Garmin Cessna Caravan G1000, Manual

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190-00709-05 Rev. D
Garmin G1000 Pilot’s Guide for the Socata TBM 850/900
671
APPENDIX A
MISCELLANEOUS MESSAGE ADVISORIES (CONT.)
Message Comments
CRUISE II – Cruise II conditions met. Cruise II engine trend data log has been captured.
EXCEEDANCE – Engine exceedance
data is being logged.
An engine exceedance log has been captured.
REGISTER CONNEXT – Data services
are inoperative, register w/ Connext.
The system is not registered with Garmin Connext, or its current registration data has
failed authentication.
AFCS ALERTS
Figure A-5 AFCS Status Annunciation
AFCS Status
Annunciation
The following alert annunciations appear in the AFCS System Status field on the PFD.
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