FAA Approved Airplane Flight Manual Supplement

ManualsBrandsGarmin ManualsFlight DecksGarmin MDL Rev 7, SA01535Wi_D

190-00716-02 Rev. 3 Hawker Beechcraft King Air 300/300LW

FAA APPROVED Page 35 of 167

Section 3 - Emergency Procedures

Table of Contents

AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 36

AUTOPILOT MALFUNCTION / PITCH TRIM RUNAWAY ..................................................................... 36

UNSCHEDULED RUDDER BOOST ACTIVATION ............................................................................... 37

MANUAL AUTOPILOT DISCONNECT .................................................................................................. 38

AUTOPILOT ABNORMAL DISCONNECT ............................................................................................. 38

AUTOPILOT FAILURE ........................................................................................................................... 39

PITCH AXIS FAILURE ............................................................................................................................ 40

ROLL AXIS FAILURE ............................................................................................................................. 40

PITCH TRIM FAILURE ........................................................................................................................... 41

AUTOPILOT PRE-FLIGHT TEST FAIL .................................................................................................. 41

AUTOPILOT OVERSPEED RECOVERY ............................................................................................... 42

AUTOPILOT UNDERSPEED PROTECTION ACTIVATION AND RECOVERY (ESP-Equipped

Aircraft Only) .......................................................................................................................................... 42

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ENGINE FAILURE .................................................................................................................................. 43

ENGINE FIRE OR FAILURE IN FLIGHT ........................................................................................... 43

ELECTRICAL SYSTEM ................................................................................................ 43

DUAL GENERATOR FAILURE [L DC GEN] [R DC GEN] .................................................................... 43

LOAD MANAGEMENT TABLE .............................................................................................................. 44

TAWS AND GPWS ....................................................................................................... 45

TAWS OR GPWS WARNING ................................................................................................................. 45

TCAS II ......................................................................................................................... 45

TCAS II RESOLUTION ADVISORY ....................................................................................................... 45

TCAS II RESOLUTION ADVISORY (GTS 8000) ................................................................................... 46

WINDSHEAR ENCOUNTER ........................................................................................ 47

ESP ENGAGEMENT .................................................................................................... 48