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 39 of 179
Section 3 - Emergency Procedures
Table of Contents
AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 40
AUTOPILOT MALFUNCTION / PITCH TRIM RUNAWAY ..................................................................... 40
MANUAL AUTOPILOT DISCONNECT .................................................................................................. 41
AUTOPILOT ABNORMAL DISCONNECT ............................................................................................. 41
AUTOPILOT FAILURE ........................................................................................................................... 42
PITCH AXIS FAILURE ............................................................................................................................ 42
ROLL AXIS FAILURE ............................................................................................................................. 43
YAW AXIS FAILURE .............................................................................................................................. 44
(Amber annunciator on PFD) ........................................................................... 44
PITCH TRIM FAILURE ........................................................................................................................... 44
AUTOPILOT PRE-FLIGHT TEST FAIL .................................................................................................. 45
OVERSPEED RECOVERY ..................................................................................................................... 45
AUTOPILOT UNDERSPEED PROTECTION ACTIVATION AND RECOVERY (ESP-Equipped Aircraft
Only)........................................................................................................................................................ 46
ENGINE FAILURE .................................................................................................................................. 46
EMERGENCY ENGINE SHUTDOWN .................................................................................................... 46
ENGINE FAILURE IN FLIGHT ............................................................................................................... 46
ELECTRICAL SYSTEM ................................................................................................ 47
DUAL GENERATOR FAILURE [L DC GEN] [R DC GEN] .................................................................... 47
TAWS AND GPWS ....................................................................................................... 49
TAWS OR GPWS WARNING ................................................................................................................. 49
TCAS II ......................................................................................................................... 50
TCAS II RESOLUTION ADVISORY ....................................................................................................... 50
WINDSHEAR ENCOUNTER ........................................................................................ 52
ESP ENGAGEMENT .................................................................................................... 52