Garmin G300 User Manual

Garmin G300 Pilot’s Guide
190-00921-00 Rev. D
14
System Overview
System
Overview
Flight
InstrumentsEIS
COM
Interface
GPS
Navigation
Flight
Planning
Hazard
Avoidance
Additional
Features
Integrated
AutopilotAnnun/AlertsAppendixIndex
AHRS Operation
Attitude/Heading Invalid
AHRS
no-GPS
Mode
AHRS Normal
Operation
AHRS no-
Mag Mode
AHRS no-Mag/
no-Air Mode
Heading Invalid
available available
unavailable
unavailable
available
unavailable unavailable
available
l
e
e
l
bl
e
e
e
e
e
e
e
Air Data
l
e
e
e
e
l
l
bl
e
e
e
e
Magnetometer Data
unavailable
available
l
bl
e
e
e
e
e
l
e
e
e
GPS Data
b
l
e
e
e
e
e
l
e
e
e
Magnetometer Data
bl
e
e
e
e
un
Air Data
Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by
message advisory alerts. Any failure of the internal AHRS inertial sensors results
in loss of attitude and heading information (indicated by red ‘X’ flags over the
corresponding flight instruments).
If GPS input fails, the AHRS can continue to provide attitude and heading
information to the PFD as long as magnetometer and airspeed data are available
and valid.
If the magnetometer input fails, the AHRS continues to output valid attitude
information; however, the heading output on the PFD Page is flagged as invalid
with a red ‘X’.
Failure of the air data input has no effect on the AHRS output while AHRS is
receiving valid GPS information. Invalid/unavailable airspeed data in addition to
GPS failure results in loss of all attitude and heading information. Likewise, loss
of magnetometer (heading) data, in combination with loss of GPS data results in
a loss of all attitude and heading information.

Garmin G300 Specifications

General

Brand	Garmin
Model	G300
Category	GPS
Language	English