190-00595-00 Rev. AGarmin G1000 Pilot’s Guide for Beechcraft A36/G367-30AUTOMATIC FLIGHT CONTROL SYSTEM7.6 AFCS ANNUNCIATIONS AND ALERTSAFCS STATUS ALERTSThe following annunciations (listed in order of increasing priority) can appear on the PFD above the Airspeedand Attitude indicators. Only one annunciation occurs at a time, and messages are prioritized by criticality.Figure 7-34 AFCS Status AnnunciationAFCS StatusAnnunciationAlert Condition Annunciation DescriptionRudder Mistrim Right Yaw servo providing sustained force in the indicated directionRudder Mistrim LeftAileron Mistrim RightRoll servo providing sustained force in indicated directionAileron Mistrim LeftElevator Mistrim DownPitch servo providing sustained force in the indicated directionElevator Mistrim UpPitch Trim Failure(or Stuck MET Switch)If AP engaged, take control of the aircraft and disengage APIf AP disengaged, move MET switches separately to unstickYaw Damper Failure YD control failure; AP also inoperativeRoll Failure Roll axis control failure; AP inoperativePitch Failure Pitch axis control failure; AP inoperativeSystem Failure AP and MET are unavailable; FD may still be availablePreflight TestPerforming preflight system test; aural alert sounds at completionDo not press the AP DISC Switch during servo power-up and preflightsystem tests as this may cause the preflight system test to fail or neverto start (if servos fail their power-up tests). Power must be cycled to theservos to remedy the situation.Preflight system test failed; aural alert sounds at failureTable 7-4 AFCS Status Alerts
