FAA Approved Airplane Flight Manual Supplement

190-00716-02 Rev. 3 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 49 of 167
Section 3A - Abnormal Procedures
Table of Contents
AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 51
AILERON MISTRIM ................................................................................................................................ 51
ELECTRIC PITCH TRIM INOPERATIVE ............................................................................................... 52
ELEVATOR MISTRIM ............................................................................................................................. 53
RUDDER MISTRIM ................................................................................................................................. 54
FLASHING AMBER MODE ANNUNCIATION ....................................................................................... 55
YAW DAMPER AUTOMATIC DISCONNECT (Amber Flashing ‘YD’) ................................................. 55
YAW AXIS FAILURE .............................................................................................................................. 56
ELECTRONIC STABILITY AND PROTECTION .......................................................... 56
MANUAL ESP DISENGAGEMENT ........................................................................................................ 56
G1000 INTEGRATED AVIONICS SYSTEM ................................................................. 57
ALTITUDE MISCOMPARE ..................................................................................................................... 57
AIRSPEED MISCOMPARE .................................................................................................................... 60
PITCH MISCOMPARE ............................................................................................................................ 61
ROLL MISCOMPARE ............................................................................................................................. 61
HEADING MISCOMPARE ...................................................................................................................... 62
AMBER HEADING DISPLAY ................................................................................................................. 62
LOSS OF ALTITUDE REPORTING IN RVSM AIRSPACE .................................................................... 63
LOSS OF ALTITUDE ERROR CORRECTION....................................................................................... 63
DISPLAY UNIT FAILURE ............................................................................................. 64
PFD FAILURE ......................................................................................................................................... 64
MFD FAILURE ........................................................................................................................................ 65
DUAL GPS/SBAS FAILURE (AMBER “DR” OR “LOI” ON HSI) ......................................................... 65
GPS APPROACH INTEGRITY LIMITS EXCEEDED ............................................................................. 66
ILS DATABASE FREQUENCY AND/OR COURSE MISMATCH .......................................................... 67
LOSS OF TEMPERATURE INPUT ON BARO VNAV APPROACHES (VDI NO COMP on PFD) ....... 68
VDI MISCOMPARE ON BARO VNAV APPROACHES (VDI MISCOMP on PFD) ................................ 69
LOSS OF RADIO TUNING FUNCTIONS ............................................................................................... 69
FAILED AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED ............................................................ 70
FAILED ATTITUDE AND/OR HEADING ................................................................................................ 71
ENGINE INDICATION SYSTEM (EIS) FAILURE ................................................................................... 73