Section 1 System Overview - Garmin G1000 Pilot's Manual

SECTION 1 SYSTEM OVERVIEW

Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin AFCS.
NOTE:
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 63W Integrated Avionics Units (IAU)
• GDC 74A Air Data Computer (ADC)
• GEA 71 Engine/Airframe Unit
• GTX 33 ES Extended Squitter Mode S Transponder
• GRS 77 Attitude and Heading Reference System
(AHRS)
• GMU 44 Magnetometer
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 Garmin AFCS Automated Flight Control System,
providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System.
190-00962-04 Rev. A Garmin G1000 Pilot's Guide for the Diamond DA42NG
• GDL 69/69A or 69/69A SXM Data Link Receiver
• GSA 80 AFCS Yaw Damper Servo
• GSA 81 AFCS Servos (3)
• GSM 85 ( or GSM 86) Servo Mounts (4)
• GSR 56 Iridium Transceiver
• GWX 68/70 Weather Radar
• GRA 5500 Radar Altimeter
• Flight Stream 210 Wireless Bluetooth
• GDL 88 ADS-B Transceiver
• GDL 59 Data Link
SYSTEM OVERVIEW
® Gateway
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