Garmin G300 Pilot’s Guide
190-00921-00 Rev. D 13
System Overview
System
Overview
Flight
Instruments EIS
COM
Interface
GPS
Navigation
Flight
Planning
Hazard
Avoidance
Additional
Features
Integrated
Autopilot Annun/Alerts Appendix Index
G300 SYSTEM ANNUNCIATIONS
When an LRU or an LRU function fails, a large red ‘X’ is typically displayed
over the instrument(s) or data experiencing the failure (Refer to Appendix E,
Abnormal Operation). Upon G300 power-up, certain instruments remain invalid
as equipment begins to initialize. All instruments should be operational within
one minute of power-up. If any instrument remains flagged, the G300 should be
serviced by an authorized repair facility.
PFD Initialization
AHRS OPERATION
The Attitude and Heading Reference System (AHRS) performs attitude,
heading, and vertical acceleration calculations for the G300 System, utilizing GPS,
magnetometer, and air data in addition to information from its internal sensors.
Attitude and heading information are updated on the PFD while the AHRS receives
appropriate combinations of information from the external sensor inputs.