Airplane Description DA 62 AFM
7.13 GARMIN G1000 INTEGRATED AVIONICS SYSTEM
7.13.1 GENERAL
The Gamin G1000 is a fully integrated flight, engine, communication, navigation and
surveillance instrumentation system. This integrated avionics system consists of a primary
flight display (PFD), a multi-function display (MFD), an audio panel, an attitude and
heading reference system (AHRS), an air data computer (ADC) and the sensors and
computers to process flight and engine information for display to the pilot. The system
contains dual GPS receivers, dual VOR/ILS receivers, dual VHF communications
transceivers, a transponder, and an integrated annunciation system to alert the pilot of
certain abnormal conditions.
A remote avionic box is located in the front electric/avionic compartment. A push-to-talk
(PTT) button for the COM portion of the G1000 is mounted on the end of each control
stick. There are connection facilities for up to 5 (or optionally 7) headsets. The connections
for the pilot, copilot and 1
st
passenger row are located between the pilot´s and copilot´s
seat. The connections for the 2
nd
passenger row are located on the left and right outboard
side of each seat. As the audio panel is limited to a maximum of 6 microphones, a switch
is optionally installed, swapping the 6
th
microphone input between the 1
st
row middle seat
and the 2
nd
row right seat. The headset phones are not affected by the switch.
Refer to the Garmin G1000 Cockpit Reference Guide, P/N 190-01896-( ), and Garmin
G1000 Pilot's Guide for the Diamond DA 62, P/N 190-01895-( ), for complete descriptions
of the G1000 system and operating procedures.
If MÄM 62-254 is installed, refer to the Garmin G1000 NXi Cockpit Reference Guide,
P/N 190-01905-( ) and Garmin G1000 NXi Pilot's Guide for the Diamond DA 62,
P/N 190-01904-( ) for complete descriptions of the G1000 NXi system and operating
procedures.
Page 7 - 78 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E
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