Garmin | G1000: Diamond DA40NG | Garmin G1000: Diamond DA40NG G1000® Cockpit Reference Guide for Diamond DA40NG

Garmin G1000: Diamond DA40NG G1000® Cockpit Reference Guide for Diamond DA40NG
G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the DA40NG
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 © 2010, 2011 Garmin Ltd. or its subsidiaries. All rights reserved.
This manual reflects the operation of System Software version 0915.03 or later for the Diamond
DA40NG. Some differences in operation may be observed when comparing the information in
this manual to earlier or later software versions.
Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.
Tel: 913/397.8200Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411Fax 503/364.2138
Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park,
Southampton, SO40 9RB, U.K.
Tel: 44/0870.8501241
Fax: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Tel: 886/02.2642.9199
Fax: 886/02.2642.9099
For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount
and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.
Web Site Address: www.garmin.com
Except as expressly provided herein, no part of this manual may be reproduced, copied,
transmitted, disseminated, downloaded or stored in any storage medium, for any purpose
without the express written permission of Garmin. Garmin hereby grants permission to
download a single copy of this manual and of any revision to this manual onto a hard drive or
other electronic storage medium to be viewed for personal use, provided that such electronic
or printed copy of this manual or revision must contain the complete text of this copyright
notice and provided further that any unauthorized commercial distribution of this manual or any
revision hereto is strictly prohibited.
Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. 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.
March, 2011
190-00953-01 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 avoidance feature. The terrain avoidance feature is NOT
intended to be used as a primary reference for terrain avoidance and does
not relieve the pilot from the responsibility of being aware of surroundings
during flight. The terrain avoidance feature is only to be used as an aid for
terrain avoidance. Terrain data is obtained from third party sources. Garmin
is not able to independently verify the accuracy of the terrain data.
WARNING: The displayed minimum safe altitudes (MSAs) are only advisory
in nature and should not be relied upon as the sole source of obstacle and
terrain avoidance information. Always refer to current aeronautical charts
for appropriate minimum clearance altitudes.
WARNING: 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 system displays is provided as an
aid in visually acquiring traffic. Pilots must maneuver the aircraft based only
upon ATC guidance or positive visual acquisition of conflicting traffic.
WARNING: 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 DA40NG
190-00953-01 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 DA40NG
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 DA40NG Airplane Flight Manual (AFM). Thoroughly practice basic
operation prior to actual use. During flight operations, carefully compare
indications from the G1000 to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety
purposes, always resolve any discrepancies before continuing navigation.
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
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 DA40NG
190-00953-01 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.
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Record of Revisions
Part Number
190-00953-00
190-00953-01
Change Summary
Initial Release
Changed Oil Pressure warning annunciation description.
Changed system software number from 0915.01 to 0915.03
Revision Date of Revision Affected Pages
A
March, 2011
All
190-00953-01 Rev. A
Description
Production release
Garmin G1000 Cockpit Reference Guide for the DA40NG
RR-1
Record of Revisions
Blank Page
RR-2
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Table of Contents
FLIGHT INSTRUMENTS................................................................................................................. 1
Selecting the Altimeter Barometric Pressure Setting....................................................... 1
Selecting Standard Barometric Pressure (29.92 in Hg)..................................................... 1
Change Altimeter Barometric Pressure Setting Units....................................................... 1
Change Navigation Sources.................................................................................................... 1
Enable/Disable OBS Mode While Navigating with GPS..................................................... 2
Generic Timer.............................................................................................................................. 2
Configure Vspeed Bugs............................................................................................................. 2
Set Barometric Minimum Descent Altitude......................................................................... 3
Displaying Wind Data............................................................................................................... 3
Changing HSI Format................................................................................................................ 3
ENGINE INDICATION SYSTEM.................................................................................................. 5
Engine SYSTEM Display............................................................................................................ 6
Engine Fuel Display................................................................................................................... 6
NAV/COM/TRANSPONDER/AUDIO PANEL.......................................................................... 9
ADF Tuning (Optional)............................................................................................................... 9
DME Tuning (Optional).............................................................................................................. 9
Enter a Transponder Code....................................................................................................... 9
Selecting a COM Radio........................................................................................................... 10
Selecting a NAV Radio............................................................................................................ 10
NAV/COM Tuning...................................................................................................................... 10
Digital Clearance Recorder and Player............................................................................... 10
Intercom System (ICS) Isolation........................................................................................... 11
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM........................................................ 13
Flight Director Activation...................................................................................................... 13
Vertical Modes.......................................................................................................................... 14
Lateral Modes........................................................................................................................... 15
GPS NAVIGATION......................................................................................................................... 17
Direct-to Navigation............................................................................................................... 17
Activate a Stored Flight Plan................................................................................................ 18
Activate a Flight Plan Leg...................................................................................................... 18
Stop Navigating a Flight Plan............................................................................................... 19
Vertical Navigation (VNAV)................................................................................................... 19
FLIGHT PLANNING....................................................................................................................... 21
Trip Planning............................................................................................................................. 21
Create a User Waypoint.......................................................................................................... 23
Delete a User Waypoint.......................................................................................................... 24
Create a Flight Plan................................................................................................................. 24
Insert a Waypoint in the Active Flight Plan....................................................................... 25
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
i
Table of Contents
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............................................................................. 34
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............................................................................................ 40
Terrain-SVS................................................................................................................................ 40
ADDITIONAL FEATURES............................................................................................................ 43
Synthetic Vision........................................................................................................................ 43
Terminal Procedure Charts.................................................................................................... 44
XM® Radio Entertainment..................................................................................................... 46
Electronic Checklists (Optional)............................................................................................ 48
ABNORMAL OPERATION.......................................................................................................... 51
Reversionary Mode................................................................................................................. 51
Abnormal COM Operation..................................................................................................... 51
Hazard Displays with Loss of GPS Position........................................................................ 51
Unusual Attitudes.................................................................................................................... 52
Dead Reckoning....................................................................................................................... 52
ii
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Table of Contents
ANNUNCIATIONS & ALERTS.................................................................................................... 55
WARNING Annunciation......................................................................................................... 55
CAUTION Annunciation........................................................................................................... 55
Advisory Annunciation........................................................................................................... 56
Alert Message........................................................................................................................... 56
AFCS Alerts................................................................................................................................ 56
Terrain-SVS Alerts.................................................................................................................... 57
Terrain-SVS System Status Annunciations......................................................................... 58
Voice Alerts............................................................................................................................... 58
MFD & PFD Message Advisories........................................................................................... 59
Database Message Advisories.............................................................................................. 60
GMA 1347 Message Advisories............................................................................................. 62
GIA 63 Message Advisories.................................................................................................... 63
GIA 63W Message Advisories................................................................................................ 65
GEA 71 Message Advisories................................................................................................... 68
GTX 33 Message Advisories................................................................................................... 69
GRS 77 Message Advisories................................................................................................... 69
GMU 44 Message Advisories................................................................................................. 70
GDL 69A Message Advisories................................................................................................ 70
GDC 74A Message Advisories................................................................................................ 70
Miscellaneous Message Advisories...................................................................................... 71
APPENDIX........................................................................................................................................ 75
PFD Softkey Map..................................................................................................................... 75
MFD Softkey Map.................................................................................................................... 80
INDEX..........................................................................................................................................Index-1
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
iii
Table of Contents
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iv
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Flight Instruments
Flight
Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
EIS
Press the PFD Softkey.
2)
Press the STD BARO Softkey to set standard barometric pressure.
AFCS
1)
Nav/Com/
XPDR/Audio
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Flight
Planning
Press the PFD Softkey to display the second-level softkeys.
GPS Nav
1)
Procedures
Or:
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
Press the BACK Softkey to return to the top-level softkeys.
Hazard
Avoidance
4)
CHANGE NAVIGATION SOURCES
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
frequency.
3)
Press the CDI Softkey a third time to return to GPS.
Annun/
Alerts
2)
Abnormal
Operation
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
Additional
Features
1)
Appendix
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
1
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
1)
Press the OBS Softkey to select OBS Mode.
2)
Turn a CRS Knob to select the desired course to/from the waypoint. Press a
CRS Knob to synchronize the Selected Course with the bearing to the next
waypoint.
3)
Press the OBS Softkey again to disable OBS Mode.
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to select the
time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then
press the ENT Key. The UP/DOWN field is now highlighted.
2)
Turn the small FMS Knob to display the UP/DOWN window. Turn the FMS
Knob to select ‘UP’ or ‘DOWN’, then press the ENT Key. ‘START?’ is now
highlighted.
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it starts counting UP after reaching zero). Press the CLR
Key or the TMR/REF Softkey to remove the window.
Additional
Features
CONFIGURE VSPEED BUGS
1) Press the TMR/REF Softkey.
2) Turn the large FMS Knob to highlight the desired Vspeed.
3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
Abnormal
Operation
Hazard
Avoidance
Procedures
Flight
Planning
AFCS
GENERIC TIMER
GPS Nav
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Instruments
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
5)
Turn the small FMS Knob clockwise to ON or counterclockwise to OFF.
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
Index
Appendix
Annun/
Alerts
speed has been changed from a default value, an asterisk appears next to
the speed).
2
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Flight Instruments
Flight
Instruments
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
1) Press the TMR/REF Softkey.
Turn the small FMS Knob clockwise to BARO.
4)
Press the ENT Key.
5)
Use the small FMS Knob to enter the desired altitude.
6)
Press the ENT Key.
7)
To remove the window, press the CLR Key or the TMR/REF Softkey.
AFCS
3)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.
EIS
2)
2)
Press the WIND Softkey to display wind data to the left of the HSI.
3)
Press one of the OPTN softkeys to change how wind data is displayed.
4)
To remove the Wind Data Window, press the OFF Softkey.
Procedures
Press the PFD Softkey.
Flight
Planning
1)
GPS Nav
DISPLAYING WIND DATA
CHANGING HSI FORMAT
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI Softkey to display the full size HSI.
Additional
Features
Press the PFD Softkey.
Hazard
Avoidance
1)
Or:
Abnormal
Operation
Press the ARC HSI Softkey to display the arc style HSI.
Annun/
Alerts
Appendix
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
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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Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Engine Indication System
Flight
Instruments
ENGINE INDICATION SYSTEM
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Engine Instrument Display on the MFD
Annun/
Alerts
Appendix
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
5
ENGINE SYSTEM DISPLAY
Pressing the ENGINE Softkey displays the SYSTEM Softkey. Press the SYSTEM
Softkey to view the Engine System Display.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Engine Indication System
Index
Appendix
Annun/
Alerts
Engine System Display on the MFD
ENGINE FUEL DISPLAY
Pressing the ENGINE Softkey displays the FUEL Softkey. Press the FUEL Softkey
to view the Engine Fuel Display.
Fuel used (GAL USED), endurance, and range (RANGE NM) are all calculated
based on the last manual adjustment of the fuel remaining (GAL REM).
6
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Engine Indication System
The following softkeys allow for adjustment of the remaining fuel quantity.
EIS
Nav/Com/
XPDR/Audio
AFCS
- 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 1gallon increments
- RST FUEL – Resets the fuel remaining to the maximum fuel quantity for the
aircraft and fuel used to zero.
Flight
Instruments
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.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index
Engine Fuel Display on the MFD
7
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
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Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Nav/Com/XPDR/Audio Panel
Flight
Instruments
NAV/COM/TRANSPONDER/AUDIO PANEL
ADF TUNING (OPTIONAL)
EIS
3)
Turn the large FMS Knob to select the next desired field.
4)
Turn the small FMS Knob to enter the desired number.
5)
Repeat steps 3 and 4 until the desired ADF frequency is entered.
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.
9)
Turn the small FMS Knob to select ANT, ADF, ADF/BFO, or ANT/BFO.
Flight
Planning
Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
GPS Nav
2)
AFCS
Press the ADF/DME Softkey.
Nav/Com/
XPDR/Audio
1)
10) Press the ENT Key to complete the selection.
Procedures
DME TUNING (OPTIONAL)
2)
Turn the large FMS to select the DME source field.
3)
Turn the small FMS Knob to select the desired Nav radio.
4)
Press the ENT Key to complete the selection.
Additional
Features
Press the ADF/DME or DME Softkey.
Hazard
Avoidance
1)
Press the XPDR Softkey to display the transponder mode selection softkeys.
2)
Press the CODE Softkey to display the transponder code selection softkeys,
for digit entry.
3)
Press the digit softkeys to enter the code in the code field. When entering
the code, the next key in sequence must be pressed within 10 seconds, or
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
Annun/
Alerts
1)
Abnormal
Operation
ENTER A TRANSPONDER CODE
Appendix
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
9
SELECTING A COM RADIO
Transmit/Receive
Press the COM1 MIC, COM2 MIC, or COM3 MIC Key (optional COM, if
installed) on the audio panel.
EIS
Flight
Instruments
Nav/Com/XPDR/Audio Panel
Press the COM1, COM2, or COM3 Key (optional COM, if installed) on the
audio panel.
SELECTING A NAV RADIO
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
2)
Press the NAV1, NAV2, DME, or ADF Key on the audio panel to select or
deselect the navigation radio audio source. All radio keys can be selected
individually or together.
Press the small tuning knob to select the desired radio for tuning. A light
blue box highlights the radio frequency to be tuned.
2)
Turn the respective tuning knobs to enter the desired frequency into the
standby frequency field. The large knob enters MHz and the small knob
enters kHz.
3)
Press the Frequency Transfer Key to place the frequency into the active
frequency field.
DIGITAL CLEARANCE RECORDER AND PLAYER
NOTE: Only the audio for the selected COM MIC Key is recorded. Audio is
not recorded for COM3 MIC.
Annun/
Alerts
Abnormal
Operation
1)
Hazard
Avoidance
NAV/COM TUNING
Additional
Features
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Receive Only
Index
Appendix
• 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.
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Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Nav/Com/XPDR/Audio Panel
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
Selected
radios; pilot;
copilot;
passengers;
music
Selected
radios; pilot;
copilot;
passengers;
music
Copilot;
passengers;
music
Copilot;
passengers;
music
PILOT
ON
OFF
Selected
radios; pilot
Copilot
Selected
radios; pilot;
passengers;
music
Selected
radios; pilot;
copilot
Passengers;
music
COPILOT
OFF
ON
Selected
radios; pilot;
passengers;
music
CREW
ON
ON
Selected
radios; pilot;
copilot
Hazard
Avoidance
OFF
Procedures
OFF
Flight
Planning
ALL
Selected
radios; pilot;
copilot;
passengers;
music
GPS Nav
Passenger
Hears
AFCS
Copilot
Hears
Nav/Com/
XPDR/Audio
Pilot Hears
EIS
Mode
Flight
Instruments
INTERCOM SYSTEM (ICS) ISOLATION
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
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 DA40NG
190-00953-01 Rev. A
AFCS
AFCS
FLIGHT DIRECTOR ACTIVATION
Modes Selected
HDG
Appendix
Heading Select
PIT
GP
GS
PIT
Annun/
Alerts
HDG Key
Pitch Hold (default)
Glidepath
Glideslope
Pitch Hold (default)
Abnormal
Operation
Approach**
PIT
Additional
Features
APR Key
GPS
VAPP
LOC
Pitch Hold (default)
Hazard
Avoidance
Navigation**
Procedures
NAV Key
ROL
ROL
ROL
GA
ROL
ROL
ROL
GPS
VOR
LOC
BC
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
Flight
Planning
FD Key
AP Key
CWS Switch
GA Switch
ALT Key
VS Key
VNV Key
Lateral
Roll Hold (default)
Roll Hold (default)
Roll Hold (default)
Go Around
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 DA40NG
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.
190-00953-01 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.
Control Pressed
Nav/Com/
XPDR/Audio
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
EIS
NOTE: If sensor information (other than attitude) required for a flight director
mode becomes invalid or unavailable, the flight director automatically reverts
to the default mode for that axis.
Flight
Instruments
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM
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 DA40NG
190-00953-01 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
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
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 DA40NG
190-00953-01 Rev. A
GPS Navigation
NOTE: Refer to the Aircraft Flight Manual (AFM) to determine if SBAS
functionality is approved.
Flight
Instruments
GPS NAVIGATION
EIS
DIRECT-TO NAVIGATION
1)
3)
5)
7)
11)
Direct-to Navigation from the PFD
2)
4)
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
17
Index
5)
).
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.
Appendix
3)
Press the Direct-to Key (
Annun/
Alerts
1)
Abnormal
Operation
12)
Additional
Features
10)
Hazard
Avoidance
9)
Procedures
8)
Flight
Planning
6)
GPS Nav
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.
AFCS
2)
Press the Direct-to (
Nav/Com/
XPDR/Audio
Direct-to Navigation from the MFD
6)
Turn the large FMS Knob to place the cursor over the ‘ALT’ altitude field.
7)
Turn the small FMS Knob to enter the desired altitude.
8)
Press the ENT Key. If the waypoint entered is an airport, the option to
select MSL or AGL is now displayed. If the waypoint is not an airport,
proceed to step 10.
9)
Turn the small FMS Knob to select ‘MSL’ or ‘AGL’.
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
GPS Navigation
10) Press the ENT Key. The cursor is placed in the ‘OFFSET’ field.
AFCS
11) Turn the small FMS Knob to enter the desired target altitude offset from
the selected Direct-to.
GPS Nav
12) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to
highlight the ‘CRS’ field.
13) Turn the small FMS Knob to enter the desired course to the waypoint.
14) Press the ENT Key to highlight ‘ACTIVATE?’.
ACTIVATE A STORED FLIGHT PLAN
1)
Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan
4)
Press the ACTIVE Softkey. The confirmation window is now displayed.
5)
With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel
the flight plan activation, turn the large FMS Knob to highlight ‘CANCEL’ and
press the ENT Key.
ACTIVATE A FLIGHT PLAN LEG
1)
From the Active Flight Plan Page, press the FMS Knob to activate the cursor
and turn the large FMS Knob to highlight the desired waypoint.
2)
On the MFD, press the ACT LEG Softkey.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
15) Press the ENT again to activate the Direct-to.
OR
Index
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)
18
With ‘Activate’ highlighted, press the ENT Key.
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
GPS Navigation
Flight
Instruments
STOP NAVIGATING A FLIGHT PLAN
2)
Press the MENU Key to display the Page Menu Window.
3)
Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT
Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan.
This does not delete the stored flight plan, only the active flight plan.
VERTICAL NAVIGATION (VNAV)
AFCS
GPS Nav
The aviation database only contains altitudes for procedures that call for “Cross
at” altitudes. If the procedure states “Expect to cross at,” the altitude is not in the
database. In this case the altitude may be entered manually.
Nav/Com/
XPDR/Audio
Press the FPL Key to display the Active Flight Plan Page.
EIS
1)
Flight
Planning
Procedures
Large White
Text
Large Light
Blue Text
Hazard
Avoidance
Small Light
Blue Text
Additional
Features
Small Light
Blue Subdued
Text
Abnormal
Operation
Small White Text
with Altitude
Restriction Bar
Annun/
Alerts
Cross AT or ABOVE 5,000 ft
Appendix
Cross AT 2,300 ft
Cross AT or BELOW 3,000 ft
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
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 the aviation
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
aviation database and is
provided as a reference.
Altitude is designated
for use in giving vertical
flight path guidance.
Altitude has been
retrieved from the
aviation database or has
been entered by the pilot
and matches a published
altitude in the aviation
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 DA40NG
Light Blue
Subdued Text
190-00953-01 Rev. A
Flight Planning
Flight
Instruments
FLIGHT PLANNING
TRIP PLANNING
Turn the large FMS Knob to select the ‘AUX’ page group.
2)
Turn the small FMS Knob to select the first rectangular page icon.
3)
The current ‘PAGE MODE’ is displayed at the top of the page: ‘AUTOMATIC’
or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL
Softkey.
4)
For Direct-to planning:
EIS
1)
AFCS
GPS Nav
b) If necessary, press the MENU Key and select ‘Set WPT to Present
Position’ to display ‘P.POS’.
Flight
Planning
c) Press the ENT Key and the flashing cursor moves to the ending
waypoint field.
Procedures
d) Enter the identifier of the ending waypoint and press the ENT Key to
accept the waypoint.
Or:
Hazard
Avoidance
For point-to-point planning:
a) Enter the identifier of the starting waypoint.
Additional
Features
b) Once the waypoint’s identifier is entered, press the ENT Key to accept
the waypoint. The flashing cursor moves to the ending waypoint.
Abnormal
Operation
c) Again, enter the identifier of the ending waypoint.
d) Press the ENT Key to accept the waypoint.
Or:
Annun/
Alerts
For flight plan leg planning:
a) Press the FPL Softkey (at the bottom of the display).
Appendix
b) Turn the small FMS Knob to select the desired flight plan (already
stored in memory), by number.
c) Turn the large FMS Knob to highlight the ‘LEG’ field.
Garmin G1000 Cockpit Reference Guide for the DA40NG
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.
190-00953-01 Rev. A
Nav/Com/
XPDR/Audio
a) Press the WPTS Softkey and verify that the starting waypoint field
indicates ‘P.POS’ (present position).
Flight
Instruments
Selecting ‘FPL 00’ displays the active flight plan. If an active flight plan
is selected, ‘REM’ is an available option to display planning data for the
remainder of the flight plan.
EIS
Flight Planning
NOTE: The page mode must be set to ‘MANUAL’ to perform the following
steps.
Nav/Com/
XPDR/Audio
5)
Turn the large FMS Knob to highlight the departure time (DEP TIME) field.
Enter the departure time. Press the ENT Key when finished. Departure time
may be entered in local or UTC time, depending upon system settings.
7)
The flashing cursor moves to the ground speed (GS) field. Enter the ground
speed. Press the ENT Key when finished. Note that in ‘automatic’ page
mode, ground speed is provided by the system.
8)
The flashing cursor moves to the fuel flow field. Enter the fuel flow. Press
the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel flow
is provided by the system.
9)
The flashing cursor moves to the fuel onboard field. Enter the fuel onboard.
Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page mode, fuel
onboard is provided by the fuel totalizer.
Additional
Features
6)
10) The flashing cursor moves to the calibrated airspeed (CALIBRATED AS) field.
Enter the calibrated airspeed. Press the ENT Key when finished. Note that
in ‘AUTOMATIC’ page mode, calibrated airspeed is provided by the system.
Abnormal
Operation
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
NOTE: The departure time on the Trip Planning Page is used for preflight
planning. Refer to the Utility Page for the actual flight departure time.
11) The flashing cursor moves to the altitude (IND ALTITUDE) field. Enter the
altitude. Press the ENT Key when finished. Note that in ‘AUTOMATIC’ page
mode, altitude is provided by the system.
Appendix
Annun/
Alerts
12) The flashing cursor moves to the barometric setting (PRESSURE) field. Enter
the desired baro setting. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, the baro setting is provided by the setting entered
on the PFD.
Index
13) The flashing cursor moves to the air temperature (TOTAL AIR TEMP) field. Enter
the desired air temperature. Press the ENT Key when finished. Note that in
‘AUTOMATIC’ page mode, air temperature is provided by the system outside
air temperature.
22
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Flight Planning
Flight
Instruments
CREATE A USER WAYPOINT
Turn the large FMS Knob to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the NEW Softkey. A waypoint is created at the current aircraft
position.
4)
Enter the desired waypoint name.
5)
Press the ENT Key.
6)
The cursor is now in the ‘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:
EIS
1)
Nav/Com/
XPDR/Audio
GPS Nav
Flight
Planning
b) Turn the large FMS Knob to select the desired waypoint.
c) Press the ENT Key.
b) Turn the small FMS Knob to the right to display the ‘NRST’ waypoints
to the aircraft’s current position.
Additional
Features
c) Turn the large FMS Knob to select the desired waypoint.
d) Press the ENT Key.
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
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.
Press the ENT Key.
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index
8)
Abnormal
Operation
Or:
After pressing the ENT Key, the cursor is displayed in the ‘RAD’ (radial)
field. Enter the desired radial from the reference waypoint.
Hazard
Avoidance
a) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list
is displayed.
Procedures
Or:
7)
AFCS
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.
23
Flight Planning
Flight
Instruments
9)
11) Press the FMS Knob to remove the flashing cursor.
DELETE A USER WAYPOINT
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
10) Press the ENT Key. The cursor is now placed for entering another reference
waypoint, if desired.
1)
Turn the large FMS Knob to select the ‘WPT’ page group.
2)
Turn the small FMS Knob to select the User WPT Information Page.
3)
Press the FMS Knob to activate the cursor.
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.
6)
Press the DELETE Softkey.
7)
The message ‘Would you like to delete the user waypoint?’ is displayed. With
‘YES’ highlighted, press the ENT Key.
CREATE A FLIGHT PLAN
NOTE: When creating a flight plan in the Active Flight Plan Window, the first
leg is activated automatically after it is created.
Hazard
Avoidance
Procedures
The cursor is now displayed in the ‘DIS’ (distance) field. Enter the desired
distance from the reference waypoint.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
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.
24
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Flight Planning
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
If necessary, press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired flight plan waypoint. The
new waypoint is inserted before the highlighted waypoint.
4)
Turn the small FMS Knob. The Waypoint Information Window is now
displayed.
5)
Enter the new flight plan waypoint by one of the following:
Abnormal
Operation
2)
Additional
Features
Press the FPL Key to display the active flight plan.
Hazard
Avoidance
1)
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’ airport
waypoints 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 DA40NG
EIS
INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN
190-00953-01 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.
2)
Press the FMS Knob to activate the cursor (not required on the PFD).
3)
Turn the large FMS Knob to highlight the waypoint after the desired airway
entry point. If this waypoint is not a valid airway entry point, a valid entry
point should be entered at this time.
4)
Turn the small FMS Knob one click clockwise and press the LD AIRWY
Softkey, or press the MENU Key and select “Load Airway”. The Select
Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway”
menu item is available only when an acceptable airway entry waypoint has
been chosen (the waypoint ahead of the cursor position).
5)
Turn the FMS Knob to select the desired airway from the list, and press the
ENT Key. Low altitude airways are shown first in the list, followed by “all”
altitude airways, and then high altitude airways.
6)
Turn the FMS Knob to select the desired airway exit point from the list, and
press the ENT Key. ‘LOAD?’ is highlighted.
7)
Press the ENT Key. The system returns to editing the flight plan with the
new airway inserted.
INVERT AN ACTIVE FLIGHT PLAN
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
c) Turn the large FMS Knob to select the desired waypoint.
26
1)
Press the FPL Key to display the active flight plan.
2)
Press the MENU Key to display the Page Menu.
3)
Turn the large FMS Knob to highlight ‘Invert Flight Plan’.
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Flight Planning
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.
Flight
Instruments
4)
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
AFCS
Or, for a stored flight plan:
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.
4)
With ‘OK’ highlighted, press the ENT Key to remove the selected procedure
or airway.
After creating a flight plan on either the PFD or MFD, it may be saved by
pressing the MENU Key.
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.
3)
Turn the large FMS Knob to highlight the desired flight plan.
4)
Press the EDIT Softkey.
Index
Press the FPL Key on the MFD and turn the small FMS Knob to display the
Flight Plan Catalog Page.
Appendix
1)
Garmin G1000 Cockpit Reference Guide for the DA40NG
Abnormal
Operation
1)
Additional
Features
STORE A FLIGHT PLAN
Hazard
Avoidance
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.
Procedures
2)
Flight
Planning
d) Press the EDIT Softkey.
190-00953-01 Rev. A
Nav/Com/
XPDR/Audio
1)
EIS
REMOVE A DEPARTURE, ARRIVAL, APPROACH, OR AIRWAY FROM A FLIGHT
PLAN
27
5)
Turn the large FMS Knob to place the cursor in the desired location.
6)
Enter the changes, then press the ENT Key.
7)
Press the FMS Knob to return to the Flight Plan Catalog Page.
DELETE A WAYPOINT FROM THE FLIGHT PLAN
1)
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Flight Planning
Press the FPL Key to display the active flight plan. Press the FMS Knob to
activate the cursor.
Or, for a stored flight plan:
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.
2)
Turn the large FMS Knob to highlight the waypoint to be deleted.
3)
Press the CLR Key to display a ‘REMOVE (Wpt Name)?’ confirmation
window.
4)
With ‘OK’ highlighted, press the ENT Key to remove the waypoint. To cancel
the delete request, turn the large FMS Knob to highlight ‘CANCEL’ and press
the ENT Key.
5)
Once all changes have been made, press the FMS Knob to remove the
cursor.
INVERT AND ACTIVATE A STORED FLIGHT PLAN
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
d) Press the EDIT Softkey.
28
1)
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the desired flight plan.
5)
Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key. The selected flight plan is now
inverted and activated. The original flight plan remains intact in its flight plan
catalog storage location.
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Flight Planning
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be copied.
5)
Press the COPY Softkey. A ‘Copy to flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
AFCS
EIS
1)
Nav/Com/
XPDR/Audio
Flight
Instruments
COPY A FLIGHT PLAN
GPS Nav
DELETE A FLIGHT PLAN
Press the FPL Key on the MFD.
2)
Turn the small FMS Knob to select the Flight Plan Catalog Page.
3)
Press the FMS Knob to activate the cursor.
4)
Turn the large FMS Knob to highlight the flight plan to be deleted.
5)
Press the DELETE Softkey. A ‘Delete flight plan #?’ confirmation window is
displayed.
6)
With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel,
turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key.
Flight
Planning
1)
Additional
Features
The default insertion point is at the end of the flight plan. If the selected
waypoint is to be placed anywhere other than the end of the flight plan,
press the FMS Knob to activate the cursor. Waypoints are inserted ABOVE
the cursor. Turn the large FMS Knob to select the desired insertion point.
4)
Press the LD WPT Softkey. The selected waypoint is inserted at the selected
point. The default user waypoint naming is USR000, USR001, USR002, and
so on.
5)
To change the user waypoint name, follow the procedure for modifying a user
waypoint.
29
Index
3)
Appendix
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.
Annun/
Alerts
2)
Abnormal
Operation
Press the FPL Key to display the Active Flight Plan Page on the MFD.
Garmin G1000 Cockpit Reference Guide for the DA40NG
Hazard
Avoidance
1)
190-00953-01 Rev. A
Procedures
GRAPHICAL FLIGHT PLAN CREATION
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 DA40NG
190-00953-01 Rev. A
Procedures
Flight
Instruments
PROCEDURES
LOAD AND ACTIVATE A DEPARTURE PROCEDURE
EIS
3)
Press the ENT Key. The cursor is displayed in the ‘DEPARTURE’ field with a
list of available departures.
4)
Turn the large FMS Knob to highlight the desired departure.
5)
Press the ENT Key. A list of runways may be displayed for the departure. If
so, turn either FMS Knob to select the desired runway.
6)
Press the ENT Key. The cursor is displayed in the ‘TRANSITION’ field with a
list of available transitions.
7)
Turn the large FMS Knob to highlight the desired transition.
8)
Press the ENT Key.
9)
With ‘LOAD?’ highlighted, press the ENT Key. The departure is active when
the flight plan is active.
Flight
Planning
Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’.
Hazard
Avoidance
Press the FPL Key on the MFD to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
departure.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Additional
Features
1)
Abnormal
Operation
Annun/
Alerts
LOAD AN ARRIVAL PROCEDURE
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘SELECT ARRIVAL’.
3)
Press the ENT Key. The cursor is displayed in the ‘ARRIVAL’ field with a list
of available arrivals.
Appendix
1)
31
Index
Garmin G1000 Cockpit Reference Guide for the DA40NG
Procedures
ACTIVATE A DEPARTURE LEG
190-00953-01 Rev. A
GPS Nav
2)
AFCS
Press the PROC Key.
Nav/Com/
XPDR/Audio
1)
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
4)
Turn the large FMS Knob to highlight the desired arrival.
5)
Press the ENT Key. A list of transitions is displayed for the selected arrival.
6)
Turn either FMS Knob to select the desired transition.
7)
Press the ENT Key. A list of runways may be displayed for the selected
arrival.
8)
Turn the large FMS Knob to highlight the desired runway.
9)
Press the ENT Key.
10) With ‘LOAD?’ highlighted, press the ENT Key.
AFCS
11) The arrival becomes part of the active flight plan.
GPS Nav
12) If an altitude associated with a waypoint in an arrival procedure is to be
used to calculate vertical guidance perform the following steps:
a) Press the FMS Knob to activate the cursor.
c) Press the ENT Key to designate the altitude for use in giving vertical
guidance.
ACTIVATE AN ARRIVAL LEG
1)
Press the FPL Key to display the active flight plan.
2)
Press the FMS Knob to activate the cursor.
3)
Turn the large FMS Knob to highlight the desired waypoint within the
arrival.
4)
Press the ACT LEG Softkey. A confirmation window showing the selected
leg is displayed.
5)
With ‘ACTIVATE’ highlighted, press the ENT Key.
LOAD AND/OR ACTIVATE AN APPROACH PROCEDURE
NOTE: Refer to the Aircraft Flight Manual (AFM) to determine if SBAS
functionality is approved.
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
b) Turn the large FMS Knob to highlight the desired waypoint altitude.
Index
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.
32
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Procedures
3)
Press the ENT Key. A list of available approaches for the destination airport
is displayed.
4)
Turn either FMS Knob to highlight the desired approach.
5)
Press the ENT Key. A list of available transitions for the selected approach
procedure is now displayed.
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.
7)
Press the ENT Key. The cursor moves to the MINIMUMS field.
8)
If desired, the DA/MDA for the selected approach procedure may be
entered and displayed on the PFD. Turn the small FMS Knob in the
direction of the green arrow to change the display from OFF to BARO.
9)
Press the ENT Key. The cursor moves to the altitude field. Turn the small
FMS Knob to enter the published DA/MDA for the selected approach
procedure.
AFCS
Turn the large FMS Knob to highlight ‘SELECT APPROACH’.
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
10) Press the ENT Key. ‘LOAD? or ACTIVATE?’ is now displayed with ‘LOAD?’
highlighted.
11) Turn the large FMS Knob to select either ‘LOAD?’ or ‘ACTIVATE?’.
Additional
Features
Selecting ‘LOAD?’ enters the selected approach procedure into the active
flight plan, but is not currently active. Selecting ‘ACTIVATE?’ enters the
selected approach procedure into the active flight plan and activates the
first leg of the approach.
Abnormal
Operation
12) Press the ENT Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’.
3)
Press the ENT Key.
Appendix
Press the PROC Key.
Annun/
Alerts
ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN
1)
Nav/Com/
XPDR/Audio
2)
EIS
Press the PROC Key.
Flight
Instruments
1)
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
33
ACTIVATE A VECTOR TO FINAL APPROACH FIX
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE VECTOR-TO-FINAL’.
3)
Press the ENT Key.
4)
The final approach course becomes the active leg.
ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Procedures
1)
Press the PROC Key.
2)
Turn the large FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’.
3)
Press the ENT Key. A confirmation window is displayed.
4)
With ‘ACTIVATE’ highlighted, press the ENT Key.
Flight
Planning
Or:
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Press the Go-around Switch.
34
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Hazard Avoidance
Flight
Instruments
HAZARD AVOIDANCE
CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP
With the Navigation Map Page displayed, press the MENU Key to display
the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’
option.
2)
Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS
Knob to select ‘Weather’ to customize the display of weather features.
Select ‘Traffic’ to customize the display of traffic.
3)
Press the small FMS Knob to return to the Navigation Map Page.
EIS
1)
AFCS
Procedures
Press the MAP Softkey.
2)
Press the STRMSCP Softkey. Press the STRMSCP Softkey again to remove
Stormscope Lightning Data from the Navigation Map Page.
Additional
Features
Symbol
Abnormal
Operation
Strike is between 6 and 60 seconds old
Annun/
Alerts
Strike is between 1 and 2 minutes old
Strike is between 2 and 3 minutes old
3)
Press the ENT Key.
4)
Turn the small FMS Knob to highlight ‘Weather’.
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index
Turn either FMS Knob to highlight ‘Map Setup’.
Appendix
Select ‘Cell’ or ‘Strike’ as the Stormscope Lightning Mode
2)
Hazard
Avoidance
1)
Press the MENU Key (with the Navigation Map Page displayed).
Flight
Planning
Displaying Stormscope Lightning Data on the Navigation Map Page
1)
GPS Nav
WARNING: The Stormscope system is not intended to be used for hazardous
thunderstorm penetration. Weather information on the G1000 MFD is
approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for
detailed operation.
Lightning Age
Strike is less than 6 seconds old
Nav/Com/
XPDR/Audio
STORMSCOPE® (OPTIONAL)
35
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Hazard Avoidance
5)
Press the ENT Key.
6)
Turn the large FMS Knob to place the cursor in the ‘STRMSCP MODE’ field.
7)
Turn the small FMS Knob to display the ‘Cell/Strike’ window.
8)
Turn either FMS Knob to select ‘Cell’ or ‘Strike’. Press the ENT Key.
9)
Push the FMS Knob to return to the Navigation Map Page.
AFCS
Clear Stormscope Lightning Data from the Navigation Map Page
1)
Press the MENU Key (with the Navigation Map Page displayed).
2)
Turn either FMS Knob to highlight the ‘Clear Stormscope® Lightning’ field
and press the ENT Key.
GPS Nav
NOTE: If heading input is lost, strikes and/or cells must be cleared manually
Flight
Planning
after the execution of each turn. This is to ensure that the strike and/or cell
positions are depicted accurately in relation to the nose of the aircraft.
Procedures
Stormscope Page
1)
Turn the large FMS Knob until the Map Page group is selected.
2)
Turn the small FMS Knob until the Stormscope Page is selected.
1)
Select the Stormscope Page.
2)
Press the MODE Softkey. The CELL and STRIKE Softkeys are displayed.
Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey
to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box
located in the upper left corner of the Stormscope Page.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Change the Stormscope Lightning Mode Between ‘Cell’ and ‘Strike’
Annun/
Alerts
NOTE: “Cell mode” uses a clustering program to identify clusters of electrical
activity that indicate cells.
Appendix
Change the Viewing Mode Between 360˚ and 120˚
1)
Select the Stormscope Page.
2)
Press the VIEW Softkey. The 360 and ARC Softkeys are displayed. Press
the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to
display a 120˚ viewing area.
Index
Press the CLEAR Softkey to remove all Stormscope lightning data from the
display.
36
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Hazard Avoidance
Press the MAP Softkey.
2)
Press the NEXRAD or XM LTNG Softkey to display the desired weather.
Press the applicable softkey again to remove weather data from the
Navigation Map Page.
AFCS
1)
Nav/Com/
XPDR/Audio
Displaying XM Weather on the Navigation Map Page
2)
Turn the small FMS Knob to select the Airport Information Page.
3)
Press the WX Softkey to display METAR and TAF text (METAR and TAF
information is updated every 12 minutes).
Flight
Planning
Turn the large FMS Knob to select the WPT Page Group.
GPS Nav
Display METAR and TAF information on the Airport Information Page
1)
Procedures
Displaying Weather on the Weather Data Link Page
Turn the large FMS Knob to select the Map Page Group.
2)
Turn the small FMS Knob to select the Weather Data Link Page.
3)
Press the available softkeys to select the desired XM weather product.
4)
Press the LEGEND Softkey to view the legends for the selected products. If
necessary, turn either FMS Knob to scroll through the list. Press the small
FMS Knob or the ENT Key to return to the map.
Hazard
Avoidance
1)
Abnormal
Operation
Push in the Joystick to display the panning arrow.
2)
Move the Joystick to place the panning arrow on AIRMETs, TFRs, METARs,
or SIGMETs.
3)
Press the ENT Key to display pertinent information for the selected product.
Appendix
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.
Annun/
Alerts
1)
Index
Garmin G1000 Cockpit Reference Guide for the DA40NG
Additional
Features
Map Panning Information – Weather Data Link Page
190-00953-01 Rev. A
EIS
WARNING: Use of XM weather for hazardous weather penetration is not
recommended. Weather information provided by XM Radio Service is
approved only for weather avoidance, not penetration.
Flight
Instruments
XM WEATHER (OPTIONAL)
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) (TAS only, 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
Appendix
NOTE: If the G1000 is configured to use an optional Traffic Advisory System
(TAS), TIS is not available for use.
Index
Traffic Information Service (TIS)
NOTE: Traffic Information Service (TIS) is only available when the aircraft is
within the service volume of a TIS capable terminal radar site.
38
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Hazard Avoidance
Turn the small FMS Knob to select the Traffic Map Page.
3)
Press the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is
displayed in the Traffic Mode field.
4)
Press the STANDBY Softkey to place the system in the Standby Mode.
‘STANDBY’ is displayed in the Traffic Mode field.
5)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
6)
Press the TNA MUTE Softkey to mute the “Traffic Not Available” aural
alert.
AFCS
2)
Nav/Com/
XPDR/Audio
Turn the large FMS Knob to select the Map Page Group.
EIS
1)
Flight
Instruments
Displaying Traffic on the Traffic Map Page
GPS Nav
Displaying Traffic on the Navigation Map
Ensure TIS is operating. With the Navigation Map displayed, press the
MAP Softkey.
2)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
Flight
Planning
1)
Procedures
Traffic Advisory System (TAS) (Optional)
Turn the small FMS Knob to select the Traffic Map Page. ‘OPERATING’ is
displayed in the Traffic Mode field.
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.
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.
Annun/
Alerts
2)
Abnormal
Operation
Turn the large FMS Knob to select the Map Page Group.
Additional
Features
1)
Hazard
Avoidance
Displaying Traffic on the Traffic Map Page
Appendix
Displaying Traffic on the Navigation Map
Ensure TAS is operating.
2)
With the Navigation Map displayed, press the MAP Softkey.
3)
Press the TRAFFIC Softkey. Traffic is now displayed on the map.
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index
1)
39
TERRAIN AND OBSTACLE PROXIMITY
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
EIS
Flight
Instruments
Hazard Avoidance
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.
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.
4)
Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area.
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
Displaying Terrain and Obstacles on the Terrain Proximity Page
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.
Abnormal
Operation
Additional
Features
Displaying Terrain and Obstacles on the Navigation Map
1)
With the Navigation Map displayed, press the MAP Softkey.
2)
Press the TERRAIN Softkey. Terrain and obstacle proximity will now be
displayed on the map.
TERRAIN-SVS
NOTE: Terrain-SVS is only available when the Synthetic Vision System (SVS)
option is installed.
Appendix
Annun/
Alerts
Color
Index
NOTE: Terrain data is not displayed when the aircraft latitude is greater than
75 degrees north or 60 degrees south.
40
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Hazard Avoidance
2)
Turn the small FMS Knob to select the Terrain-SVS Page.
3)
If desired, press the VIEW Softkey to access the ARC and 360 softkeys.
When the ARC Softkey is selected, a radar-like 120° view is displayed.
Press the 360 Softkey to return to the 360° default display.
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.
Flight
Planning
Red
GPS Nav
Terrain/Obstacle Location
AFCS
Color
Nav/Com/
XPDR/Audio
Turn the large FMS Knob to select the Map Page Group.
EIS
1)
Flight
Instruments
Display Terrain on the TERRAIN-SVS Page
Procedures
Enable/Disable Aviation Data
While the Terrain-SVS Page is displayed, press the MENU Key.
2)
Turn the small FMS Knob to select “Show (or Hide) Aviation Data”.
3)
Press the ENT Key.
Hazard
Avoidance
1)
Additional
Features
Terrain-SVS Inhibit
Abnormal
Operation
Inhibit Terrain Alerting
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.
Annun/
Alerts
Appendix
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index
Enable Terrain Alerting
While the Terrain-SVS Page is displayed, press the INHIBIT Softkey.
Or:
41
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.
EIS
Flight
Instruments
Hazard Avoidance
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
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.
42
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Additional Features
Flight
Instruments
ADDITIONAL FEATURES
SYNTHETIC VISION
EIS
Nav/Com/
XPDR/Audio
WARNING: Use appropriate primary systems for navigation, and for terrain,
obstacle, and traffic avoidance. SVS is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which
to solely base decisions and/or plan maneuvers to avoid terrain, obstacles,
or traffic.
AFCS
Additional
Features
Abnormal
Operation
Annun/
Alerts
Press the SYN VIS Softkey.
3)
Press the SYN TERR Softkey.
4)
Press the BACK Softkey to return to the previous page.
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index
2)
Appendix
Displaying SVS Terrain
Press the PFD Softkey.
Hazard
Avoidance
Pathways
Flight Path Marker
Horizon Heading Marks
Terrain and Obstacle Alerting
Three-dimensional Traffic
Airport Signs
Runway Display
1)
Procedures
•
•
•
•
•
•
•
Flight
Planning
Synthetic Vision System (SVS) functionality is offered as an optional enhancement
to the G1000 Integrated Flight Deck System.
SVS is primarily comprised of a computer-generated forward-looking, attitude
aligned view of the topography immediately in front of the aircraft from the pilot’s
perspective. SVS information is shown on the primary flight display (PFD).
SVS offers a three-dimensional view of terrain and obstacles. Terrain and
obstacles that pose a threat to the aircraft in flight are shaded yellow or red.
In addition to SVS enhancement to the PFD, the following feature enhancements
have been added to the PFD:
GPS Nav
WARNING: Do not use SVS runway depiction as the sole means for
determining the proximity of the aircraft to the runway or for maintaining
the proper approach path angle during landing.
43
Additional Features
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Displaying Pathways
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the PATHWAY Softkey.
5)
Press the BACK Softkey to return to the previous page.
AFCS
GPS Nav
Flight
Planning
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the HRZN HDG Softkey.
5)
Press the BACK Softkey to return to the previous page.
Procedures
Displaying Airport Signs
Hazard
Avoidance
Additional
Features
Press the PFD Softkey.
Displaying Heading on the Horizon
1)
Press the PFD Softkey.
2)
Press the SYN VIS Softkey.
3)
If not already enabled, press the SYN TERR Softkey.
4)
Press the APTSIGNS Softkey.
5)
Press the BACK Softkey to return to the previous page.
TERMINAL PROCEDURE CHARTS
NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may
be necessary to carry another source of charts on-board the aircraft.
Abnormal
Operation
Annun/
Alerts
Appendix
Index
1)
SafeTaxi®
SafeTaxi® is an enhanced feature that gives greater map detail as the map range
is adjusted in on the airport. The airport display on the map reveals runways with
numbers, taxiways identifiers, and airport landmarks including ramps, buildings,
control towers, and other prominent features. Resolution is greater at lower map
ranges. The aircraft symbol provides situational awareness while taxiing.
Pressing the DCLTR Softkey (declutter) once removes the taxiway markings and
airport identification labels. Pressing the DCLTR Softkey twice removes VOR station
ID, the VOR symbol, and intersection names if within the airport plan view. Pressing
44
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 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)
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.
Press the SHW CHRT Softkey when displayed.
Or:
3)
Press the GO BACK Softkey to return to the previous page.
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index
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.
Appendix
2)
Annun/
Alerts
Move the map pointer to point to a desired point on the map and press the
SHW CHRT Softkey.
45
Additional Features
Nav/Com/
XPDR/Audio
EIS
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.
2)
Turn the large FMS Knob to select the departure airport, destination
airport, departure, arrival, or approach.
3)
Press the SHW CHRT Softkey. The appropriate chart is displayed, if
available for the item selected.
4)
Press the GO BACK Softkey to return to the previous page.
1)
While viewing a chart press the MENU Key to display the Page Menu
OPTIONS.
2)
Turn the large FMS Knob to highlight the ‘Chart Setup’ Menu Option and
press the ENT Key.
3)
Turn the large FMS Knob to move between the ‘FULL SCREEN’ and ‘COLOR
SCHEME’ Options.
4)
Turn the small FMS Knob to choose between the ‘On’ and ‘Off’ Full Screen
Options.
5)
Turn the small FMS Knob to choose between ‘Day’, ‘Auto’, and ‘Night’
Options.
6)
In Auto Mode, turn the large FMS Knob to select the percentage field and
change percentage with the small FMS Knob. The percentage of change is
the day/night crossover point based on backlighting intensity.
7)
Press the FMS Knob when finished to remove the Chart Setup Menu.
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Change Day/Night View
XM® RADIO ENTERTAINMENT
The XM® Radio Page provides information and control of the audio entertainment
features of the XM Satellite Radio.
Index
Appendix
Selecting the XM Radio Page
46
1)
Turn the large FMS Knob to select the Auxiliary Page Group.
2)
Turn the small FMS Knob to select the displayed AUX - XM Information
Page.
3)
Press the RADIO Softkey to show the XM Radio Page where audio
entertainment is controlled.
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 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
Hazard
Avoidance
Press the CH + Softkey to go up through the list in the Channel Box, or
move down the list with the CH – Softkey.
Procedures
2)
Or:
Additional
Features
Press the FMS Knob to highlight the channel list and turn the large FMS
Knob to scroll through the channels.
3)
With the desired channel highlighted, press the ENT Key.
Press the DIR CH Softkey. The channel number in the Active Channel Box
is highlighted.
3)
Press the numbered softkeys located on the bottom of the display to
directly select the desired channel number.
4)
Press the ENT Key to activate the selected channel.
Appendix
2)
Annun/
Alerts
While on the XM Radio Page, press the CHNL Softkey.
Abnormal
Operation
Entering a Channel Directly
1)
Flight
Planning
While on the XM Radio Page, press the CHNL Softkey.
GPS Nav
1)
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) Press the CATGRY Softkey on the XM Radio Page.
2) Press the CAT + and CAT - Softkeys to cycle through the categories.
Or:
Turn the small FMS Knob to display the ‘Categories’ list. Highlight the
desired category with the small FMS Knob.
3) Press the ENT Key.
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
47
Additional Features
Flight
Instruments
Assigning Channel Presets
GPS Nav
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, press the PRESETS
Softkey to access the first five preset channels (PS1 - PS5).
2) Press the MORE Softkey to access the next five channels (PS6 – PS10),
and again to access the last five channels (PS11 – PS15). Pressing the
MORE Softkey repeatedly cycles through the preset channels.
3) Press any one of the (PS1 - PS15) softkeys to assign a number to the
active channel.
4) Press the SET Softkey on the desired channel number to save the channel
as a preset.
1)
On the XM Radio Page, press the RADIO Softkey.
2)
Press the VOL Softkey to access the volume control softkeys.
3)
Press VOL + or VOL - softkeys to adjust the volume level.
4)
Press the MUTE Softkey to mute the radio audio.
ELECTRONIC CHECKLISTS (OPTIONAL)
The system accesses the checklists from an SD card inserted into the card slot.
If the SD card contains an invalid checklist file or no checklist, the Power-up Page
messages display ‘Checklist File: Invalid’ or ‘Checklist File: N/A’ (not available) and the
CHKLIST Softkey is not available.
Accessing and Navigating Checklists
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
Adjusting Volume
48
1)
From any page on the MFD, select the CHKLIST Softkey or turn the large
FMS Knob to select the Checklist Page.
2)
Turn the large FMS Knob to select the ‘GROUP’ field.
3)
Turn the small FMS Knob to select the desired procedure and press the
ENT Key.
4)
Turn the large FMS Knob to select the ‘CHECKLIST’ field.
5)
Turn the small FMS Knob to select the desired checklist and press the ENT
Key. The selected checklist item is indicated with white text surrounded by
a white box.
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Additional Features
Press the ENT Key or select the DONE Softkey to check the selected
checklist item. The line item turns green and a checkmark is placed in the
associated box. The next line item is automatically selected for checking.
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
Flight
Instruments
6)
Nav/Com/
XPDR/Audio
When all checklist items have been checked, ‘*Checklist Finished*’ is
displayed in green text at the bottom left of the checklist window and
‘GO TO NEXT CHECKLIST?’ is highlighted. If ‘GO TO NEXT CHECKLIST?’
is selected prior to checking all the checklist items, ‘*CHECKLIST NOT
FINISHED*’ will be displayed in yellow text.
8)
Press the ENT Key. If ‘GO TO NEXT CHECKLIST?’ is displayed when
pressing the ENT Key, the next checklist in the group will be displayed. If
‘EXIT CHECKLISTS?’ is displayed when pressing the ENT Key, the system
will exit the Checklist Page.
9)
Select the EXIT Softkey to exit the Checklist Page and return to the page
last viewed. When returning to the Checklist Page after pressing the EXIT
Softkey, the system will return to the last select checklist item.
AFCS
7)
GPS Nav
Flight
Planning
Hazard
Avoidance
Select the EMERGCY Softkey.
3)
Turn the FMS Knob to select the desired emergency checklist and press the
ENT Key.
4)
Press the ENT Key or select the DONE Softkey to check the selected
emergency checklist item. The line item turns green and a checkmark is
placed in the box next to it. The next line item is automatically highlighted
for checking.
Index
Press the CLR Key or select the UNDO Softkey to remove a check mark
from an item.
When all checklist items have been checked, ‘*Checklist Finished*’ is
displayed in green text at the bottom left of the checklist window and
Garmin G1000 Cockpit Reference Guide for the DA40NG
Appendix
Either FMS Knob can be used to scroll through the checklist and select the
desired checklist item.
Annun/
Alerts
2)
Abnormal
Operation
From any page on the MFD, select the CHKLIST Softkey or turn the large
FMS Knob to select the Checklist Page.
Additional
Features
1)
190-00953-01 Rev. A
Procedures
Immediately Accessing Emergency Procedures
5)
EIS
Press the CLR Key or select the UNDO Softkey to remove a check mark
from an item.
49
Additional Features
6)
Press the ENT Key to advance to the next checklist.
7)
Select the RETURN Softkey to return to the previous checklist.
8)
Select the EXIT Softkey to exit the Checklist Page and return to the page
last viewed.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
‘GO TO NEXT CHECKLIST?’ is highlighted. If ‘GO TO NEXT CHECKLIST?’
is selected prior to checking all the checklist items, ‘*CHECKLIST NOT
FINISHED*’ will be displayed in yellow text.
50
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 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
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
NOTE: The Diamond DA40NG Airplane Flight Manual (AFM) always takes
precedence over the information found in this section.
Abnormal
Operation
Annun/
Alerts
Loss of Hazard Functions with Loss of GPS
Position
Appendix
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
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
Extreme Pitch Indication
DEAD RECKONING
While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS
solution or is unable to calculate a GPS position, the system automatically reverts to
Dead Reckoning (DR) Mode. In DR Mode, the G1000 uses its last-known position
combined with continuously updated airspeed and heading data (when available) to
calculate and display the aircraft’s current estimated position.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
52
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Abnormal Operation
EIS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’
superimposed in yellow over the ‘own aircraft’ symbol as shown in the following
figure. In addition, ‘DR’ is prominently displayed, also in yellow, on the HSI slightly
above and to the right of the aircraft symbol on the CDI as shown in the following
figure. 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.
Flight
Instruments
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.
Annun/
Alerts
Appendix
CDI ‘DR’ Indication on PFD
Symbolic Aircraft
(Map pages and Inset Map)
Index
Dead Reckoning Indications
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
53
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 Terrain-SVS and Terrain Proximity are disabled. Additionally, the accuracy of
all nearest information (airports, airspaces, and waypoints) is questionable. Finally,
airspace alerts continue to function, but with degraded accuracy.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Abnormal Operation
54
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Flight
Instruments
ANNUNCIATIONS & ALERTS
WARNING ANNUNCIATION
AFCS
Continuous
Aural Tone
GPS Nav
Flight
Planning
Procedures
Engine oil pressure is less than 0.9 bar.
Engine coolant temp is >105 deg. C.
Engine oil tem is greater than 140 deg. C.
Left fuel temp is greater than 60 deg. C.
Right fuel temp is greater than 60 deg. C.
Engine gearbox temp is >120 deg. C.
Engine alternator has failed.
Engine alternator output is >70 amps.
Engine starter is engaged.
Front or rear door is not closed.
Autopilot automatic trim is inoperative.
Engine fuel pressure is low.
Audio
Alert
Nav/Com/
XPDR/Audio
OIL PRES
ENG TEMP
OIL TEMP
L FUEL TEMP
R FUEL TEMP
GBOX TEMP
ALTN FAIL
ALTN AMPS
STARTER
DOOR OPEN
AP TRIM FAIL*
FUEL PRESS
Alerts Window Message
EIS
Annunciation Text
* Optional (KAP 140 equipped aircraft only)
Hazard
Avoidance
CAUTION ANNUNCIATION
Single
Aural Tone
Annun/
Alerts
Appendix
Engine ECU A has failed.
Engine ECU B has failed.
Left fuel quantity is low.
Bus voltage is less than 25 volts.
Engine coolant level is low.
Pitot heat has failed.
Pitot heat is off.
Audio
Alert
Abnormal
Operation
ECU A FAIL
ECU B FAIL
FUEL LOW
VOLTS LOW
COOL LVL
PITOT FAIL
PITOT HT OFF
Alerts Window Message
Additional
Features
Annunciation Text
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
55
ADVISORY ANNUNCIATION
Annunciation Text
GLOW ON
FUEL XFER
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.
None
Audio
Alert
None
AFCS ALERTS
Condition
Annunciation Description
Pitch Failure
Pitch axis control failure. AP is inoperative.
Roll Failure
Roll axis control failure. AP is inoperative.
MET Switch Stuck, or
Pitch Trim Axis Control
Failure
If annunciated when AP is engaged, take control
of the aircraft and disengage the autopilot. If
annunciated when AP is not engaged, move each
half of the MET switch separately to check if a
stuck switch is causing the annunciation.
AP and MET are unavailable. FD may still be
available.
A condition has developed causing the pitch
servo to provide a sustained force. Be prepared
to apply nose up control wheel force upon
autopilot disconnect.
A condition has developed causing the pitch
servo to provide a sustained force. Be prepared
to apply nose down control wheel force upon
autopilot disconnect.
System Failure
Elevator Mistrim Up
Annun/
Alerts
Abnormal
Operation
Audio
Alert
ALERT MESSAGE
Elevator Mistrim Down
Index
Appendix
Alerts Window Message
Engine glow plug active.
Fuel transfer in progress.
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
56
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Annunciation Description
Aileron Mistrim Left
Flight
Planning
MFD
Pop-Up Alert
Aural
Message
Procedures
Alert Type
PFD/MFD
TERRAIN-SVS
Page
Annunciation
“Warning; Terrain,
Terrain”
Imminent Terrain Impact
Warning (ITI)
“Warning; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Warning (ROC)
“Warning; Obstacle,
Obstacle”
Imminent Obstacle Impact
Warning (IOI)
“Warning; Obstacle,
Obstacle”
Reduced Required Terrain
Clearance Caution (RTC)
“Caution; Terrain,
Terrain”
Imminent Terrain Impact
Caution (ITI)
“Caution; Terrain,
Terrain”
Reduced Required Obstacle
Clearance Caution (ROC)
“Caution; Obstacle,
Obstacle”
Imminent Obstacle Impact
Caution (IOI)
“Caution; Obstacle,
Obstacle”
Additional
Features
Abnormal
Operation
Annun/
Alerts
Index
57
Appendix
Garmin G1000 Cockpit Reference Guide for the DA40NG
Hazard
Avoidance
Reduced Required Terrain
Clearance Warning (RTC)
190-00953-01 Rev. A
GPS Nav
TERRAIN-SVS ALERTS
AFCS
Preflight Test
Nav/Com/
XPDR/Audio
Aileron Mistrim Right
EIS
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
Flight
Instruments
Annunciations & Alerts
TERRAIN-SVS SYSTEM STATUS ANNUNCIATIONS
PFD/MFD
TERRAIN-SVS Page
Annunciation
EIS
Alert Type
Aural Message
“Terrain System Failure”
Terrain Alerting is disabled
None
No GPS position or excessively
degraded GPS signal
“Terrain System Not Available”
“Terrain System Available” will
be heard when sufficient GPS
signal is received.
None
System Test in progress
System Test pass
Additional
Features
Abnormal
Operation
“Terrain System Test OK”
Voice Alert
“Minimums, minimums”
“Vertical track”
“Traffic”
“Traffic Not Available”
“Traffic, Traffic”
“Traffic Advisory System
Test Passed”
“Traffic Advisory System
Test Failed”
Description
The aircraft has descended below the preset barometric minimum
descent altitude.
The aircraft is one minute from Top of Descent. Issued only when
vertical navigation is enabled.
Played when a Traffic Advisory (TA) is issued.
The aircraft is outside the Traffic Information Service (TIS) coverage area.
Played when a Traffic Advisory (TA) is issued (TAS system).
Played when the TAS system passes a pilot-initiated self test.
Played when the TAS system fails a pilot-initiated self test.
Index
Appendix
Annun/
Alerts
None
VOICE ALERTS
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
System Test fail
58
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Hazard
Avoidance
Additional
Features
Abnormal
Operation
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.
Annun/
Alerts
Appendix
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.
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index
190-00953-01 Rev. A
The PFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.
The MFD configuration settings do not match
backup configuration memory. The G1000
system should be serviced.
The MFD and PFDs have different software
versions installed. The G1000 system should be
serviced.
Procedures
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.
The PFD and/or MFD has incorrect software
installed. The G1000 system should be serviced.
Flight
Planning
SW MISMATCH – GDU software
version mismatch. Xtalk is off.
The PFD and/or MFD self-test has detected a
problem. The G1000 system should be serviced.
GPS Nav
MFD1 CONFIG – MFD1 config
error. Config service req’d.
AFCS
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.
Nav/Com/
XPDR/Audio
XTALK ERROR – A flight display
crosstalk error has occurred.
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.
EIS
Message
DATA LOST – Pilot stored data
was lost. Recheck settings.
Flight
Instruments
MFD & PFD MESSAGE ADVISORIES
59
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MFD & PFD MESSAGE ADVISORIES (CONT.)
Message
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 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.
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
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.
MFD1 DB ERR – MFD1 terrain
database error exists.
PFD1 DB ERR – PFD1 terrain
database error exists.
MFD1 DB ERR – MFD1 terrain
database missing.
PFD1 DB ERR – PFD1 terrain
database missing.
MFD1 DB ERR – MFD1 obstacle
database error exists.
PFD1 DB ERR – PFD1 obstacle
database error exists.
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.
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.
The terrain database is present on another LRU,
but is missing on the specified LRU.
The MFD and/or PFD detected a failure in the
obstacle database. Ensure that the data card is
properly inserted. Replace data card. If problem
persists, The G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
The obstacle database is present on another LRU,
but is missing on the specified LRU.
Nav/Com/
XPDR/Audio
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.
AFCS
Annun/
Alerts
Appendix
Index
61
Abnormal
Operation
Garmin G1000 Cockpit Reference Guide for the DA40NG
Additional
Features
190-00953-01 Rev. A
Hazard
Avoidance
The MFD and/or PFDs detected a failure in the
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.
Procedures
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.
Flight
Planning
The airport terrain database is present on
another LRU, but is missing on the specified LRU.
GPS Nav
MFD1 DB ERR – MFD1 airport
terrain database missing.
PFD1 DB ERR – PFD1 airport
terrain database missing.
MFD1 DB ERR – MFD1 Safe Taxi
database error exists.
PFD1 DB ERR – PFD1 Safe Taxi
database error exists.
MFD1 DB ERR – MFD1 Chartview
database error exists.
Comments
EIS
Message
MFD1 DB ERR – MFD1 obstacle
database missing.
PFD1 DB ERR – PFD1 obstacle
database missing.
MFD1 DB ERR – MFD1 airport
terrain database error exists.
PFD1 DB ERR – PFD1 airport
terrain database error exists.
Flight
Instruments
DATABASE 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
DATABASE MESSAGE ADVISORIES (CONT.)
Message
DB MISMATCH – Aviation
database type mismatch. Xtalk is
off.
Comments
The PFDs and MFD have different aviation
database types installed (Americas, European,
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.
GMA 1347 MESSAGE ADVISORIES
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.
62
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Message
Flight
Instruments
GIA 63 MESSAGE ADVISORIES
Comments
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
EIS
AFCS
The GIA1 and/or GIA2 have an error in the audio
configuration. The G1000 system should be
serviced.
Nav/Com/
XPDR/Audio
GPS Nav
The GIA1 and/or GIA2 temperature is too low
to operate correctly. Allow units to warm up to
operating temperature.
Flight
Planning
The GIA1 and/or GIA2 temperature is too high.
If problem persists, the G1000 system should be
serviced.
Procedures
Hazard
Avoidance
The GIA1 and/or GIA2 self-test has detected a
problem in the unit. The G1000 system should
be serviced.
Additional
Features
The GIA1 and/or GIA 2 has incorrect software
installed. The G1000 system should be serviced.
Abnormal
Operation
Appendix
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.
Annun/
Alerts
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
GIA1 CONFIG – GIA1 audio config
error. Config service req’d.
GIA2 CONFIG – GIA2 audio config
error. Config service req’d.
GIA1 COOLING – GIA1 temperature
too low.
GIA2 COOLING – GIA2 temperature
too low.
GIA1 COOLING – GIA1 over
temperature.
GIA2 COOLING – GIA2 over
temperature.
GIA1 SERVICE – GIA1 needs service.
Return the unit for repair.
GIA2 SERVICE – GIA2 needs service.
Return the unit for repair.
MANIFEST – 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.
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
63
GIA 63 MESSAGE ADVISORIES (CONT.)
Message
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.
Comments
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
Loss of GPS integrity monitoring.
other NAVS.
Loss of GPS navigation due to insufficient satelGPS NAV LOST – Loss of GPS
lites.
navigation. Insufficient satellites.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to position error.
navigation. Position error.
GPS NAV LOST – Loss of GPS
Loss of GPS navigation due to GPS failure.
navigation. GPS fail.
ABORT APR – Loss of GPS navigation.
Abort approach due to loss of GPS navigation.
Abort approach.
TRUE APR – True north approach.
Displayed after passing the first waypoint of
Change hdg reference to TRUE.
a true north approach when the nav angle is
set to ‘AUTO’.
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
64
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Message
GPS1 FAIL – GPS1 is inoperative.
Comments
A failure has been detected in the GPS1
and/or GPS2 receiver. The receiver may still
be available. The G1000 system should be
serviced.
Nav/Com/
XPDR/Audio
AFCS
A failure has been detected in the NAV1
and/or NAV2 receiver. The receiver may still
be available. The G1000 system should be
serviced.
GPS Nav
Abnormal
Operation
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.
Additional
Features
G/S1 SERVICE – G/S1 needs service.
Return unit for repair.
G/S2 SERVICE – G/S2 needs service.
Return unit for repair.
Hazard
Avoidance
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.
Procedures
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.
Flight
Planning
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.
EIS
A failure has been detected in the GPS1 and/or
GPS2 receiver. The receiver is unavailable. The
G1000 system should be serviced.
GPS2 FAIL – GPS2 is inoperative.
G/S1 FAIL – G/S1 is inoperative.
Flight
Instruments
GIA 63 MESSAGE ADVISORIES (CONT.)
GIA 63W MESSAGE ADVISORIES
Comments
The GIA1 and/or GIA2 configuration settings do
not match backup configuration memory. The
G1000 system should be serviced.
Index
Garmin G1000 Cockpit Reference Guide for the DA40NG
Appendix
190-00953-01 Rev. A
Annun/
Alerts
Message
GIA1 CONFIG – GIA1 config error.
Config service req’d.
GIA2 CONFIG – GIA2 config error.
Config service req’d.
65
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
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.
COM1 TEMP – COM1 over temp.
Reducing transmitter power.
COM2 TEMP – COM2 over temp.
Reducing transmitter power.
66
Comments
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.
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.
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Comments
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
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.
TRUE APR – True north approach. Displayed after passing the first waypoint of a
Change HDG reference to TRUE.
true north approach when the nav angle is set
to ‘AUTO’.
Nav/Com/
XPDR/Audio
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.
EIS
Message
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
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
67
GIA 63W MESSAGE ADVISORIES (CONT.)
Message
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
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
G1000 system should be serviced.
MANIFEST – GEA1 software
The #1 GEA 71 has incorrect software installed.
mismatch, communication halted. 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
68
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Flight
Planning
Procedures
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.
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.
GPS Nav
Message
AHRS1 TAS – AHRS1 not receiving
valid airspeed.
AFCS
GRS 77 MESSAGE ADVISORIES
Nav/Com/
XPDR/Audio
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.
EIS
Message
XPDR1 CONFIG – XPDR1 config
error. Config service req’d.
Flight
Instruments
GTX 33 MESSAGE ADVISORIES
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
69
GRS 77 MESSAGE ADVISORIES (CONT.)
Message
Comments
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.
Annun/
Alerts
Appendix
Index
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.
GDL 69A MESSAGE ADVISORIES
Message
GDL69 CONFIG – GDL 69 config
error. Config service req’d.
GDL69 FAIL – GDL 69 has failed.
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MANIFEST – GDL software
mismatch, communication halted.
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.
GDC 74A MESSAGE ADVISORIES
Message
MANIFEST – GDC1 software
mismatch, communication halted.
70
Comments
The GDC 74A has incorrect software installed.
The G1000 system should be serviced.
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Comments
Upon power-up, the 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.
DB CHANGE – Database changed. This occurs when a stored flight plan contains
Verify user modified procedures.
procedures that have been manually edited.
This alert is issued only after an aviation
database update. Verify that the user-modified
procedures in stored flight plans are correct and
up to date.
DB CHANGE – Database changed. This occurs when a stored flight plan contains
Verify stored airways.
an airway that is no longer consistent with
the aviation database. This alert is issued only
after an aviation database update. Verify use
of airways in stored flight plans and reload
airways as needed.
EIS
Message
FPL WPT LOCK – Flight plan
waypoint is locked.
Flight
Instruments
MISCELLANEOUS MESSAGE ADVISORIES
Index
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
71
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Annunciations & Alerts
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message
FPL TRUNC – Flight plan has been
truncated.
Comments
This occurs when a newly installed aviation
database eliminates an obsolete approach
or arrival used by a stored flight plan. The
obsolete procedure is removed from the flight
plan. Update flight plan with current arrival or
approach.
LOCKED FPL – Cannot navigate
This occurs when the pilot attempts to activate
locked flight plan.
a stored flight plan that contains locked
waypoint. Remove locked waypoint from flight
plan. Update flight plan with current waypoint.
WPT ARRIVAL – Arriving at
Arriving at waypoint [xxxx], where [xxxx] is the
waypoint -[xxxx]
waypoint name.
STEEP TURN – Steep turn ahead.
A steep turn is 15 seconds ahead. Prepare to
turn.
INSIDE ARSPC – Inside airspace.
The aircraft is inside the airspace.
ARSPC AHEAD – Airspace ahead
Special use airspace is ahead of aircraft. The
less than 10 minutes.
aircraft will penetrate the airspace within 10
minutes.
ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the
ahead.
aircraft position.
ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the
than 2 nm.
aircraft position.
APR INACTV – Approach is not
The system notifies the pilot that the loaded
active.
approach is not active. Activate approach when
required.
SLCT FREQ – Select appropriate
The system notifies the pilot to load the
frequency for approach.
approach frequency for the appropriate NAV
receiver. Select the correct frequency for the
approach.
SLCT NAV – Select NAV on CDI for The system notifies the pilot to set the CDI to
approach.
the correct NAV receiver. Set the CDI to the
correct NAV receiver.
72
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Annunciations & Alerts
Additional
Features
Abnormal
Operation
Annun/
Alerts
Appendix
Index
73
Hazard
Avoidance
Garmin G1000 Cockpit Reference Guide for the DA40NG
Procedures
190-00953-01 Rev. A
Flight
Planning
STRMSCP FAIL – Stormscope has
failed.
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.
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.
GPS Nav
TRAFFIC FAIL – Traffic device has
failed.
Invalid leg type for parallel offset.
AFCS
VNV – Unavailable. Excessive track
angle error.
VNV – Unavailable. Excessive
crosstrack error.
VNV – Unavailable. Parallel course
selected.
NO WGS84 WPT – Non WGS 84
waypoint for navigation -[xxxx]
Bad parallel track geometry.
Nav/Com/
XPDR/Audio
VNV – Unavailable. Unsupported
leg type in flight plan.
Comments
EIS
Message
PTK FAIL – Parallel track unavailable:
bad geometry.
PTK FAIL – Parallel track unavailable:
invalid leg type.
PTK FAIL – Parallel track unavailable:
past IAF.
UNABLE V WPT – Can’t reach
current vertical waypoint.
Flight
Instruments
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message
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
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 DA40NG
190-00953-01 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
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
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 STD BARO or
BACK Softkey to return to
the top-level softkeys
360 HSI
Annun/
Alerts
METERS
BACK
ARC HSI
IN
HPA
ALERTS
ALERTS
Appendix
ALERTS
Index
PATHWAY
SYN TERR HRZN HDG APTSIGNS
ALERTS
PFD Configuration Softkeys
76
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 Rev. A
Appendix
SYN VIS
Procedures
Hazard
Avoidance
Additional
Features
Wind direction arrow with direction
and speed
Information not displayed
HSI FRMT
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
77
Index
360 HSI
ARC HSI
Displays the HSI formatting softkeys
Displays the HSI in a 360 degree format
Displays the HSI in an arc format
Appendix
frequency.
Annun/
Alerts
Displays the DME Information Window
Cycles the Bearing 1 Information
Window through NAV1 or GPS/
waypoint identifier and GPS-derived
distance information, and ADF/
DME
BRG1
Abnormal
Operation
OFF
Flight
Planning
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
EIS
Flight
Instruments
BRG2
Nav/Com/
XPDR/Audio
ALT UNIT
AFCS
IN
Press to display the BARO setting as
inches of mercury
GPS Nav
METERS
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
When enabled, displays altimeter in
meters
HPA
Press to display the BARO setting as
hectopacals
Procedures
Flight
Planning
STD BARO
Sets barometric pressure to 29.92 in Hg
(1013 hPa)
Hazard
Avoidance
ADF/DME
ALERTS
Additional
Features
Press the BACK Softkey to return
to the top-level softkeys.
Abnormal
Operation
ALERTS
Press the BACK Softkey to return
to the previous level softkeys.
Annun/
Alerts
Transponder Softkeys
Displays transponder mode selection softkeys
XPDR
STBY
ON
Index
Appendix
ALERTS
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 DA40NG
190-00953-01 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
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
79
MFD SOFTKEY MAP
DCLTR
MAP
ENGINE
EIS
Flight
Instruments
Appendix
SHW CHRT
CHKLIST
(optional)
(optional)
DCLTR-1
Nav/Com/
XPDR/Audio
DCLTR-2
DCLTR-3
TOPO
TERRAIN
AFCS
TRAFFIC
ENGINE
SYSTEM
(Default softkey
is dependant on
the selection made
in the map setup
options)
AIRWAYS
Press the BACK Softkey on this
level to return to the top softkey level.
(optional)
(optional)
(optional)
STRMSCP
NEXRAD
XM LTNG
BACK
AIRWY ON
FUEL
GPS Nav
AIRWY LO
AIRWAY HI
Flight
Planning
DEC FUEL
The DONE Softkey changes to UNDO when the checklist
item is already checked
Procedures
DONE
EXIT
EMERGCY
MFD Softkeys
Displays the defualt Engine Display
ENGINE
Additional
Features
Hazard
Avoidance
RST FUEL
ENGINE
SYSTEM
Displays the SYSTEM Display
FUEL
Displays the FUEL Display
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 DA40NG
190-00953-01 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
190-00953-01 Rev. A
Garmin G1000 Cockpit Reference Guide for the DA40NG
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 DA40NG
190-00953-01 Rev. A
Index
Edit a flight plan 27
Electronic checklists 49, 50
Emergency checklist 49
Enable Terrain 41, 42
Endurance 6
FD 56
Flight Director 13
Flight path marker 43
FliteCharts® 44, 45
Frequency Transfer 10
Fuel remaining 6, 7
Fuel used 6
Flight
Planning
H
I
Inhibit 41
Inhibit Terrain 41
Inset Map 75, 76
IOI 57
Hazard
Avoidance
Additional
Features
J
Jeppesen 45
Abnormal
Operation
CDI 1, 10, 72
Cell 35, 36
Cell mode 36
Channel Presets 48
ChartView 44, 45
Checklists 48–49
Clearance player 10
Clearance Recorder 10
Code selection softkeys 9
COM 10, 51
Procedures
Horizon heading 43
C
L
M
Map panning 37
Message advisories 59–62, 64–74
MET 56
METAR 37
Minimums 58
Garmin G1000 Cockpit Reference Guide for the DA40NG
Index-1
Index
DCLTR Softkey 44
Dead Reckoning 52
Declutter 52, 75, 81
Direct-to 17
DME 9, 10
DR mode 52, 53, 54
Appendix
Lightning 35, 36, 76
Annun/
Alerts
D
190-00953-01 Rev. A
GPS Nav
Barometric Altitude Minimums 3
Barometric pressure 78
F
AFCS
B
Nav/Com/
XPDR/Audio
Activate a flight plan 18
Active Channel 47
ADF 9, 10, 52, 77, 78
AHRS 69, 70
Airport Signs 43, 44
Airways 81
AP 56
Audio panel controls
NAV1, NAV2 10
Autopilot 56
Aviation database 19, 20, 60, 61, 62,
71, 72
EIS
E
Flight
Instruments
A
Index
Appendix
Annun/
Alerts
Abnormal
Operation
Additional
Features
Hazard
Avoidance
Procedures
Flight
Planning
GPS Nav
AFCS
Nav/Com/
XPDR/Audio
EIS
Flight
Instruments
Index
Mistrim 56, 57
MKR/MUTE 10
Mode S 79
Mode selection softkeys 9
Multi Function Display (MFD)
Softkeys 80
N
NAV 10
NAV1 1, 10
NAV2 1, 10
NEXRAD 37, 38, 76, 81
O
OBS 2
Obstacles 62, 66
Overspeed Protection 14
P
Pathways 43, 44
Power-up page 48
R
Reversionary mode 51
ROC 57
S
SafeTaxi® 44
SBAS 14, 17, 32, 42, 66, 67
Secure Digital (SD) card 48
Store Flight Plan 27
Stormscope lightning data 35, 36, 76
Strike 35
Strike mode 36
SVS 43, 74
Synthetic Vision System 43
Index-2
T
TA 58
TAF 37
TAS 39, 58, 69
Terrain 40, 62, 76, 80, 81
Terrain-SVS 40, 41, 42, 58
Timer 71
Topographical data 76, 80
Traffic 35, 39, 80
Traffic Advisory 58
Traffic advisory 38
Traffic map page 39, 40
Transponder 9, 78, 79
V
Vertical speed guidance 20
Vertical track 58
VNV 17, 18, 52, 73
Vspeed 2
W
Waypoint Selection Submenu 24, 25
Weather data link page 37
Wind data 77
X
XM lightning 76, 81
XM weather 37
Garmin G1000 Cockpit Reference Guide for the DA40NG
190-00953-01 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.
2345 Turner Road SE
Salem, OR 97302, U.S.A.
p: 503.391.3411 f: 503.364.2138
Garmin (Europe) Ltd
Liberty House, Bulls Copse Road
Hounsdown Business Park
Southampton, SO40 9RB, U.K.
p: 44/0870.8501241 f: 44/0870.8501251
Garmin Corporation
No. 68, Jangshu 2nd Road
Shijr, Taipei County, Taiwan
p: 886/2.2642.9199 f: 886/2.2642.9099
www.garmin.com
© 2010, 2011 Garmin Ltd. or its subsidiaries
190-00953-01 Rev. A
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