Cockpit Reference Guide

Garmin G1000 Cockpit Reference Guide for the Beechcraft 200/B200 Series
190-00929-01 Rev. A 57
Annunciations & Alerts
Flight
Instruments
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features Annun/Alerts Appendix Index
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.
System Failure AP and MET are unavailable. FD may still be available.
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.