Afcs Alerts - Garmin G1000 Reference Manual

Reversionary Sensor
Window Text
USING AHRS2
USING GPS1
USING GPS2

AFCS ALERTS

Condition Annunciation Description
Pitch Failure
Roll Failure
Pitch Trim Axis
Control Failure
System Failure
Yaw Damper/
Rudder Boost
Failure
Elevator Mistrim
Up
Elevator Mistrim
Down
Aileron Mistrim
Left
Aileron Mistrim
Right
Rudder Mistrim
Left
Rudder Mistrim
Right
Preflight Test
190-01344-00 Rev. B Garmin G1000 Cockpit Reference Guide for the Beechcraft 300/B300 Series
PFD1 is displaying data from the #2 AHRS.
PFD2 is displaying data from the #1 GPS.
PFD1 is displaying data from the #2 GPS.
Pitch axis control failure.
Roll axis control failure.
If annunciated when AP is engaged, a failure has occurred in
the pitch trim system.
AP and MET are unavailable. FD may still be available.
Yaw axis control failure.
A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.
A condition has developed causing the pitch servo to
provide a sustained force in the nose down direction.
A condition has developed causing the roll servo to provide
a sustained left force.
A condition has developed causing the roll servo to provide
a sustained right force.
A condition has developed causing the yaw servo to
provide a sustained force.
A condition has developed causing the yaw servo to provide a
sustained force.
Performing preflight system test. Upon completion of the
test, the aural alert will be heard.
Preflight system test has failed.
Annunciations & Alerts
Condition
89