Garmin G300 Pilot’s Guide
190-00921-00 Rev. E
15
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
Attitude/Heading Invalid
AHRS
no-GPS
Mode
AHRS Normal
Operation
AHRS no-
Mag Mode
AHRS no-Mag/
no-Air Mode
Heading Invalid
av
ailab
le
av
ailab
le
una
vailab
le
una
vailab
le
av
ailab
le
una
vailab
le
una
vailab
le
av
ailab
le
l
e
e
e
l
l
b
e
e
e
e
Air Data
l
e
e
e
e
l
bl
b
e
e
e
e
e
Magnetometer Data
una
vailab
le
av
ailab
le
l
bl
b
e
e
e
e
e
l
e
e
e
e
GPS Data
l
bl
e
e
e
e
e
l
e
e
e
Magnetometer Data
l
e
e
e
e
u
u
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.
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