Garmin Software Version 1308.10 User's Guide Page 133

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Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240
190-01264-02 Rev. A 117
Annunciations & Alerts
Flight
Instruments EIS
Nav/Com/
XPDR/Audio AFCS FMS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
AFCS ALERTS
Alert
Condition
Annunciation Description
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
Elevator
Mistrim Up
Pitch Trim
Failure
Pitch trim servo failure. If the pitch trim servo is inoperative,
it is considered a pitch axis control failure and all vertical
autopilot modes will be unavailable. Autopilot lateral modes
may continue to be used and flight director vertical modes
may still be available.
If AP engaged, take control of the aircraft and disengage AP.
If AP disengaged, move MET switch to unstick.
Roll Failure Roll axis control failure; AP inoperative
Pitch Failure
Pitch axis control failure. All vertical autopilot modes
unavailable. Autopilot lateral modes may continue to be used
and flight director vertical modes may still be available.
System Failure AP and MET are unavailable; FD may still be available
Preflight Test
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
Overspeed
Protection
Overspeed protection is provided in situations where the
flight director cannot acquire and maintain the mode
reference for the selected vertical mode without exceeding
the certified maximum autopilot airspeed.
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