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Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-01 Rev. A
63
Annunciations & Alerts
Flight
Instruments EICAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
AFCS ALERTS
Alert Condition Annunciation Description
Rudder Mistrim
Right
Yaw servo providing sustained force in the indicated
direction. Aircraft rudder retrim after substantial pitch and
power changes required.
Rudder Mistrim
Left
Aileron Mistrim
Right
Roll servo providing sustained force in the indicated direction
Aileron Mistrim
Left
Elevator Mistrim
Down
Pitch servo providing sustained force in the indicated
direction. May indicate a failure of the pitch trim servo or
trim system.
Elevator Mistrim
Up
Pitch Trim Failure
(or stuck MEPT
Switch)
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move MEPT switches separately to unstick
Yaw Damper
Failure
YD control failure; AP also inoperative
Roll Failure Roll axis control failure; AP inoperative
Pitch Failure Pitch axis control failure; AP inoperative
System Failure AP and MEPT are unavailable; FD may still be available
Preflight Test
Performing preflight system test; aural alert sounds at
completion
Do not press the AP DISC Switch during servo power-up and
preflight system tests as this may cause the preflight system
test to fail or never to start (if servos fail their power-up tests).
Power must be cycled to the servos to remedy the situation.
Preflight system test failed; aural alert sounds at failure
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