypoint.
Enter an Airway in a Flight Plan
1) Press the FPL Key.
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
c) Turn the large FMS Knob to select the desired waypoint.
2) Press the FMS Knob to activate the cursor (not required on the PFD).
Flight
Planning
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.
Hazard
Avoidance
Procedures
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).
Additional
Features
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.
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.
Appendix
Annun/
Alerts
Abnormal
Operation
6) Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
2) Press the MENU Key to display the Page Menu.
Index
3) Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
26
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Flight Planning
Flight
Instruments
4) Press the ENT Key. The original flight plan remains intact in its flight plan
catalog storage location.
5) With ‘OK’ highlighted, press the ENT Key to invert the flight plan.
Or, for a stored flight plan:
AFCS
a) Press the FPL Key on the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
GPS Nav
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
3) Press the CLR Key to display a confirmation window.
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.
Annun/
Alerts
Edit a Stored Flight Plan
2) Press the FMS Knob to activate the cursor.
Index
3) Turn the large FMS Knob to highlight the desired flight plan.
Appendix
1) Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
4) Press the EDIT Softkey.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Abnormal
Operation
1) After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
Additional
Features
Store a Flight Plan
Hazard
Avoidance
4) With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
Procedures
2) Turn the large FMS Knob to highlight the title for the approach, departure,
arrival, or airway to be deleted. Titles appear in white directly above the
procedure’s waypoints.
Flight
Planning
d) Press the EDIT Softkey.
190-01062-01 Rev. A
Nav/Com/
XPDR/Audio
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
EIS
Remove a Departure, Arrival, Approach, or Airway from a Flight
Plan
27
Flight Planning
6) Enter the changes, then press the ENT Key.
7) Press the FMS Knob to return to the Flight Plan Catalog Page.
Delete a Waypoint from the Flight Plan
1) Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
5) Turn the large FMS Knob to place the cursor in the desired location.
Or, for a stored flight plan:
AFCS
a) Press the FPL Key on the MFD and turn the small FMS Knob to select
the Flight Plan Catalog Page.
GPS Nav
b) Press the FMS Knob to activate the cursor.
c) Turn the large FMS Knob to highlight the desired flight plan.
Flight
Planning
d) Press the EDIT Softkey.
2) Turn the large FMS Knob to highlight the waypoint to be deleted.
Procedures
3) Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
5) Once all changes have been made, press the FMS Knob to remove the
cursor.
Invert and Activate a Stored Flight Plan
1) Press the FPL Key on the MFD.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
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.
2) Turn the small FMS Knob to select the Flight Plan Catalog Page.
Annun/
Alerts
3) Press the FMS Knob to activate the cursor.
4) Turn the large FMS Knob to highlight the desired flight plan.
Appendix
5) Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
Index
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.
28
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Flight Planning
Flight
Instruments
Copy a Flight Plan
1) Press the FPL Key on the MFD.
2) Turn the small FMS Knob to select the Flight Plan Catalog Page.
EIS
3) Press the FMS Knob to activate the cursor.
5) Press the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
Nav/Com/
XPDR/Audio
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.
AFCS
4) Turn the large FMS Knob to highlight the flight plan to be copied.
GPS Nav
Delete a Flight Plan
1) Press the FPL Key on the MFD.
Flight
Planning
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.
Additional
Features
Graphical Flight Plan Creation
1) Press the FPL Key to display the Active Flight Plan Page on the MFD.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
29
Index
5) To change the user waypoint name, follow the procedure for modifying a user
waypoint.
Appendix
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.
Annun/
Alerts
3) The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
Abnormal
Operation
2) Press the Joystick to activate the map pointer. Use the Joystick to move
the pointer to the desired point on the map to be inserted as a waypoint in
the flight plan.
190-01062-01 Rev. A
Hazard
Avoidance
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.
Procedures
5) Press the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
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
30
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Procedures
Flight
Instruments
Procedures
Load and Activate a Departure Procedure
EIS
1) Press the PROC Key.
3) Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
5) Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.
Flight
Planning
7) Turn the large FMS Knob to highlight the desired transition.
GPS Nav
6) Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
AFCS
4) Turn the large FMS Knob to highlight the desired departure.
Nav/Com/
XPDR/Audio
2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
8) Press the ENT Key.
Hazard
Avoidance
Activate A Departure Leg
Procedures
9) With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
1) Press the FPL Key on the MFD to display the active flight plan.
Additional
Features
2) Press the FMS Knob to activate the cursor.
3) Turn the large FMS Knob to highlight the desired waypoint within the
departure.
Abnormal
Operation
4) Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5) With ‘ACTIVATE’ highlighted, press the ENT Key.
Annun/
Alerts
Load An Arrival Procedure
Appendix
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
31
Index
3) Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
Procedures
Flight
Instruments
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.
EIS
7) Press the ENT Key. A list of runways may be displayed for the selected
arrival.
Nav/Com/
XPDR/Audio
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.
Hazard
Avoidance
Procedures
Flight
Planning
b) Turn the large FMS Knob to highlight the desired waypoint altitude.
2) Press the FMS Knob to activate the cursor.
Additional
Features
3) Turn the large FMS Knob to highlight the desired waypoint within the
arrival.
5) With ‘ACTIVATE’ highlighted, press the ENT Key.
Load and/or Activate an Approach Procedure
Index
Appendix
Annun/
Alerts
Abnormal
Operation
4) Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
32
NOTE: Check the Aircraft Flight Manual (AFM) to determine if SBAS
functionality is approved.
NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some
published approach procedures for the desired airport may not be displayed
in the list of available approaches.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Procedures
2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
4) Turn either FMS Knob to highlight the desired approach.
AFCS
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.
GPS Nav
7) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
9) Press the ENT Key.
Procedures
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 is immediately
activated.
Flight
Planning
8) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Nav/Com/
XPDR/Audio
5) Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
EIS
3) Press the ENT Key. A list of available approaches for the destination airport
is displayed.
Flight
Instruments
1) Press the PROC Key.
Hazard
Avoidance
Activate An Approach in the Active Flight Plan
Additional
Features
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
Abnormal
Operation
3) Press the ENT Key.
Activate a Vector to Final Approach Fix
Annun/
Alerts
1) Press the PROC Key.
2) Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
Appendix
3) Press the ENT Key.
4) The final approach course becomes the active leg.
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
33
Flight
Instruments
Procedures
Activate A Missed Approach in the Active Flight Plan
1) Press the PROC Key.
EIS
2) Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3) Press the ENT Key. A confirmation window is displayed.
Or:
Press the go-around button:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
4) With ‘ACTIVATE’ highlighted, press the ENT Key.
34
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Hazard Avoidance
Flight
Instruments
Hazard Avoidance
Customizing the Hazard Displays on the Navigation Map
EIS
1) With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
GPS Nav
STORMSCOPE® (Optional)
Flight
Planning
WARNING: The Stormscope system is not intended to be used for hazardous
thunderstorm penetration. Weather information on the G1000 MFD is
approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for
detailed operation.
Procedures
Displaying Stormscope Lightning Data on the Navigation Map Page
2) Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove
Stormscope Lightning Data from the Navigation Map Page.
Hazard
Avoidance
1) Press the MAP Softkey.
Additional
Features
Lightning Age
Strike is less than 6 seconds old
AFCS
3) Press the small FMS Knob to return to the Navigation Map Page.
Nav/Com/
XPDR/Audio
2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.
Symbol
Abnormal
Operation
Strike is between 6 and 60 seconds old
Annun/
Alerts
Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
1) Press the MENU Key (with the Navigation Map Page displayed).
2) Turn either FMS Knob to highlight ‘Map Setup’.
Index
3) Press the ENT Key.
4) Turn the small FMS Knob to highlight ‘Weather’.
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
35
Hazard Avoidance
Flight
Instruments
5) Press the ENT Key.
6) Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field.
7) Turn the small FMS Knob to display the ‘Cell/Strike’ window.
EIS
8) Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
Nav/Com/
XPDR/Audio
9) Push the FMS Knob to return to the Navigation Map Page.
Clear Stormscope Lightning Data from the Navigation Map Page
1) Press the MENU Key (with the Navigation Map Page displayed).
AFCS
2) Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field
and press the ENT Key.
GPS Nav
NOTE: If heading input is lost, strikes and/or cells must be cleared manually
after the execution of each turn. This is to ensure that the strike and/or cell
Flight
Planning
positions are depicted accurately in relation to the nose of the aircraft.
Stormscope Page
Procedures
1) Turn the large FMS Knob until the Map Page group is selected.
2) Turn the small FMS Knob until the Stormscope Page is selected.
Hazard
Avoidance
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
1) Select the Stormscope Page.
Abnormal
Operation
Additional
Features
2) Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed.
Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey
to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box
located in the upper left corner of the Stormscope Page.
Annun/
Alerts
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Change the Viewing Mode Between 360˚ and 120˚
Appendix
1) Select the Stormscope Page.
2) Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press
the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to
display a 120˚ viewing area.
Index
36
Press the CLEAR Softkey to remove all Stormscope lightning data from the
display.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Hazard Avoidance
Nav/Com/
XPDR/Audio
Displaying XM Weather on the Navigation Map Page
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)
1) Press the MAP Softkey.
AFCS
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.
GPS Nav
Display METAR and TAF information on the Airport Information Page
1) Turn the large FMS Knob to select the WPT Page Group.
2) Turn the small FMS Knob to select the Airport Information Page.
Flight
Planning
3) Press the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
Procedures
Displaying Weather on the Weather Data Link Page
1) Turn the large FMS Knob to select the Map Page Group.
Hazard
Avoidance
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.
Abnormal
Operation
Map Panning Information – Weather Data Link Page
Additional
Features
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.
1) Push in the Joystick to display the panning arrow.
Annun/
Alerts
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.
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 DA42-L360
Index
190-01062-01 Rev. A
Appendix
37
Hazard Avoidance
Flight
Instruments
Weather Products and Symbols
Echo Top (Cloud Top and Echo Top Mutually Exclusive)
Nav/Com/
XPDR/Audio
EIS
Cell Movement
NEXRAD
XM Lightning
METARs
County Warnings
Surface Analysis
Winds Aloft
SIGMETs/AIRMETs
AFCS
Cloud Top
Cyclone Warnings
City Forecast Freezing Levels
GPS Nav
Traffic Systems
Flight
Planning
• 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.
Procedures
Traffic Symbol
Description
Non-Threat Traffic
(intruder is beyond 5 nm and greater than 1200’ vertical separation)
Hazard
Avoidance
Proximity Advisory (PA)(not available with TIS)
(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
Annun/
Alerts
Traffic Symbol Description
Index
Appendix
Traffic Information Service (TIS)
38
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Hazard Avoidance
Flight
Instruments
Displaying Traffic on the Traffic Map Page
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Traffic Map Page.
EIS
3) Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
Nav/Com/
XPDR/Audio
4) Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
AFCS
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
Displaying Traffic on the Navigation Map
Flight
Planning
1) 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.
Procedures
Traffic Advisory System (TAS) (Optional)
Hazard
Avoidance
Displaying Traffic on the Traffic Map Page
1) Turn the large FMS Knob to select the Map Page Group.
Additional
Features
2) Turn the small FMS Knob to select the Traffic Map Page. ‘OPERATING’ is
displayed in the Traffic Mode field.
Abnormal
Operation
3) Press 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.
Annun/
Alerts
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
5) Press the MUTE Softkey to mute TAS voice alerts.
Appendix
Displaying Traffic on the Navigation Map
1) Ensure TAS is operating.
Index
2) With the Navigation Map displayed, press the MAP Softkey.
3) Press the TRAFFIC Softkey. Traffic is now displayed on the map.
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
39
ADS-B Traffic (Optional)
ADS-B is limited to displaying traffic in the G1000. Operation is similar to the
TAS system discussed previously, with the exception of symbology. In addition to the
traffic symbols previously discussed, the following traffic symbols are used to display
traffic with the ADS-B system.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
Symbol
Description
AFCS
Traffic Advisory with directional information. Points in the direction of the
intruder aircraft track.
Non-threat traffic with directional information. Points in the direction of the
aircraft track.
GPS Nav
Other traffic with directional information. Points in the direction of the intruder
aircraft track.
Flight
Planning
Traffic with directional information, but positional accuracy is degraded. Points
in the direction of the aircraft track.
Procedures
Traffic located on the ground with directional information. Points in the
direction of the aircraft track. Ground traffic is only displayed when own
aircraft is below 1,000 feet AGL or on the ground.
Hazard
Avoidance
Ground traffic without directional information. Ground traffic is only displayed
when own aircraft is below 1,000 feet AGL or on the ground.
Additional
Features
Non-aircraft ground traffic. Ground traffic is only displayed when own aircraft
is below 1,000 feet AGL or on the ground.
Annun/
Alerts
Abnormal
Operation
Aircraft
Identification
(tail number
or Flight ID
number)
Index
Appendix
Intruder
Aircraft
Ground Track
(extends in
the direction
of the aircraft
movement)
Relative Altitude
(in this case 1200
feet above own
aircraft)
Altitude Trend
(up arrow
indicates
climbing, down
arrow indicates
descending)
Example ADS-B Traffic Advisory
40
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Hazard Avoidance
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Flight
Instruments
Terrain And Obstacle Proximity
EIS
Displaying Terrain and Obstacles on the Terrain Proximity Page
Nav/Com/
XPDR/Audio
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the last rectangular page icon.
GPS Nav
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Hazard
Avoidance
Red
Procedures
Terrain/Obstacle Location
Flight
Planning
Color
Additional
Features
Displaying Terrain and Obstacles on the Navigation Map
1) With the Navigation Map displayed, press the MAP Softkey.
Abnormal
Operation
2) Press the TERRAIN Softkey. Terrain and obstacle proximity will now be
displayed on the map.
Annun/
Alerts
Terrain-SVS
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
41
Index
NOTE: Terrain-SVS is only available when the Synthetic Vision System (SVS)
option is installed.
Appendix
190-01062-01 Rev. A
AFCS
3) If desired, press the VIEW Softkey to access the ARC and 360 Softkeys.
When the ARC Softkey is pressed, a radar-like 120° view is displayed. Press
the 360 Softkey to return to the 360° default display.
Hazard Avoidance
Flight
Instruments
Display Terrain on the TERRAIN-SVS Page
1) Turn the large FMS Knob to select the Map Page Group.
2) Turn the small FMS Knob to select the Terrain-SVS Page.
Nav/Com/
XPDR/Audio
EIS
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.
Color
Terrain/Obstacle Location
Red
Terrain/Obstacle above or within 100’
below current aircraft altitude.
Yellow
Terrain/Obstacle between 100’ and
1000’ below current aircraft altitude.
Black
Terrain/Obstacle is more than 1000’
below aircraft altitude.
Procedures
Flight
Planning
GPS Nav
AFCS
4) Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Enable/Disable Aviation Data
Hazard
Avoidance
1) While the Terrain-SVS Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
Additional
Features
3) Press the ENT Key.
Terrain-SVS Inhibit
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Inhibit Terrain
While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.
Or:
1) Press the MENU Key.
2) Turn the small FMS Knob to select ‘Inhibit Terrain’.
3) Press the ENT Key.
42
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Hazard Avoidance
EIS
Nav/Com/
XPDR/Audio
GPS Nav
NOTE: If Terrain-SVS alerts are inhibited when the Final Approach Fix is the
active waypoint in a GPS SBAS approach, a LOW ALT annunciation may appear
on the PFD next to the altimeter if the current aircraft altitude is at least 164
feet below the prescribed altitude at the Final Approach Fix.
AFCS
Flight
Instruments
Enable Terrain
While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.
Or:
1) While the Terrain-SVS Page is displayed, press the MENU Key.
2) Turn the small FMS Knob to select ‘Enable Terrain’.
3) Press the ENT Key.
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
43
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
44
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Additional Features
Flight
Instruments
Additional Features
Synthetic Vision (Optional)
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
Index
3) Press the SYN TERR Softkey.
4) Press the BACK Softkey to return to the previous page.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Procedures
Displaying SVS Terrain
190-01062-01 Rev. A
Flight
Planning
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
GPS Nav
•
•
•
•
•
•
•
AFCS
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:
Nav/Com/
XPDR/Audio
WARNING: Do not use SVS runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
EIS
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVS is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles,
or traffic.
45
Additional Features
Flight
Instruments
Displaying Pathways
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
EIS
3) If not already enabled, press the SYN TERR Softkey.
Nav/Com/
XPDR/Audio
4) Press the PATHWAY Softkey.
5) Press the BACK Softkey to return to the previous page.
Displaying Heading on the Horizon
AFCS
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
GPS Nav
3) If not already enabled, press the SYN TERR Softkey.
4) Press the HRZN HDG Softkey.
Flight
Planning
5) Press the BACK Softkey to return to the previous page.
Displaying Airport Signs
Procedures
1) Press the PFD Softkey.
2) Press the SYN VIS Softkey.
3) If not already enabled, press the SYN TERR Softkey.
5) Press the BACK Softkey to return to the previous page.
Terminal Procedure Charts
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
4) Press the APTSIGNS Softkey.
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
46
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Additional Features
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
the DCLTR Softkey a third time removes the airport runway layout, unless the airport
in view is part of an active route structure. 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.
ChartView
Hazard
Avoidance
Additional
Features
Abnormal
Operation
1) Press the SHW CHRT Softkey when displayed.
Procedures
View Charts from the Navigation Map Page
Flight
Planning
FliteCharts® resemble the paper version of AeroNav Services terminal procedures
charts. The charts are displayed with high-resolution and in color for applicable
charts. Current aircraft position is not displayed on FliteCharts.
The FliteCharts database contains procedure charts for the United States only.
This database is updated on a 28-day cycle. If not updated within 180 days of the
expiration date, FliteCharts will no longer function.
GPS Nav
FliteCharts®
AFCS
ChartView resembles the paper version of Jeppesen terminal procedures charts.
The charts are displayed in full color with high-resolution. The MFD depiction shows
the aircraft position on the moving map in the plan view of most approach charts and
on airport diagrams.
The ChartView database is updated on a 14-day cycle. If the ChartView database
is not updated within 70 days of the expiration date, ChartView will no longer
function.
Or:
Move the map pointer to point to a desired point on the map and press the
SHW CHRT Softkey.
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Index
3) Press the GO BACK Softkey to return to the previous page.
Appendix
2) Select the DP, STAR, APR, WX, and NOTAM softkeys to access charts for
departures, arrivals, approaches, weather and NOTAMs Note that NOTAMS
are only available with ChartView.
Annun/
Alerts
47
Additional Features
Flight
Instruments
View Charts from the Active Flight Plan Page
1) While viewing the Active Flight Plan Page, press the FMS Knob to activate
the cursor.
EIS
2) Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
Nav/Com/
XPDR/Audio
3) 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.
AFCS
Change Day/Night View
GPS Nav
1) While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
Flight
Planning
2) Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
Procedures
3) Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR
SCHEME’ Options.
4) Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.
Hazard
Avoidance
5) Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
Additional
Features
6) In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.
Abnormal
Operation
XM® Radio Entertainment
Annun/
Alerts
7) Press the FMS Knob when finished to remove the Chart Setup Menu.
The XM® Radio Page provides information and control of the audio entertainment
features of the XM Satellite Radio.
Appendix
Selecting the XM Radio Page
1) Turn the large FMS Knob to select the Auxiliary Page Group.
2) Turn the small FMS Knob to select XM Radio.
Index
3) Select the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
48
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Additional Features
EIS
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.
Flight
Instruments
Active Channel and Channel List
Selecting a Category
Additional
Features
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
Hazard
Avoidance
Or:
Procedures
Flight
Planning
2) Select the CH + Softkey to go down through the list in the Channel Box, or
move up the list with the CH – Softkey.
GPS Nav
1) While on the XM Radio Page, select the CHNL Softkey.
AFCS
Select an Available Channel within the Selected Category
Nav/Com/
XPDR/Audio
The Category Box of the XM Radio Page displays the currently selected category
of audio.
1) Select the CATGRY Softkey on the XM Radio Page.
2) Select the CAT + and CAT - softkeys to cycle through the categories.
Or:
Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.
3) Press the ENT Key.
3) With the desired channel highlighted, press the ENT Key.
Abnormal
Operation
Entering a Channel Directly
1) While on the XM Radio Page, select the CHNL Softkey.
Appendix
3) Select the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
Annun/
Alerts
2) Select the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
4) Press the ENT Key to activate the selected channel.
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
49
Additional Features
Flight
Instruments
Assigning Channel Presets
AFCS
Nav/Com/
XPDR/Audio
EIS
Up to 15 channels from any category can be assigned a preset number.
1) On the XM Radio Page, with the desired channel active, select the
PRESETS Softkey to access the first five preset channels (PS1 - PS5).
2) Select the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Selecting the
MORE Softkey repeatedly cycles through the preset channels.
3) Select the SET Softkey.
4) Select any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
GPS Nav
Adjusting Volume
1) On the XM Radio Page, press the RADIO Softkey.
Flight
Planning
2) Press the VOL Softkey to access the volume control softkeys.
3) Press VOL + or VOL - softkeys to adjust the volume level.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
4) Press the MUTE Softkey to mute the radio audio.
50
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 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
NOTE: The Diamond DA42-L360 Pilot’s Operating Handbook (POH) always
takes precedence over the information found in this section.
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.
Hazard
Avoidance
Hazard Displays with Loss of GPS Position
Procedures
When a COM tuning failure is detected by the system, the emergency frequency
(121.500 MHz) is automatically loaded into the active frequency field of the COM
radio for which the tuning failure was detected.
Flight
Planning
Abnormal COM Operation
GPS Nav
Abnormal
Operation
Annun/
Alerts
Loss of Hazard Functions with Loss of GPS
Position
Appendix
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
51
Unusual Attitudes
The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary
functions are displayed in these situations.
The following information is removed from the PFD (and corresponding softkeys
are disabled) when the aircraft experiences unusual attitudes:
• Traffic Annunciations
• AFCS Annunciations
• Flight director Command Bars
• Inset Map
• Temperatures
• DME Information
Window
• Wind Data
• Selected Heading Box
• Selected Course Box
• Transponder Status
Box
• System Time
• PFD Setup Menu
• Windows displayed in
the lower right corner
of the PFD:
– Timer/References
– Nearest Airports
– Flight Plan
– Messages
– Procedures
– ADF/DME Tuning
• Barometric Minimum
Descent Altitude Box
• Glideslope, Glidepath, and Vertical
Deviation Indicators
• Altimeter Barometric
Setting
• Selected Altitude
• VNV Target Altitude
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
Index
Appendix
Annun/
Alerts
Extreme Pitch Indication
52
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Abnormal Operation
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. Also, the CDI deviation bar is removed from the display. Lastly, but at the same
time, a ‘GPS NAV LOST’ alert message appears on the PFD.
Normal navigation using GPS/SBAS source data resumes automatically once a valid
GPS solution is restored.
It is important to note that estimated navigation data supplied by the G1000 in
DR Mode may become increasingly unreliable and must not be used as a sole means
of navigation. If, while in DR Mode, airspeed and/or heading data is also lost or
not available, the DR function may not be capable of estimating your position and,
consequently, the system may display a path that is different than the actual movement
of the aircraft. Estimated position information displayed by the G1000 through
DR while there is no heading and/or airspeed data available should not be used for
navigation.
DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the
lack of satellite measurements needed to determine a position. Changes in wind speed
and/or wind direction compounds the relative inaccuracy of DR Mode. Because of this
degraded accuracy, the crew must maintain position awareness using other navigation
equipment until GPS-derived position data is restored.
AFCS
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.
Nav/Com/
XPDR/Audio
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
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
53
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
• 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 not couple to GPS, and
both TAWS and Terrain Proximity are disabled. Additionally, the accuracy of all nearest
information (airports, airspaces, and waypoints) is questionable. Finally, airspace
alerts continue to function, but with degraded accuracy.
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
54
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
Flight
Instruments
Annunciations & Alerts
WARNING Annunciation
Alerts Window Message
No Tone
Repeating
Aural Tone
Procedures
Hazard
Avoidance
CAUTION Annunciation
Appendix
Index
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Single
Aural Tone
Annun/
Alerts
Left auxiliary fuel tank is empty.
Right auxiliary fuel tank is empty.
Landing gear is not down and locked.
De-icing fluid level is low.
De-icing pressure is high.
De-icing pressure is low.
Left engine main tank fuel quantity is low.
Right engine main tank fuel quantity is low.
Pitot heat has failed.
Pitot heat is off.
Stall warning heat has failed.
Audio
Alert
Abnormal
Operation
190-01062-01 Rev. A
Alerts Window Message
Additional
Features
Annunciation
Window Text
L AUX FUEL E
R AUX FUEL E
CHECK GEAR
DEICE LVL LO
DEIC PRES HI
DEIC PRES LO
L FUEL LOW
R FUEL LOW
PITOT FAIL
PITOT HT OFF
STAL HT FAIL
Flight
Planning
Autopilot automatic trim is inoperative.
Front, rear, or baggage door is not closed.
Left engine fuel pressure is greater than 35 psi.
Right engine fuel pressure is greater than 35 psi.
Left engine fuel pressure is less than 14 psi.
Right engine fuel pressure is less than 14 psi.
Left engine oil pressure is less than 25 psi bar.
Right engine oil pressure is less than 25 psi bar.
Left engine starter is engaged.
Right engine starter is engaged.
GPS Nav
AP TRIM FAIL
DOOR OPEN
L FUEL PR HI
R FUEL PR HI
L FUEL PR LO
R FUEL PR LO
L OIL PRES
R OIL PRES
L STARTER
R STARTER
AFCS
Left engine alternator has failed.
Right engine alternator has failed.
Nav/Com/
XPDR/Audio
L ALTN FAIL
R ALTN FAIL
Audio
Alert
Repeating
Aural Tone
EIS
Annunciation
Window Text
55
Annunciations & Alerts
Annunciation
Window Text
L FUEL XFER
R FUEL XFER
GPS Nav
Flight
Planning
Procedures
Stall warning heat is off.
Stick limiting system has failed.
Left bus voltage is less than 25 volts.
Right bus voltage is less than 25 volts.
Audio
Alert
Single
Aural Tone
Alerts Window Message
Left fuel transfer from aux to main in progress.
Right fuel transfer from aux to main in progress.
Audio
Alert
No Tone
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.
GIA FAN FAIL – The cooling fan for the GIAs is inoperative.
Audio
Alert
None
Additional
Features
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.
AP and MET are unavailable. FD may still be
available.
Index
Appendix
Condition
Abnormal
Operation
AFCS Alerts
Annun/
Alerts
Hazard
Avoidance
Alerts Window Message
Annunciation Advisory Alerts
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciation
Window Text
STAL HT OFF
STICK LIMIT
L VOLTS LOW
R VOLTS LOW
Annunciation Description
System Failure
Yaw Damper Failure
56
Yaw Damper control failure.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
Annunciation Description
Elevator Mistrim Up
Additional
Features
Aural
Message
Abnormal
Operation
MFD
Pop-Up Alert
“Warning; Terrain,
Terrain”
Imminent Terrain Impact
Warning (ITI)
“Warning; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Warning (ROC)
“Warning; Obstacle,
Obstacle”
Imminent Obstacle Impact
Warning (IOI)
“Warning; Obstacle,
Obstacle”
Index
57
Appendix
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Annun/
Alerts
Reduced Required Terrain
Clearance Warning (RTC)
190-01062-01 Rev. A
Hazard
Avoidance
Alert Type
PFD/MFD
TERRAIN-SVS
Page
Annunciation
Procedures
Terrain-SVS Alerts
Flight
Planning
Preflight Test
GPS Nav
Aileron Mistrim Right
AFCS
Aileron Mistrim Left
Nav/Com/
XPDR/Audio
Elevator Mistrim Down
EIS
A condition has developed causing the pitch
servo to provide a sustained force. Be prepared
to apply nose up control wheel force upon
autopilot disconnect.
A condition has developed causing the pitch
servo to provide a sustained force. Be prepared
to apply nose down control wheel force upon
autopilot disconnect.
A condition has developed causing the roll servo
to provide a sustained left force. Ensure the
slip/skid indicator is centered and observe any
maximum fuel imbalance limits.
A condition has developed causing the roll servo
to provide a sustained right force. Ensure the
slip/skid indicator is centered and observe any
maximum fuel imbalance limits.
Performing preflight system test. Upon
completion, the aural alert will be heard.
Preflight system test has failed.
Flight
Instruments
Condition
Alert Type
Aural
Message
“Caution; Terrain,
Terrain”
Imminent Terrain Impact
Caution (ITI)
“Caution; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Caution (ROC)
“Caution; Obstacle,
Obstacle”
Imminent Obstacle Impact
Caution (IOI)
“Caution; Obstacle,
Obstacle”
Terrain-SVS System Status Annunciations
TERRAIN-SVS Page
Annunciation
Aural Message
TERRAIN TEST
None
None
“Terrain System
Test OK”
Terrain Alerting is disabled
None
None
Terrain System Test Fail
TERRAIN FAIL
“Terrain System
Failure”
Terrain or Obstacle
database unavailable or
invalid, invalid software
configuration, system
audio fault
TERRAIN FAIL
“Terrain System
Failure”
NO GPS POSITION
“Terrain System
Not Available”
None
“Terrain System
Not Available”
None
“Terrain System
Available”
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
MFD
Pop-Up Alert
Alert Type
PFD/MFD Alert
Annunciation
System Test in Progress
System Test Pass
None
No GPS position
Excessively degraded GPS
signal, Out of database
coverage area
Sufficient GPS signal
received after loss
None
Index
Appendix
PFD/MFD
TERRAIN-SVS
Page
Annunciation
Reduced Required Terrain
Clearance Caution (RTC)
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
58
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
Voice Alert
“Minimums, minimums”
GPS Nav
Flight
Planning
MFD & PFD Message Advisories
Additional
Features
Abnormal
Operation
The PFD and/or MFD self-test has detected a
problem. The G1000 system should be serviced.
Annun/
Alerts
The PFD and/or MFD has incorrect software
installed. The G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Index
The PFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.
Appendix
190-01062-01 Rev. A
Hazard
Avoidance
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 PFDs are not communicating
with each other. The G1000 system should be
serviced.
Procedures
XTALK ERROR – A flight display
crosstalk error has occurred.
AFCS
Played when the TAS system fails a pilot-initiated self test.
Message
DATA LOST – Pilot stored data
was lost. Recheck settings.
Nav/Com/
XPDR/Audio
“Traffic”
“Traffic Not Available”
“Traffic, Traffic”
“Traffic Advisory System
Test Passed”
“Traffic Advisory System
Test Failed”
EIS
“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.
The aircraft is outside the Traffic Information Service (TIS) coverage area.
Played when a Traffic Advisory (TA) is issued (TAS system).
Played when the TAS system passes a pilot-initiated self test.
Flight
Instruments
Voice Alerts
59
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
MFD1 CONFIG – MFD1 config
error. Config service req’d.
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
PFD1 COOLING – PFD1 has poor
cooling. Reducing power usage.
MFD1 COOLING – MFD1 has poor
cooling. Reducing power usage.
PFD1 KEYSTK – PFD1 [key name]
Key is stuck.
MFD1 KEYSTK – MFD [key name]
Key is stuck.
CNFG MODULE – PFD1
configuration module is inoperative.
PFD1 VOLTAGE – PFD1 has low
voltage. Reducing power usage
MFD1 VOLTAGE – MFD1 has low
voltage. Reducing power usage
Comments
The MFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.
The MFD and PFDs have different software
versions installed. The G1000 system should be
serviced.
The PFD and/or MFD is overheating and is
reducing power consumption by dimming the
display. If problem persists, the G1000 system
should be serviced.
A key is stuck on the PFD and/or MFD bezel.
Attempt to free the stuck key by pressing it
several times. The G1000 system should be
serviced if the problem persists.
The PFD1 configuration module backup memory
has failed. The G1000 system should be serviced.
The PFD1 voltage is low. The G1000 system
should be serviced.
The MFD voltage is low. The G1000 system
should be serviced.
Database Message Advisories
Message
MFD1 DB ERR – MFD1 aviation
database error exists.
PFD1 DB ERR – PFD1 aviation
database error exists.
MFD1 DB ERR – MFD1 basemap
database error exists.
PFD1 DB ERR – PFD1 basemap
database error exists.
60
Comments
The MFD and/or PFD detected a failure in
the aviation database. Attempt to reload the
aviation database. If problem persists, the
G1000 system should be serviced.
The MFD and/or PFD detected a failure in the
basemap database.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
AFCS
Procedures
The obstacle database is present on another LRU,
but is missing on the specified LRU.
Flight
Planning
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 G1000 system should be serviced.
GPS Nav
Hazard
Avoidance
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 G1000 system should be
serviced.
Additional
Features
Appendix
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 G1000 system should be serviced.
Annun/
Alerts
The airport terrain database is present on
another LRU, but is missing on the specified LRU.
Abnormal
Operation
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.
The terrain database is present on another LRU,
but is missing on the specified LRU.
Nav/Com/
XPDR/Audio
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
MFD1 DB ERR – MFD1 airport
terrain database error exists.
PFD1 DB ERR – PFD1 airport
terrain database error exists.
Comments
The MFD and/or PFD detected a failure in the
terrain database. Ensure that the terrain card is
properly inserted in display. Replace terrain card.
If problem persists, The G1000 system should be
serviced.
EIS
Message
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
Flight
Instruments
Database Message Advisories (Cont.)
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
61
Database Message Advisories (Cont.)
Message
Comments
MFD1 DB ERR – MFD1 Chartview The MFD and/or PFDs detected a failure in the
database error exists.
ChartView database (optional feature). Ensure
that the data card is properly inserted. Replace
data card. If problem persists, The G1000 system
should be serviced.
MFD1 DB ERR – MFD1 FliteCharts The MFD and/or PFDs detected a failure in the
database error exists.
FliteCharts database (optional feature). Ensure
that the data card is properly inserted. Replace
data card. If problem persists, The G1000 system
should be serviced.
DB MISMATCH – Aviation
The PFDs and MFD have different aviation
database version mismatch. Xtalk database versions installed. Crossfill is off.
is off.
Install correct aviation database version in all
displays.
DB MISMATCH – Aviation
The PFDs and MFD have different aviation
database type mismatch. Xtalk is database types installed (Americas, European,
off.
etc.). Crossfill is off. Install correct aviation
database type in all displays.
DB MISMATCH – Terrain database The PFDs and MFD have different terrain
version mismatch.
database versions installed. Install correct terrain
database version in all displays.
DB MISMATCH – Terrain database The PFDs and MFD have different terrain
type mismatch.
database types installed. Install correct terrain
database type in all displays.
DB MISMATCH – Obstacle
The PFDs and MFD have different obstacle
database version mismatch.
database versions installed. Install correct
obstacle database version in all displays.
DB MISMATCH – Airport Terrain
The PFDs and MFD have different airport terrrain
database mismatch.
databases installed. Install correct airport terrain
database in all displays.
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
62
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
Procedures
Hazard
Avoidance
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
Abnormal
Operation
Annun/
Alerts
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Additional
Features
The GIA1 and/or GIA2 have an error in the audio
configuration. The G1000 system should be
serviced.
Appendix
Index
The GIA1 and/or GIA2 temperature is too high.
If problem persists, the G1000 system should be
serviced.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Flight
Planning
190-01062-01 Rev. A
GPS Nav
Comments
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
AFCS
Message
Nav/Com/
XPDR/Audio
GIA 63 Message Advisories
EIS
Message
Comments
GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure.
The audio panel is unavailable. The G1000
system should be serviced.
GMA1 CONFIG – GMA1 config
The audio panel configuration settings do not
error. Config service req’d.
match backup configuration memory. The
G1000 system should be serviced.
The audio panel has incorrect software installed. The
MANIFEST – GMA1 software
G1000 system should be serviced.
mismatch, communication halted.
The audio panel self-test has detected a problem in
GMA1 SERVICE – GMA1 needs
the unit. Certain audio functions may still be availservice. Return unit for repair.
able, and the audio panel may still be usable. The
G1000 system should be serviced when possible.
Flight
Instruments
GMA 1347 Message Advisories
63
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
GIA 63 Message Advisories (Cont.)
Message
Comments
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
MANIFEST – GIA1 software mismatch,
communication halted.
MANIFEST – GIA2 software mismatch,
communication halted.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
COM1 SERVICE – COM1 needs service.
Return unit for repair.
COM2 SERVICE – COM2 needs service.
Return unit for repair.
COM1 PTT – COM1 push-to-talk key is
stuck.
COM2 PTT – COM2 push-to-talk key is
stuck.
COM1 RMT XFR – COM1 remote
transfer key is stuck.
COM2 RMT XFR – COM2 remote
transfer key is stuck.
RAIM UNAVAIL – RAIM is not available
from FAF to MAP waypoints.
The GIA1 and/or GIA2 self-test has detected a
problem in the unit. The G1000 system should
be serviced.
The GIA1 and/or GIA 2 has incorrect software
installed. The G1000 system should be serviced.
The system has detected an over temperature
condition in COM1 and/or COM2. The transmitter
is operating at reduced power. If the problem
persists, the G1000 system should be serviced.
The system has detected a failure in COM1 and/
or COM2. COM1 and/or COM2 may still be usable. The G1000 system should be serviced when
possible.
The COM1 and/or COM2 external push-to-talk
switch is stuck in the enable (or “pressed”) position.
Press the PTT switch again to cycle its operation.
If the problem persists, the G1000 system should be
serviced.
The COM1 and/or COM2 transfer switch is stuck
in the enabled (or “pressed”) position. Press the
transfer switch again to cycle its operation. If the
problem persists, the G1000 system should be
serviced.
GPS satellite coverage is insufficient to perform
Receiver Autonomous Integrity Monitoring
(RAIM) from the FAF to the MAP waypoints.
LOI – GPS integrity lost. Crosscheck with GPS integrity is insufficient for the current
other NAVS.
phase of flight.
Loss of GPS navigation due to insufficient
GPS NAV LOST – Loss of GPS
satellites.
navigation. Insufficient satellites.
64
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
Displayed after passing the first waypoint of
a true north approach when the nav angle is
set to ‘AUTO’.
A failure has been detected in the GPS1 and/or
GPS2 receiver. The receiver is unavailable. The
G1000 system should be serviced.
Flight
Planning
A failure has been detected in the GPS1
and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be
serviced.
Procedures
A failure has been detected in the NAV1
and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be
serviced.
Hazard
Avoidance
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
65
Index
A failure has been detected in glideslope receiver
1 and/or receiver 2. The receiver may still be
available. The G1000 system should be serviced
when possible.
Appendix
G/S1 SERVICE – G/S1 needs service.
Return unit for repair.
G/S2 SERVICE – G/S2 needs service.
Return unit for repair.
Annun/
Alerts
G/S2 FAIL – G/S2 is inoperative.
A failure has been detected in glideslope receiver
1 and/or receiver 2. The G1000 system should be
serviced.
Abnormal
Operation
The remote NAV1 and/or NAV2 transfer
switch is stuck in the enabled (or “pressed”)
state. Press the transfer switch again to cycle
its operation. If the problem persists, the
G1000 system should be serviced.
Additional
Features
G/S1 FAIL – G/S1 is inoperative.
Abort approach due to loss of GPS navigation.
GPS Nav
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.
Loss of GPS navigation due to GPS failure.
AFCS
GPS2 FAIL – GPS2 is inoperative.
Loss of GPS navigation due to position error.
Nav/Com/
XPDR/Audio
GPS1 FAIL – GPS1 is inoperative.
Comments
EIS
Message
GPS NAV LOST – Loss of GPS
navigation. Position error.
GPS NAV LOST – Loss of GPS
navigation. GPS fail.
ABORT APR – Loss of GPS navigation.
Abort approach.
TRUE APR – True north approach.
Change hdg reference to TRUE.
Flight
Instruments
GIA 63 Message Advisories (Cont.)
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
GIA 63W Message Advisories
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.
66
Comments
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
The GIA1 and/or GIA2 have an error in the
audio configuration. The G1000 system should
be serviced.
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
The GIA1 and/or GIA2 temperature is too high.
If problem persists, the G1000 system should be
serviced.
The GIA1 and/or GIA2 self-test has detected a
problem in the unit. The G1000 system should
be serviced.
A GIA mismatch has been detected, where only
one is SBAS capable.
The GIA1 and/or GIA 2 has incorrect software
installed. The G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
Comments
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
67
Procedures
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Flight
Planning
190-01062-01 Rev. A
GPS Nav
The COM1 and/or COM2 external push-to-talk
switch is stuck in the enable (or “pressed”)
position. Press the PTT switch again to cycle its
operation.
If the problem persists, the G1000 system
should be serviced.
COM1 RMT XFR – COM1 remote The COM1 and/or COM2 transfer switch is stuck
transfer key is stuck.
in the enabled (or “pressed”) position. Press the
COM2 RMT XFR – COM2 remote transfer switch again to cycle its operation. If
the problem persists, the G1000 system should
transfer key is stuck.
be serviced.
LOI – GPS integrity lost. Crosscheck GPS integrity is insufficient for the current phase
with other NAVS.
of flight.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to insufficient
navigation. Insufficient satellites.
satellites.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to position error.
navigation. Position error.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to GPS failure.
navigation. GPS fail.
ABORT APR – Loss of GPS
Abort approach due to loss of GPS navigation.
navigation. Abort approach.
APR DWNGRADE – Approach
Vertical guidance generated by SBAS is
downgraded.
unavailable, use LNAV only minimums.
AFCS
The system has detected a failure in COM1 and/
or COM2. COM1 and/or COM2 may still be
usable. The G1000 system should be serviced
when possible.
Nav/Com/
XPDR/Audio
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 G1000 system should be serviced.
EIS
Message
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.
Flight
Instruments
GIA 63W Message Advisories (Cont.)
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
GIA 63W Message Advisories (Cont.)
Message
TRUE APR – True north approach.
Change HDG reference to TRUE.
GPS1 SERVICE – GPS1 needs
service. Return unit for repair.
GPS2 SERVICE – GPS2 needs
service. Return unit for repair.
NAV1 SERVICE – NAV1 needs
service. Return unit for repair.
NAV2 SERVICE – NAV2 needs
service. Return unit for repair.
NAV1 RMT XFR – NAV1 remote
transfer key is stuck.
NAV2 RMT XFR – NAV2 remote
transfer key is stuck.
G/S1 FAIL – G/S1 is inoperative.
G/S2 FAIL – G/S2 is inoperative.
G/S1 SERVICE – G/S1 needs
service. Return unit for repair.
G/S2 SERVICE – G/S2 needs
service. Return unit for repair.
Comments
Displayed after passing the first waypoint of a
true north approach when the nav angle is set
to ‘AUTO’.
A failure has been detected in the GPS1 and/
or GPS2 receiver. The receiver may still be
available. The G1000 system should be serviced.
A failure has been detected in the NAV1
and/or NAV2 receiver. The receiver may still be
available. The G1000 system should be serviced.
The remote NAV1 and/or NAV2 transfer switch
is stuck in the enabled (or “pressed”) state.
Press the transfer switch again to cycle its
operation. If the problem persists, the G1000
system should be serviced.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The G1000 system
should be serviced.
A failure has been detected in glideslope
receiver 1 and/or receiver 2. The receiver may
still be available. The G1000 system should be
serviced when possible.
GEA 71 Message Advisories
Message
Comments
GEA1 CONFIG – GEA1 config error. The GEA1 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
system should be serviced.
GEA2 CONFIG – GEA2 config error. The GEA2 configuration settings do not match
Config service req’d.
those of backup configuration memory. The
system should be serviced.
68
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
Comments
The #1 GEA 71 has incorrect software installed.
The system should be serviced.
The #2 GEA 71 has incorrect software installed.
The system should be serviced.
EIS
Nav/Com/
XPDR/Audio
Message
MANIFEST – GEA1 software
mismatch, communication halted.
MANIFEST – GEA2 software
mismatch, communication halted.
Flight
Instruments
GEA 71 Message Advisories (Cont.)
GTX 33 Message Advisories
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
The #1 AHRS is not receiving true airspeed from
the air data computer. The AHRS relies on GPS
information to augment the lack of airspeed.
The G1000 system should be serviced.
AHRS1 GPS – AHRS1 using backup The #1 AHRS is using the backup GPS path.
GPS source.
Primary GPS path has failed. The G1000 system
should be serviced when possible.
AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving any or any useful
any GPS information.
GPS information. Check AFMS limitations. The
G1000 system should be serviced.
Procedures
Message
AHRS1 TAS – AHRS1 not receiving
airspeed.
Flight
Planning
GRS 77 Message Advisories
GPS Nav
MANIFEST – GTX1 software
mismatch, communication halted.
XPDR1 SRVC – XPDR1 needs
service. Return unit for repair.
XPDR1 FAIL – XPDR1 is
inoperative.
Comments
The transponder configuration settings do not
match those of backup configuration memory.
The G1000 system should be serviced.
The transponder has incorrect software installed.
The G1000 system should be serviced.
The #1 transponder should be serviced when
possible.
There is no communication with the #1
transponder.
AFCS
Message
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
69
GRS 77 Message Advisories (Cont.)
Message
Comments
AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS
backup GPS information.
information. The G1000 system should be
serviced.
AHRS1 GPS – AHRS1 operating
The #1 AHRS is operating exclusively in no-GPS
exclusively in no-GPS mode.
mode. The G1000 system should be serviced.
AHRS1 SRVC – AHRS1 Magnetic- The #1 AHRS earth magnetic field model is out
field model needs update.
of date. Update magnetic field model when
practical.
GEO LIMITS – AHRS1 too far
The aircraft is outside geographical limits for
North/South, no magnetic compass. approved AHRS operation. Heading is flagged
as invalid.
MANIFEST – GRS1 software
The #1 AHRS has incorrect software installed.
mismatch, communication halted.
The G1000 system should be serviced.
GMU 44 Message Advisories
Message
HDG FAULT – AHRS1
magnetometer fault has occurred.
MANIFEST – GMU1 software
mismatch, communication halted.
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.
GDC 74A Message Advisories
Message
MANIFEST – GDC1 software
mismatch, communication halted.
Comments
The GDC 74A 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
70
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
AFCS
MANIFEST – GDL software
mismatch, communication halted.
Nav/Com/
XPDR/Audio
GDL69 FAIL – GDL 69 has failed.
Comments
GDL 69 configuration settings do not match
those of backup configuration memory. The
G1000 system should be serviced.
A failure has been detected in the GDL 69.
The receiver is unavailable. The G1000 system
should be serviced
The GDL 69 has incorrect software installed.
The G1000 system should be serviced.
EIS
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
Flight
Instruments
GDL 69A Message Advisories
GPS Nav
Miscellaneous Message Advisories
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
Upon power-up, the G1000 system detects
that a stored flight plan waypoint is locked.
This occurs when an aviation database update
eliminates an obsolete waypoint. The flight
plan cannot find the specified waypoint and
flags this message. This can also occur with
user waypoints in a flight plan that is deleted.
Remove the waypoint from the flight plan if it
no longer exists in any database,
Or
update the waypoint name/identifier to reflect
the new information.
FPL WPT MOVE – Flight plan
The system has detected that a waypoint
waypoint moved.
coordinate has changed due to a new aviation
database update. Verify that stored flight plans
contain correct waypoint locations.
TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has
expired.
Flight
Planning
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
71
Miscellaneous Message Advisories (Cont.)
Message
DB CHANGE – Database changed.
Verify user modified procedures.
DB CHANGE – Database changed.
Verify stored airways.
FPL TRUNC – Flight plan has been
truncated.
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
LOCKED FPL – Cannot navigate
locked flight plan.
WPT ARRIVAL – Arriving at
waypoint -[xxxx]
STEEP TURN – Steep turn ahead.
INSIDE ARSPC – Inside airspace.
ARSPC AHEAD – Airspace ahead
less than 10 minutes.
ARSPC NEAR – Airspace near and
ahead.
72
Comments
This occurs when a stored flight plan contains
procedures that have been manually edited.
This alert is issued only after an aviation
database update. Verify that the user-modified
procedures in stored flight plans are correct
and up to date.
This occurs when a stored flight plan contains
an airway that is no longer consistent with
the aviation database. This alert is issued only
after an aviation database update. Verify use
of airways in stored flight plans and reload
airways as needed.
This occurs when a newly installed aviation
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.
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.
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint name.
A steep turn is 15 seconds ahead. Prepare to
turn.
The aircraft is inside the airspace.
Special use airspace is ahead of aircraft. The
aircraft will penetrate the airspace within 10
minutes.
Special use airspace is near and ahead of the
aircraft position.
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Annunciations & Alerts
Bad parallel track geometry.
Procedures
Invalid leg type for parallel offset.
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
IAF waypoint for parallel offset has been
passed.
The current vertical waypoint can not be
reached within the maximum flight path angle
and vertical speed constraints. The system
automatically transitions to the next vertical
waypoint.
The lateral flight plan contains a procedure
turn, vector, or other unsupported leg type
prior to the active vertical waypoint. This
prevents vertical guidance to the active vertical
waypoint.
The current track angle error exceeds the limit,
causing the vertical deviation to go invalid.
Hazard
Avoidance
VNV – Unavailable. Excessive track
angle error.
Flight
Planning
VNV – Unavailable. Unsupported
leg type in flight plan.
GPS Nav
PTK FAIL – Parallel track unavailable:
bad geometry.
PTK FAIL – Parallel track unavailable:
invalid leg type.
PTK FAIL – Parallel track unavailable:
past IAF.
UNABLE V WPT – Can’t reach
current vertical waypoint.
AFCS
SLCT NAV – Select NAV on CDI for
approach.
Nav/Com/
XPDR/Audio
SLCT FREQ – Select appropriate
frequency for approach.
Comments
Special use airspace is within 2 nm of the
aircraft position.
The system notifies the pilot that the loaded
approach is not active. Activate approach
when required.
The system notifies the pilot to load the
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.
The system notifies the pilot to set the CDI to
the correct NAV receiver. Set the CDI to the
correct NAV receiver.
EIS
Message
ARSPC NEAR – Airspace near – less
than 2 nm.
APR INACTV – Approach is not
active.
Flight
Instruments
Miscellaneous Message Advisories (Cont.)
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
73
Miscellaneous Message Advisories (Cont.)
Message
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
NO WGS84 WPT – Non WGS 84
waypoint for navigation -[xxxx]
TRAFFIC FAIL – Traffic device has
failed.
STRMSCP FAIL – Stormscope has
failed.
FAILED PATH – A data path has
failed.
MAG VAR WARN – Large magnetic
variance. Verify all course angles.
SVS – SVS DISABLED: Out of
available terrain region.
SVS – SVS DISABLED: Terrain DB
resolution too low.
SCHEDULER [#] – <message>.
Comments
The current crosstrack exceeds the limit,
causing vertical deviation to go invalid.
A parallel course has been selected, causing
the vertical deviation to go invalid.
The position of the selected waypoint [xxxx]
is not calculated based on the WGS84 map
reference datum and may be positioned in
error as displayed. Do not use GPS to navigate
to the selected non-WGS84 waypoint.
The G1000 is no longer receiving data from
the traffic system. The traffic device should be
serviced.
Stormscope has failed. The G1000 system
should be serviced.
A data path connected to the GDU or the GIA
63/W has failed.
The GDU’s internal model cannot determine
the exact magnetic variance for geographic
locations near the magnetic poles. Displayed
magnetic course angles may differ from the
actual magnetic heading by more than 2°.
Synthetic Vision is disabled because the aircraft
is not within the boundaries of the installed
terrain database.
Synthetic Vision is disabled because a terrain
database of sufficient resolution (9 arc-second
or better) is not currently installed.
Message criteria entered by the user.
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
74
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Appendix
Flight
Instruments
Appendix
PFD Softkey Map
EIS
ADF/DME
ALERTS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Top Level PFD Softkeys
ADF/DME
ALERTS
Flight
Planning
TRFC-1
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
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
75
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.
TRFC-2
Procedures
ALERTS
STRMSCP
Appendix
Cycles through traffic display options:
TRFC-1: Traffic displayed on inset map
TRFC-2: Traffic Map Page is displayed in
the inset map window
Displays topographical data (e.g.,
coastlines, terrain, rivers, lakes) and
elevation scale on Inset Map
Displays terrain information on Inset Map
EIS
Flight
Instruments
TRAFFIC
Nav/Com/
XPDR/Audio
TOPO
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)
AFCS
STRMSCP
GPS Nav
NEXRAD
Flight
Planning
XM LTNG
Procedures
ADF/DME
SYN VIS
ALERTS
ALERTS
ALT UNIT
Hazard
Avoidance
HSI FMT
Abnormal
Operation
Additional
Features
Select the BACK Softkey
to return to the top-level softkeys
360 HSI
IN
HPA
Annun/
Alerts
METERS
BACK
ARC HSI
ALERTS
ALERTS
Appendix
ALERTS
PATHWAY
SYN TERR HRZN HDG APTSIGNS
ALERTS
Index
PFD Configuration Softkeys
76
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Appendix
SYN VIS
Additional
Features
Appendix
Index
77
Annun/
Alerts
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Abnormal
Operation
190-01062-01 Rev. A
Hazard
Avoidance
HSI FRMT
Procedures
360 HSI
ARC HSI
Displays the DME Information Window
Cycles the Bearing 1 Information Window through NAV1 or GPS/waypoint
identifier and GPS-derived distance
information, and ADF/frequency.
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree format
Displays the HSI in an arc format
DME
BRG1
Flight
Planning
OFF
Direction with head and crosswind
speed components
Information not displayed
OPTN 3
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
Wind direction arrows with headwind
OPTN 1
and crosswind components
Wind direction arrow and speed
OPTN 2
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, and ADF/frequency.
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)
ALERTS
Procedures
ADF/DME
Hazard
Avoidance
ALERTS
Additional
Features
Press the BACK Softkey to return
to the top-level softkeys.
ALERTS
Transponder Softkeys
Displays transponder mode selection softkeys
XPDR
STBY
Appendix
Annun/
Alerts
Abnormal
Operation
Press the BACK Softkey to return
to the previous level softkeys.
Index
ON
78
Selects Standby Mode (transponder does
not reply to any interrogations)
Selects Mode A (transponder replies to
interrogations)
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Appendix
Displays Alerts Window
Hazard
Avoidance
ALERTS
Procedures
Displays Nearest Airports Window
Flight
Planning
NRST
GPS Nav
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
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
Use numbers to enter code
ALT
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
79
Flight
Instruments
Appendix
MFD Softkey Map
DCLTR
MAP
ENGINE
SHW CHRT
CHKLIST
(optional)
(optional)
EIS
DCLTR-1
DCLTR-2
Nav/Com/
XPDR/Audio
DCLTR-3
AFCS
TRAFFIC
ENGINE
SYSTEM
TOPO
(Default softkey
Press the BACK Softkey on this
is dependant on
the selection made
level to return to the top softkey level.
in the map setup
options)
(optional) (optional) (optional)
TERRAIN
AIRWAYS
STRMSCP
NEXRAD
BACK
XM LTNG
AIRWY ON
FUEL
AIRWY LO
GPS Nav
AIRWAY HI
DEC FUEL
Flight
Planning
Procedures
ENGINE
DONE
EXIT
EMERGCY
MFD Softkeys
Displays EIS-Engine Page
ENGINE
Additional
Features
Hazard
Avoidance
RST FUEL
The DONE Softkey changes to UNDO when the checklist
item is already checked
SYSTEM
Displays EIS-System Page
FUEL
Selects the fuel quantity softkeys
Abnormal
Operation
DEC FUEL Press to decrease remainingfuel
quantity in 1-gallon increments
INC FUEL Press to increase remaining fuel
quantity in 1-gallon increments
RST FUEL Press to reset fuel to full
MAP
TRAFFIC
Appendix
Annun/
Alerts
INC FUEL
Index
TOPO
80
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
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Appendix
AIRWAYS
Hazard
Avoidance
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
When available, displays optional
airport and terminal procedure charts
When available, displays optional
checklists
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
CHKLIST
Procedures
SHW CHRT
Flight
Planning
DCLTR (3)
GPS Nav
BACK
AFCS
XM LTNG
Nav/Com/
XPDR/Audio
NEXRAD
EIS
STRMSCP
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
TERRAIN
Index
190-01062-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
81
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
82
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 Rev. A
Index
Activate a flight plan 18
Active Channel 49
ADF 9, 10, 52, 77, 78
ADS-B 40
AHRS 69, 70
Airport Signs 45, 46
Airways 81
AP 56
Assist 8
Audio panel controls
NAV1, NAV2 10
Autopilot 57
Edit a flight plan 27
Enable Terrain 43
Endurance 6
F
Nav/Com/
XPDR/Audio
GPS Nav
H
Flight
Planning
Barometric Altitude Minimums 3
Barometric pressure 78
AFCS
FD 56
Flight Director 13
Flight ID 9
Flight path marker 45
FliteCharts® 46, 47
Frequency Transfer 10
Fuel remaining 6
Fuel used 6
B
Horizon heading 45
Inhibit 42
Inhibit Terrain 42
Inset Map 75, 76
IOI 57, 58
D
Lightning 35, 36, 76
DCLTR Softkey 46
Dead Reckoning 53
Declutter 52, 75, 81
Direct-to 17
DME 9, 10
DR mode 53, 54
M
Additional
Features
CDI 1, 10, 73
Cell 35, 36
Cell mode 36
Channel Presets 50
ChartView 46, 47
Clearance player 11
Clearance Recorder 11
Code selection softkeys 9
COM 10, 11, 51
Hazard
Avoidance
I
Procedures
C
J
Jeppesen 47
Abnormal
Operation
L
Annun/
Alerts
Map panning 37
Message advisories 59–74
MET 56
METAR 37
Appendix
Index
190-01062-01 Rev. A
EIS
E
Flight
Instruments
A
Garmin G1000 Cockpit Reference Guide for the DA42-L360
Index-1
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Index
Minimums 59
Mistrim 57
MKR/MUTE 11
Mode S 79
Mode selection softkeys 9
Multi Function Display (MFD)
Softkeys 80
N
NAV 10
NAV1 1, 10
NAV2 1, 10
Navigation database 19, 20
NEXRAD 37, 38, 76, 81
O
OBS 2
Obstacles 62, 66
Overspeed Protection 14
P
TA 59
TAF 37
TAS 39, 59, 69
Terrain 41, 62, 76, 80, 81
Terrain-SVS 41, 42, 43
Timer 71
Topographical data 76, 80
Traffic 35, 39, 80
Traffic Advisory 59
Traffic advisory 38
Traffic map page 39, 41
Transponder 9, 78, 79
V
Vertical speed guidance 20
Vertical track 59
VNV 17, 52, 73, 74
Vspeed 2
W
Pathways 45, 46
R
Reversionary mode 51
ROC 57, 58
S
SafeTaxi® 46
SBAS 14, 32, 43, 53, 66, 67
Store Flight Plan 27
Stormscope lightning data 35, 36, 76
Strike 35
Strike mode 36
SVS 45, 74
Synthetic Vision System 45
Index-2
T
Waypoint Selection Submenu 24, 25
Weather data link page 37
Wind data 77
X
XM lightning 76, 81
XM weather 37
Y
Yaw damper 56
Garmin G1000 Cockpit Reference Guide for the DA42-L360
190-01062-01 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.
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Garmin (Europe) Ltd
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Garmin Corporation
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Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com
© 2004-2010 Garmin Ltd. or its subsidiaries
190-01062-01 Rev. A