Airplane Flight Manual Supplement

Hawker Beechcraft 200, 200C, B200, B200C, 190-00915-02 Rev. 8
B200GT and B200CGT King Air FAA APPROVED
Page 44 of 179
YAW AXIS FAILURE
(Amber annunciator on PFD)
1. Indicates a failure of the yaw axis of the autopilot. The yaw damper will disconnect. The
autopilot may be re-engaged and disengaged normally, but the yaw damper will remain
inoperative.
2. Autopilot .......................................................................................................... AS DESIRED
DO NOT USE THE AUTOPILOT TO FLY A COUPLED ILS, LOC, LP/LPV OR LNAV/VNAV
APPROACH WITH AN INOPERATIVE YAW DAMPER. THE AUTOPILOT MAY NOT BE ABLE
TO MAINTAIN DIRECTIONAL CONTROL IF AN ENGINE FAILS DURING THE APPROACH.
NOTE
If the amber annunciator illuminates without the autopilot engaged, it may indicate a
faulted AHRS. Monitor both PFDs and the standby attitude indicator for abnormal attitude
indications.
NOTE
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.
PITCH TRIM FAILURE
(Red annunciator on PFD)
1. Indicates a failure of the pitch trim servo of the autopilot. The autopilot and ESP (if installed) will
be inoperative. The yaw damper will remain operative.
2. Control Wheel ............................................................................................................. GRIP FIRMLY
3. AP/YD DISC / TRIM INTRPT Button ............................................................ PRESS and RELEASE
(Be prepared for high elevator control forces)
4. Elevator Trim ...................................................... AS REQUIRED USING ELEVATOR TAB WHEEL
If Red Message Clears
5. Autopilot ....................................................................................................................... RE-ENGAGE
WARNING