FAA Approved Airplane Flight Manual Supplement
190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 31 of 137
Section 3 - Emergency Procedures
Table of Contents
AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 32
AUTOPILOT MALFUNCTION / PITCH TRIM RUNAWAY ..................................................................... 32
UNSCHEDULED RUDDER BOOST ACTIVATION ............................................................................... 33
MANUAL AUTOPILOT DISCONNECT .................................................................................................. 34
AUTOPILOT ABNORMAL DISCONNECT ............................................................................................. 34
AUTOPILOT FAILURE ........................................................................................................................... 35
PITCH AXIS FAILURE ............................................................................................................................ 36
ROLL AXIS FAILURE ............................................................................................................................. 36
PITCH TRIM FAILURE ........................................................................................................................... 37
AUTOPILOT PRE-FLIGHT TEST FAIL .................................................................................................. 37
AUTOPILOT OVERSPEED RECOVERY ............................................................................................... 38
AUTOPILOT UNDERSPEED PROTECTION ACTIVATION AND RECOVERY (ESP-Equipped
Aircraft Only) ................................................................................................ Error! Bookmark not defined.
ENGINE FAILURE (AUTOPILOT ENGAGED) ...................................................................................... 39
ELECTRICAL SYSTEM ................................................................................................ 39
DUAL GENERATOR FAILURE [L DC GEN] [R DC GEN] .................................................................... 39
LOAD MANAGEMENT TABLE .............................................................................................................. 40
TAWS AND GPWS ....................................................................................................... 41
TAWS OR GPWS WARNING ................................................................................................................. 41
TCAS II ......................................................................................................................... 41
TCAS II RESOLUTION ADVISORY ....................................................................................................... 41
WINDSHEAR ENCOUNTER ........................................................................................ 42
ESP ENGAGEMENT .................................................................................................... 42










