This manual reflects the operation of System Software version 0670.02 or later for the Diamond
DA42NG. Some differences in operation may be observed when comparing the information in this
manual to earlier or later software versions.
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.
April, 2009 190-00963-00 Rev. B 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 Diamond DA42NG
190-00963-00 Rev. B
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 DA42NG
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 DA42NG Pilot’s Operating Handbook (POH). Thoroughly practice
basic operation prior to actual use. During flight operations, carefully compare
indications from the G1000 to all available navigation sources, including
the information from other NAVAIDs, visual sightings, charts, etc. For safety
purposes, always resolve any discrepancies before continuing navigation.
190-00963-00 Rev. B
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
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 anomalies in the earth’s magnetic field, operating
the G1000 within the following areas could result in loss of reliable attitude
and heading indications. North of 70° North latitude and south of 70° South
latitude. An area north of 65° North latitude between longitude 75º West
and 120º West. An area south of 55° South latitude between longitude 120º
East and 165º East.
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.
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.
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
Warnings, Cautions & Notes
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.
190-00963-00 Rev. B
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
Warnings, Cautions & Notes
Blank Page
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
Record of Revisions
Part NumberChange Summary
190-00963-00
Rev AInitial release at GDU 9.05
RevisionDate of RevisionAffected PagesDescription
Rev B4/09i-Index-4Added Synthetic Vision
System
190-00963-00 Rev. BRR-1
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
Record of Revisions
RR-2
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
INDEX .........................................................................................................................................Index-1
190-00963-00 Rev. Biii
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
Table of Contents
Blank Page
iv
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
Flight Instruments
FLIGHT INSTRUMENTS
SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING
Turn the BARO Knob to select the desired setting.
SELECTING STANDARD BAROMETRIC PRESSURE (29.92 IN HG)
1)
Press the PFD Softkey.
2)
Press the STD BARO Softkey to set standard barometric pressure.
CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS
1)
Press the PFD Softkey to display the second-level softkeys.
2)
Press the ALT UNIT Softkey.
3)
Press the IN Softkey to display the barometric pressure setting in inches of
mercury (in Hg).
Or
:
Press the HPA Softkey to display the barometric pressure setting in
hectopascals.
4)
Press the BACK Softkey to return to the top-level softkeys.
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
CHANGE NAVIGATION SOURCES
1)
Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places
the light blue tuning box over the NAV1 standby frequency in the upper left
corner of the PFD.
2)
Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2
or LOC2. This places the light blue tuning box over the NAV2 standby
frequency.
3)
Press the CDI Softkey a third time to return to GPS.
190-00963-00 Rev. B1
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
Flight Instruments
ENABLE/DISABLE OBS MODE WHILE NAVIGATING WITH GPS
Flight
1)
InstrumentsEIS
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.
Nav/Com/
XPDR/AudioAFCSGPS Nav
GENERIC TIMER
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.
Flight
PlanningProcedures
3)
Press the ENT Key to START, STOP, or RESET the timer (if the timer is
counting DOWN, it starts counting UP after reaching zero). Press the CLR
Key or the TMR/REF Softkey to remove the window.
CONFIGURE VSPEED BUGS
Hazard
Avoidance
1)
Press the TMR/REF Softkey.
2)
Turn the
large
FMS Knob to highlight the desired Vspeed.
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
3)
Use the small FMS Knob to change the Vspeed in 1-kt increments (when a
speed has been changed from a default value, an asterisk appears next to
the speed).
4)
Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF
field
5)
Turn the
6)
To remove the window, press the CLR Key or the TMR/REF Softkey.
2
small
FMS Knob clockwise to ON or counterclockwise to OFF.
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
Flight Instruments
SET BAROMETRIC MINIMUM DESCENT ALTITUDE
1)
Press the TMR/REF Softkey.
2)
Turn the large FMS Knob to highlight the OFF/BARO field to the right of
‘MINIMUMS’.
3)
Turn the small FMS Knob clockwise to BARO.
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 press the TMR/REF Softkey.
DISPLAYING WIND DATA
1)
Press the PFD Softkey.
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.
CHANGING HSI FORMAT
1)
Press the PFD Softkey.
2)
Press the HSI FRMT Softkey.
3)
Press the 360 HSI Softkey to display the full size HSI.
Or
:
Press the ARC HSI Softkey to display the arc style HSI.
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
190-00963-00 Rev. B3
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
AlertsAppendixIndex
Annun/
Flight Instruments
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
4
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
ENGINE DISPLAY
Engine Indication System
ENGINE INDICATION SYSTEM
InstrumentsEIS
Flight
Engine Load
Indicator
Fuel Flow
Indicator
Oil Pressure
Indicator
Fuel
Temperature
Indicator
Tachometer
Oil Temperature
Indicator
Coolant
Temperature
Indicator
Fuel Quantity
Indicator
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
ENGINE Display
190-00963-00 Rev. B5
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
AlertsAppendixIndex
Annun/
Engine Indication System
SYSTEM DISPLAY
Flight
Pressing the ENGINE Softkey displays the SYSTEM and FUEL softkeys. Press the
InstrumentsEIS
SYSTEM Softkey to show the System Display.
Engine Load
Indicator
Nav/Com/
XPDR/AudioAFCSGPS Nav
Tachometer
Flight
PlanningProcedures
Voltmeter
Gearbox
Hazard
Avoidance
Features
Additional
Temperature
Indicator
Oil Temperature
Indicator
Abnormal
Operation
AlertsAppendixIndex
Annun/
Deice Fluid
Indicator
FUEL DISPLAY
Pressing the ENGINE Softkey displays the SYSTEM and FUEL softkeys. Press the
FUEL Softkey to show the Fuel Display.
Ammeter
Coolant
Temperature
Indicator
Oil Pressure
Indicator
SYSTEM Display
6
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
Engine Indication System
Fuel used (GAL USED), endurance (ENDUR), and range (RANGE NM) are all
calculated based on the last manual adjustment of the fuel remaining (GAL REM).
Measured fuel quantity has no effect on fuel calculations. Fuel calculations are
based on sensed fuel flow and the last manual adjustment of the fuel remaining.
- DEC FUEL – Allows the pilot to decrease the gallons of fuel remaining (GAL
REM) in 1-gallon increments
- INC FUEL – Allows the pilot to increase the gallons of fuel remaining in
1-gallon increments
- RST FUEL – Resets the fuel remaining to 50.0 gallons with standard fuel tanks
or 76.4 gallons with auxiliary fuel tanks.
Engine Load
Indicator
Tachometer
Fuel
Quantity
Indicator
Fuel
Temperature
Indicator
Gallons
Used
Range in
Nautical
Miles
Fuel Flow
Indicator
Gallons
Remaining
Endurance
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
Total Time
In Service
Indicator
FUEL Display
190-00963-00 Rev. B7
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
Engine Indication System
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
8
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
NAV/COM/TRANSPONDER/AUDIO PANEL
ENTER OR CHANGE FLIGHT ID
1)
Press the TMR/REF Softkey, then turn the large FMS Knob to highlight the
Flight ID field.
2)
Turn the small FMS Knob to enter the first character.
3)
Turn the large FMS Knob to select the next field.
4)
Turn the small FMS Knob to enter the next desired character.
5)
Repeat steps 3 and 4 until the desired Flight ID is entered.
6)
Press the ENT Key to update the Flight ID.
ADF TUNING (OPTIONAL)
1)
Press the ADF/DME Softkey.
2)
Turn the small FMS Knob to enter the first digit of the desired ADF
frequency.
3)
Turn the large FMS Knob to select the next desired field.
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.
10)
Press the ENT Key to complete the selection.
Nav/Com/XPDR/Audio Panel
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
DME TUNING (OPTIONAL)
1)
Press the ADF/DME or DME Softkey.
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.
190-00963-00 Rev. B9
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
AlertsAppendixIndex
Annun/
Nav/Com/XPDR/Audio Panel
ENTER A TRANSPONDER CODE
Flight
1)
InstrumentsEIS
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
Nav/Com/
XPDR/AudioAFCSGPS Nav
the entry is cancelled and restored to the previous code. Five seconds after
the fourth digit has been entered, the transponder code becomes active.
SELECTING A COM RADIO
Transmit/Receive
Press the COM1 MIC, COM2 MIC
installed) on the audio panel.
Flight
PlanningProcedures
Receive Only
Press the COM1, COM2
audio panel.
SELECTING A NAV RADIO
Hazard
Avoidance
1)
To begin navigating using a navigation radio, press the CDI Softkey on the
PFD to select VOR1/LOC1 (NAV1) or VOR2/LOC2 (NAV2).
, or
COM3 MIC Key (optional COM, if
, or
COM3 Key (optional COM, if installed) on the
2)
Features
Additional
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.
Abnormal
Operation
NAV/COM TUNING
1)
AlertsAppendixIndex
Annun/
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.
10
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
Nav/Com/XPDR/Audio Panel
DIGITAL CLEARANCE RECORDER AND PLAYER
NOTE: Only the audio for the selected
COM MIC
Key is recorded. Audio is
not recorded for COM3 MIC.
• PressingthePLAY Key once plays the latest recorded memory block, then returns
to normal operation.
• PressingtheMKR/MUTE Key while playing a memory block stops play.
• Pressingthe 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.
INTERCOM SYSTEM (ICS) ISOLATION
Press the PILOT and/or COPLT Key to select those isolated from hearing the Nav/
Com radios and music.
Mode
PILOT KEY
ANNUNCIATOR
ALLOFFOFF
PILOTONOFF
COPLT KEY
ANNUNCIATOR
Pilot Hears
Selected
radios; pilot;
copilot;
passengers;
music
Selected
radios; pilot
Copilot
Hears
Selected
radios; pilot;
copilot;
passengers;
music
Copilot;
passengers;
music
Passenger
Hears
Selected
radios; pilot;
copilot;
passengers;
music
Copilot;
passengers;
music
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Selected
COPILOTOFFON
radios; pilot;
passengers;
Copilot
music
Selected
CREWONON
radios; pilot;
copilot
190-00963-00 Rev. B11
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
Selected
radios; pilot;
copilot
Selected
radios; pilot;
passengers;
music
Passengers;
music
AlertsAppendixIndex
Annun/
Nav/Com/XPDR/Audio Panel
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Blank Page
Hazard
Avoidance
Features
Additional
Abnormal
Operation
AlertsAppendixIndex
Annun/
12
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM
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.
NOTE: If the attitude information required for the default flight director modes
becomes invalid or unavailable, the autopilot automatically disengages.
FLIGHT DIRECTOR ACTIVATION
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.
AFCS
InstrumentsEIS
Flight
XPDR/AudioAFCSGPS Nav
Nav/Com/
Control Pressed
Modes Selected
LateralVertical
FD KeyRoll Hold (default)ROLPitch Hold (default)PIT
AP KeyRoll Hold (default)ROLPitch Hold (default)PIT
CWS ButtonRoll Hold (default)ROLPitch Hold (default)PIT
GA Button
Takeoff (on ground)
Go Around (in air)
TO
GA
Takeoff (on ground)
Go Around (in air)TOGA
A LT KeyRoll Hold (default)ROLAltitude HoldALT
VS KeyRoll Hold (default)ROLVertical SpeedVS
VNV KeyRoll Hold (default)ROLVertical Path Tracking*VPTH
GPS
NAV KeyNavigation**
VOR
LOC
Pitch Hold (default)PIT
BC
GPS
APR KeyApproach**
VOR
Pitch Hold (default)PIT
LOC
HDG KeyHeading SelectHDGPitch Hold (default)PIT
*Valid VNV flight plan must be entered before VNV Key press activates flight director.
**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.
PlanningProcedures
Flight
Avoidance
Hazard
Additional
Features
Operation
Abnormal
Annun/
AlertsAppendixIndex
190-00963-00 Rev. B13
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
AFCS
VERTICAL MODES
Flight
InstrumentsEIS
Vertical ModeDescriptionControlAnnunciation
Holds the current aircraft pitch
Pitch Hold
Selected Altitude
Armed
Nav/Com/
XPDR/AudioAFCSGPS Nav
Altitude Hold
Vertical Speed
Flight Level Change
Flight
PlanningProcedures
Vertical Path Tracking
VNAV Target Altitude
Capture
Hazard
Glidepath ***
Avoidance
Glideslope
Features
Additional
Go Around
Abnormal
Operation
* 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
AlertsAppendixIndex
Annun/
** ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of
Selected Altitude
***GP is available in installations with GIA 63W IAUs when WAAS is available. Refer to the
Airplane Flight Manual to determine whether WAAS functionality is approved.
attitude; may be used to climb/
(default)PIT
descend to the Selected Altitude
Captures the Selected Altitude*ALTS
Holds the current Altitude
Reference
A LT KeyA LTnnnnn f T
Holds aircraft vertical speed; may
be used to climb/descend to the
VS KeyVSnnnn f p m
Selected Altitude
Holds aircraft airspeed while aircraft
is climbing/descending to the
FLC KeyFLCnnn k T
Selected Altitude
Captures and tracks descent legs of
an active vertical profile
Captures the Vertical Navigation
(VNV) Target Altitude
VNV KeyVPTH
**ALTV
Captures and tracks the WAAS
glidepath on approach
APR Key
Captures and tracks the ILS
glideslope on approach
Disengages the autopilot and
commands a constant pitch attitude
and wings level in the air
GA
Button
GP
GS
GA
14
Garmin G1000 Cockpit Reference Guide for the Diamond DA42NG
190-00963-00 Rev. B
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