Afcs System Status Annunciations; Manual Electric Elevator Trim - Garmin G5000 Airplane Flight Manual Supplement

Model 560XL

AFCS System Status Annunciations

The following alert annunciations appear in the AFCS System Status field on the PFDs.
Alert Condition
Rudder Mistrim Right
Rudder Mistrim Left
Aileron Mistrim Right
Aileron Mistrim Left
Elevator Mistrim Down
Elevator Mistrim Up
Rudder Mistrim Right
Rudder Mistrim Left
Aileron Mistrim Right
Aileron Mistrim Left
Elevator Mistrim Down
Elevator Mistrim Up
Preflight Test

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.
190-02313-03 Rev. 8
Table A-3, AFCS System Status Alerts
Annunciation
Yaw servo providing sustained force in the
indicated
procedures.
Roll servo providing sustained force in the
indicated
procedures.
Pitch servo providing sustained force in the
indicated
procedures.
Yaw servo providing high sustained force in the
indicated
procedures.
Roll servo providing high sustained force in the
indicated
procedures.
Pitch servo providing high sustained force in the
indicated
procedures.
Performing preflight system test; aural alert
sounds at completion.
Appendix – Systems Description
Description
direction. Refer to
direction. Refer to
direction. Refer to
direction. Refer to
direction. Refer to
direction. Refer to
Textron Aviation Citation 560XL
abnormal
abnormal
abnormal
emergency
emergency
emergency
A-13