Garmin G2000 Pilot’s Guide for the Cessna T240
190-01263-01 Rev. A
482
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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.
Figure 7-40 AFCS Status Annunciation
AFCS Status
Annunciation
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
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; AP inoperative
System Failure
AP and MET are unavailable; FD may still be available
Prefl ight Test
Performing prefl ight system test; aural alert sounds at completion
Do not press the
AP DISC
Switch during servo power-up and prefl ight system tests
as this may cause the prefl ight 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.
Prefl ight system test failed; aural alert sounds at failure
Table 7-5 AFCS Status Alerts
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