Garmin G3X Pilot’s Guide
190-01115-00 Rev. K
2
System Overview
System
Overview
Flight
Instruments
EIS
CNS
Interface
GPS
Navigation
Flight
Planning
Hazar
d
Avoidance
Additional
Featur
es
AFCS
Annun/Alerts
Appendix
Index
• GSU 73
–
Garmin Sensor Unit sub-system for the G3X (Air Data Computer (ADC), Engine/
Airframe Unit, and the Attitude and Heading Reference System (AHRS))
– ADC: Processes data from the pitot-static system and outside air tem-
perature (OAT) sensor.
– Engine/Airframe Unit: Receives and processes signals from the engine
and airframe sensors.
– AHRS: Provides aircraft attitude and heading information to the PFD.
The AHRS contains advanced sensors (including accelerometers and rate
sensors) and interfaces with the Magnetometer to obtain magnetic field
information, with the ADC to obtain air data, and with the GDU to obtain
GPS information. AHRS operation is discussed later in this section.
– ARINC 429 interface: Transmits and receives ARINC 429 signals for inter-
face to panel-mount IFR GPS navigators.
GSU 73
Summary of Contents for G3X Touch
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