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G1000 Cockpit Reference Guide for the Piper PA-46 Mirage/Matrix
190-01107-03 Rev. A
96
Annunciations & Alerts
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
AFCS ALERTS
Condition Annunciation Description
Pitch Failure Pitch axis control failure.
Roll Failure Roll axis control failure.
Pitch Trim Axis
Control Failure
If annunciated when AP is engaged, a failure has occurred in
the pitch trim system.
Yaw Damper
Failure
YD control failure; AP also inoperative
System Failure AP and MET are unavailable. FD may still be available.
Yaw Damper
Failure
YD control failure.
Elevator Mistrim
Up
A condition has developed causing the pitch servo to
provide a sustained force in the nose up direction.
Elevator Mistrim
Down
A condition has developed causing the pitch servo to
provide a sustained force in the nose down direction.
Aileron Mistrim
Left
A condition has developed causing the roll servo to provide
a sustained left force.
Aileron Mistrim
Right
A condition has developed causing the roll servo to provide
a sustained right force.
Rudder Mistrim
Left
A condition has developed causing the yaw servo to
provide a sustained force.
Rudder Mistrim
Right
A condition has developed causing the yaw servo to provide a
sustained force.
Preflight Test Performing preflight system test. Upon completion of the
test, the aural alert will be heard.
Preflight system test has failed.
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