190-00962-02 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
1
SYSTEM OVERVIEW
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
SECTION 1 SYSTEM OVERVIEW
NOTE:
Refer to the Automatic Flight Control System (AFCS) Section for details on the GFC 700 AFCS.
The G1000 Integrated Flight Deck System presents flight instrumentation, position, navigation, communication,
and identification information using flat-panel color displays. The system is distributed across the following Line
Replaceable Units (LRUs):
•
GDU 1040
Primary Flight Display (PFD)
•
GDU 1045
Multi Function Display (MFD)
•
GMA 1347
Audio Panel with Integrated Marker
Beacon Receiver
•
GIA 63/63W
Integrated Avionics Units (IAU)
•
GDC 74A
Air Data Computer (ADC)
•
GEA 71
Engine/Airframe Unit
•
GTX 33
Mode S Transponder
•
GRS 77
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
•
GDL 69/69A
Data Link Receiver (optional)
•
GSA 80
AFCS Yaw Damper Servo (optional)
•
GSA 81
AFCS Servos (3) (optional)
•
GSM 85 (
or
GSM 86)
Servo Mounts (4) (optional)
•
GSR 56
Iridium Transceiver (optional)
•
GWX 68
Weather Radar (optional)
•
GDL 90
ADS-B/FIS-B Data Link Transceiver (optional)
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2.
The Diamond DA42NG may be optionally equipped with a GFC 700 Automated Flight Control System (AFCS),
providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System.
