FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.2
Page 34 of 135 FAA APPROVED
PITCH AXIS FAILURE
(Red annunciator on PFD)
1. Indicates a failure of the pitch axis of the autopilot. The autopilot 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
NOTE
The standby altimeter must be corrected for position error using the Altimeter Correction –
Standby System chart in the Performance section of this supplement.
5. Perform appropriate RVSM contingency procedures outlined in the operator’s RVSM manual for
the loss of automatic altitude hold capability.
ROLL AXIS FAILURE
(Red annunciator on PFD)
1. Indicates a failure of the roll axis of the autopilot. The autopilot 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
NOTE
The standby altimeter must be corrected for position error using the Altimeter Correction –
Standby System chart in the Performance section of this supplement.
5. Perform appropriate RVSM contingency procedures outlined in the operator’s RVSM manual for
the loss of automatic altitude hold capability.