Afcs Alerts - Garmin G2000 Cockpit Reference Manual

AFCS ALERTS

Condition Annunciation Description
Pitch Failure
Roll Failure
MET Switch
Stuck, or Pitch
Trim Axis Con-
trol Failure
System Failure
Elevator
Mistrim Up
Elevator
Mistrim Down
Aileron
Mistrim Left
Aileron
Mistrim Right
Preflight Test
190-01264-01 Rev. A
Pitch axis control failure. AP is inoperative.
Roll axis control failure. AP is inoperative.
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.
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.
Garmin G2000 Cockpit Reference Guide for the Cessna Corvalis T240
Annunciations & Alerts
115