Garmin G900X Pilot's Manual - page 13
190-00726-00 Rev. A
Garmin G900X Pilot’s Guide
1-1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
The G900X Integrated Flight Deck System presents flight instrumentation, position, navigation, communication,
and identification information to the pilot using flat-panel color displays. The system is distributed across the
following Line Replaceable Units (LRUs):
•
GDU 1040
Primary Flight Display (PFD)
•
GDU 1040
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
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
G900X is capable of interfacing with the following optional equipment:
•
GCU 476
MFD/PFD Control Unit
•
GDL 69A
Data Link Receiver
• CO Guardian Aero 353R/452R Remote Carbon
Monoxide Detector
• Avidyne TAS600-series Traffic Advisory System
• Artex ELT 406-N Emergency Locator Transmitter
• S-TEC 55X Autopilot
• TruTrak Digiflight I/Sorecerer/DFC Series autopilots
• TruTrak Digiflight II-series autopilots
• TruTrak Digitrak/Pictorial Pilot autopilots
• TruTrak Altrak Altitude Hold Autopilot
• TruTrak ADI
• Trio Avionics EZ Pilot Autopilot
• Trio Avionics EZ Altitude Control Autopilot