Garmin G2000 Pilots Guide - Page 586
AFCS Status Annunciations, A-7
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SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO & CNS AVOIDANCE MANAGEMENT Appendix A AFCS Status Annunciations The following annunciations (listed in order of increasing priority) can appear on the PFD above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality. AFCS Status Annunciation Figure A-7 AFCS Status Annunciation Condition Pitch Failure Annunciation Description Pitch axis control failure. AP is inoperative. Roll Failure Roll axis control failure. AP is inoperative. MET Switch Stuck, or Pitch Trim Axis Control Failure System Failure If annunciated when AP is engaged, take control of the aircraft and disengage the autopilot. If annunciated when AP is not engaged, move each half of the MET switch separately to check if a stuck switch is causing the annunciation. AP and MET are unavailable. FD may still be available. Elevator Mistrim Up Elevator Mistrim Down Aileron Mistrim Left Aileron Mistrim Right Preflight Test A condition has developed causing the pitch servo to provide a sustained force. Be prepared to apply nose up control wheel force upon autopilot disconnect. A condition has developed causing the pitch servo to provide a sustained force. Be prepared to apply nose down control wheel force upon autopilot disconnect. A condition has developed causing the roll servo to provide a sustained left force. Ensure the slip/skid indicator is centered and observe any maximum fuel imbalance limits. A condition has developed causing the roll servo to provide a sustained right force. Ensure the slip/skid indicator is centered and observe any maximum fuel imbalance limits. Performing preflight system test. Upon completion of the test, the aural alert is heard. Preflight system test has failed. NOTE: 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. FLIGHT HAZARD AFCS ADDITIONAL FEATURES APPENDICES INDEX 572 Garmin G2000 Pilot's Guide for the Cessna T240 190-01263-01 Rev. A
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