
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-03 Rev. B 69
Annunciations & Alerts
Flight
Instruments EAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
Reversionary
Sensor
Window Text
Condition
USING AHRS2
PFD1 is displaying data from the #2 AHRS.
USING GPS1
PFD2 is displaying data from the #1 GPS.
USING GPS2
PFD1 is displaying data from the #2 GPS.
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 Trim Failure
(or stuck MEYT
Switch)
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move the MEYT switch to
check if a stuck
switch is causing the annunciation
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
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