Garmin G2000 Pilots Guide - Page 496

SyStem overvieW Flight inStrumentS eiS & cnS AuDio pAnel AvoiDAnce mAnAgement AutomAtic Flight control SyStem 7.7 AFcS AnnunciAtionS AnD AlertS AFcS StAtuS AlertS The annunciations in Table 7-5 (listed in order of increasing priority) can appear on the PFD above the Airspeed and Attitude indicators. Only one annunciation occurs at a time, and messages are prioritized by criticality. AFCS Status Annunciation Figure 7-40 AFCS Status Annunciation Alert Condition Aileron Mistrim Right Aileron Mistrim Left Annunciation Description Roll servo providing sustained force in the indicated direction Elevator Mistrim Down Elevator Mistrim Up Pitch Trim Failure Roll Failure Pitch servo providing sustained force in the indicated direction If AP engaged, take control of the aircraft and disengage AP If AP disengaged, move MeT switch to unstick Roll axis control failure; AP inoperative Pitch Failure Pitch axis control failure; AP inoperative System Failure Preflight Test AP and MET are unavailable; FD may still be available Performing preflight system test; aural alert sounds at completion 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. Preflight system test failed; aural alert sounds at failure Table 7-5 AFCS Status Alerts Flight hAZArD AFcS ADDitionAl FeAtureS AppenDiceS inDex 482 Garmin G2000 Pilot's Guide for the Cessna T240 190-01263-01 Rev. A