FAA Approved Airplane Flight Manual Supplement

190-00915-02 Rev. 7 Hawker Beechcraft 200, 200C, B200, B200C,
FAA APPROVED B200GT and B200CGT King Air
Page 45 of 179
If Red Message Remains
5. Autopilot ........................................................................................................ DO NOT RE-ENGAGE
6. Elevator Trim .......................................................... CONTINUE TO USE ELEVATOR TAB WHEEL
7. Yaw Damper ............................................................................................. ENGAGE AS REQUIRED
In RVSM Airspace:
8. Advise ATC of loss of autopilot system.
9. 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.
10. Perform appropriate RVSM contingency procedures outlined in the operator’s RVSM manual for
the loss of automatic altitude hold capability.
AUTOPILOT PRE-FLIGHT TEST FAIL
(Red annunciator on PFD)
1. Indicates the AFCS system failed the automatic Pre-Flight test. The autopilot, ESP (if installed),
and electric elevator trim are inoperative. Flight Director may still function.
OVERSPEED RECOVERY
(Amber annunciation on PFD)
1. Power Levers ..................................................................................................................... REDUCE
When overspeed condition is corrected:
2. Autopilot ..................................................................... RESELECT VERTICAL MODE (if necessary)
NOTE
Overspeed recovery mode provides a pitch up command to decelerate the airplane at or
below the maximum autopilot operating speed (259 KIAS / 0.52 M). Overspeed recovery is not
active in altitude hold (ALT), glideslope (GS), or glidepath (GP) modes.