Garmin G1000 Pilot's Guide

190-00962-04 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA42NG
1
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the Garmin 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 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
• 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
®
Gateway
• GDL 88 ADS-B Transceiver
• GDL 59 Data Link
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.

Garmin G1000 Specifications

General

Brand	Garmin
Model	G1000
Category	Avionics Display
Language	English