FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft 200, 200C, B200, B200C, 190-00915-02 Rev. 7
B200GT and B200CGT King Air FAA APPROVED
Page 42 of 179
AUTOPILOT FAILURE
(Red annunciator on PFD, Red ‘AP’ flashing on PFD, Continuous high-low aural tone)
1. AP/YD DISC / TRIM INTRPT Button ..................................................................................... PRESS
(to cancel disconnect tone)
If red ‘AFCS’ is displayed, the autopilot, ESP (If installed), yaw damper, and manual electric
pitch trim will be inoperative.
2. Advise ATC of loss of autopilot system.
NOTE
A loss of the autopilot may also cause the yaw damper to be inoperative. Some King Air 200,
200C, B200 and B200C airplanes require the yaw damper to be operative above 17,000 feet
MSL. Refer to the Limitations section of the Aircraft Flight Manual, or appropriate Airplane
Flight Manual Supplement for further information.
3. Altitude ........................................ MONITOR AND MAINTAIN ASSIGNED ALTITUDE MANUALLY
Record each altimeter reading for contingency procedure use
NOTE
The standby altimeter must be corrected for position error using the Altimeter Correction –
Standby System chart in the Performance section of this supplement.
4. Perform appropriate RVSM contingency procedures outlined in the operator’s RVSM manual for
the loss of automatic altitude hold capability.
PITCH AXIS FAILURE
(Red annunciator on PFD)
1. Indicates a failure of the pitch axis of the autopilot. The autopilot and ESP (if installed) will be
inoperative. The yaw damper will be operative.
NOTE
If the red annunciator illuminates without the autopilot engaged, it may indicate a
faulted AHRS. Monitor both PFDs and the standby attitude indicator for abnormal attitude
indications.
2. Advise ATC of loss of autopilot system.
3. Yaw Damper ............................................................................................. ENGAGE AS REQUIRED
4. Altitude ........................................ MONITOR AND MAINTAIN ASSIGNED ALTITUDE MANUALLY
Record each altimeter reading for contingency procedure use