FAA Approved Airplane Flight Manual Supplement

190-00716-03 Rev. 4 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 51 of 173
Section 3A - Abnormal Procedures
Table of Contents
AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 53
AILERON MISTRIM ................................................................................................................................ 53
ELECTRIC PITCH TRIM INOPERATIVE ............................................................................................... 54
ELEVATOR MISTRIM ............................................................................................................................. 55
RUDDER MISTRIM ................................................................................................................................. 56
FLASHING AMBER MODE ANNUNCIATION ....................................................................................... 57
YAW DAMPER AUTOMATIC DISCONNECT (Amber Flashing ‘YD’) ................................................. 57
YAW AXIS FAILURE .............................................................................................................................. 58
ELECTRONIC STABILITY AND PROTECTION .......................................................... 58
MANUAL ESP DISENGAGEMENT ........................................................................................................ 58
G1000 INTEGRATED AVIONICS SYSTEM ................................................................. 59
ALTITUDE MISCOMPARE ..................................................................................................................... 59
AIRSPEED MISCOMPARE .................................................................................................................... 62
PITCH MISCOMPARE ............................................................................................................................ 63
ROLL MISCOMPARE ............................................................................................................................. 63
HEADING MISCOMPARE ...................................................................................................................... 64
AMBER HEADING DISPLAY ................................................................................................................. 64
LOSS OF ALTITUDE REPORTING IN RVSM AIRSPACE .................................................................... 65
LOSS OF ALTITUDE ERROR CORRECTION....................................................................................... 65
DISPLAY UNIT FAILURE ............................................................................................. 66
PFD FAILURE ......................................................................................................................................... 66
MFD FAILURE ........................................................................................................................................ 67
DUAL GPS/SBAS FAILURE (AMBER “DR” OR “LOI” ON HSI) ......................................................... 67
GPS APPROACH INTEGRITY LIMITS EXCEEDED ............................................................................. 69
ILS DATABASE FREQUENCY AND/OR COURSE MISMATCH .......................................................... 69
LOSS OF TEMPERATURE INPUT ON BARO VNAV APPROACHES (VDI NO COMP on PFD) ....... 70
VDI MISCOMPARE ON BARO VNAV APPROACHES (VDI MISCOMP on PFD) ................................ 71
LOSS OF RADIO TUNING FUNCTIONS ............................................................................................... 71
FAILED AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED ............................................................ 72
FAILED ATTITUDE AND/OR HEADING ................................................................................................ 73
ENGINE INDICATION SYSTEM (EIS) FAILURE ................................................................................... 75