Garmin G5000 - AFCS System Status Annunciations; Manual Electric Elevator Trim

Model 560XL Appendix – Systems Description
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
A-13
AFCS System Status Annunciations
The following alert annunciations appear in the AFCS System Status field on the PFDs.
Table A-3, AFCS System Status Alerts
Alert Condition Annunciation Description
Rudder Mistrim Right
Yaw servo providing sustained force in the
indicated direction. Refer to abnormal
procedures.
Rudder Mistrim Left
Aileron Mistrim Right
Roll servo providing sustained force in the
indicated direction. Refer to abnormal
procedures.
Aileron Mistrim Left
Elevator Mistrim Down
Pitch servo providing sustained force in the
indicated direction. Refer to abnormal
procedures.
Elevator Mistrim Up
Rudder Mistrim Right
Yaw servo providing high sustained force in the
indicated direction. Refer to emergency
procedures.
Rudder Mistrim Left
Aileron Mistrim Right
Roll servo providing high sustained force in the
indicated direction. Refer to emergency
procedures.
Aileron Mistrim Left
Elevator Mistrim Down
Pitch servo providing high sustained force in the
indicated direction. Refer to emergency
procedures.
Elevator Mistrim Up
Preflight Test
Performing preflight system test; aural alert
sounds at completion.
Manual Electric Elevator Trim
Manual electric elevator trim is an integrated function included with the G5000 system. The electric
elevator trim can be operated manually by the pilot using the pitch trim switches on either control wheel,
or automatically by the autopilot. The pilot’s pitch trim switch inputs override those made by the copilot.
Runaway or malfunctioning pitch trim can be interrupted by pressing and holding the red AP YD
DISC/TRIM INT switch on either control wheel. Pulling the AP SERVO circuit breaker on either circuit
breaker panel will disable the electric elevator trim, both manual and automatic, so it will not move when
the AP YD DISC/TRIM INT switch is released.