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 46 of 179
AUTOPILOT UNDERSPEED PROTECTION ACTIVATION AND RECOVERY
(ESP-Equipped Aircraft Only)
(Red Warning Annunciator on the PFDs on ESP-equipped aircraft. May also be
accompanied by an amber annunciator above the airspeed tape display and aural
“AIRSPEED” alert)
1. Power Levers ..................... INCREASE POWER AS REQUIRED TO CORRECT UNDERSPEED
2. Aircraft Attitude and Altitude ......................................................................................... MONITOR
After underspeed condition is corrected:
3. Autopilot .........................................RESELECT VERTICAL AND LATERAL MODES (if necessary)
4. Power Levers .......................................................................................... ADJUST AS NECESSARY
NOTE
Autopilot Underspeed Protection Mode provides a pitch down command to maintain 90, 95 or 100
+/-2 KIAS, or 2 KIAS above stall warning airspeed, depending on the flap position and the vertical
mode selected. Underspeed recovery is not available below 200 feet AGL, except in go-around
(GA) mode.
ENGINE FAILURE
EMERGENCY ENGINE SHUTDOWN
ENGINE FAILURE IN FLIGHT
1. AP/YD DISC / TRIM INTRPT Button .......................................................... PRESS and RELEASE
2. Engine Failure Procedure in
EMERGENCY PROCEDURES Section of AFM ........................................................ COMPLETE
3. Trim Tabs .............................. MANUALLY ADJUST ELEVATOR, AILERON, AND RUDDER TABS
4. Autopilot ............................................................. PRESS ‘AP’ BUTTON (if desired) to RE-ENGAGE
5. Rudder Tab ............................................................... MANUALLY ADJUST AS REQUIRED AFTER
POWER AND CONFIGURATION CHANGES
6. TCAS II (IF INSTALLED) ................................................................................... SELECT TA ONLY