Model 560XL Section III – Operating Procedures
Abnormal Procedures
190-02313-03 Rev. 8 Textron Aviation Citation 560XL
FAA Approved 3-35
FLASHING AMBER AFCS MODE ANNUNCIATION
Abnormal mode transitions (those not initiated by the pilot or by normal sequencing of the AFCS) will
be annunciated by flashing the disengaged mode in amber on the PFD. Upon loss of a selected
mode, the system will revert to the default mode for the affected axis, either ROL or PIT. After 10
seconds, the new mode (PIT or ROL) will be annunciated in green.
IF NOT ON AN INSTRUMENT APPROACH:
1. Autopilot mode controls – SELECT another mode.
Procedure completed
IF ON AN INSTRUMENT APPROACH:
1. AP YD DISC/TRIM INT button – PRESS and RELEASE.
2. Continue approach manually or execute missed approach.
3. YD button – PRESS to engage yaw damper if desired.
Procedure completed
YAW DAMPER AUTOMATIC DISCONNECT
YD FLASHING on PFD
Flashing amber ‘YD’ in flight indicates that yaw damper has disconnected. The yaw servo or one of
its sensors may have failed.
The yaw damper disconnect may be accompanied by an AP-YD FAIL CAS annunciation. Refer to
the AP-YD FAIL procedure before attempting to re-engage the yaw damper.
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