Garmin G300 Pilot’s Guide
190-00921-00 Rev. E
2
System Overview
System
Overview
Flight
Instruments
EIS
COM
Interface
GPS
Navigation
Flight
Planning
Hazar
d
Avoidance
Additional
Featur
es
Integr
ated
Autopilot
Annun/Alerts
Appendix
Index
•
GSU 73
–
Garmin Sensor Unit sub-system for the G300 (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
temperature (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 accelerom-
eters 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.
GSU 73
Summary of Contents for G300 for Cessna SkyCatcher
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