Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240
190-01264-01 Rev. A
115
Annunciations & Alerts
Flight
Instruments
EIS
Nav/Com/
XPDR/Audio
AFCS
FMS Nav
Flight
Planning
Pr
ocedur
es
Hazar
d
Avoidance
Additional
Featur
es
Abnormal
Oper
ation
Annun/
Alerts
Appendix
Index
AFCS ALERTS
Condition
Annunciation Description
Pitch Failure
Pitch axis control failure. AP is inoperative.
Roll Failure
Roll axis control failure. AP is inoperative.
MET Switch
Stuck, or Pitch
Trim Axis Con-
trol 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.
System Failure
AP and MET are unavailable. FD may still be available.
Elevator
Mistrim Up
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.
Elevator
Mistrim Down
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.
Aileron
Mistrim Left
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.
Aileron
Mistrim Right
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.
Preflight Test
Performing preflight system test. Upon completion of the test,
the aural alert is heard.
Preflight system test has failed.
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