FAA Approved Airplane Flight Manual Supplement

190-00716-03 Rev. 3 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 41 of 139
Section 3A - Abnormal Procedures
Table of Contents
AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 43
AILERON MISTRIM ................................................................................................................................ 43
ELECTRIC PITCH TRIM INOPERATIVE ............................................................................................... 44
ELEVATOR MISTRIM ............................................................................................................................. 45
RUDDER MISTRIM ................................................................................................................................. 46
FLASHING AMBER MODE ANNUNCIATION ....................................................................................... 47
YAW DAMPER AUTOMATIC DISCONNECT (Amber Flashing ‘YD’) ................................................. 47
YAW AXIS FAILURE .............................................................................................................................. 48
ELECTRONIC STABILITY AND PROTECTION .......................................................... 48
MANUAL ESP DISENGAGEMENT ........................................................................................................ 48
G1000 INTEGRATED AVIONICS SYSTEM ................................................................. 49
ALTITUDE MISCOMPARE ..................................................................................................................... 49
AIRSPEED MISCOMPARE .................................................................................................................... 52
PITCH MISCOMPARE ............................................................................................................................ 53
ROLL MISCOMPARE ............................................................................................................................. 53
HEADING MISCOMPARE ...................................................................................................................... 54
LOSS OF ALTITUDE REPORTING IN RVSM AIRSPACE .................................................................... 54
LOSS OF ALTITUDE ERROR CORRECTION....................................................................................... 54
DISPLAY UNIT FAILURE ............................................................................................. 55
PFD FAILURE ......................................................................................................................................... 55
MFD FAILURE ........................................................................................................................................ 56
DUAL GPS/SBAS FAILURE (AMBER “DR” OR “LOI” ON HSI) ......................................................... 56
GPS APPROACH ALARM LIMITS EXCEEDED ................................................................................... 57
ILS DATABASE FREQUENCY AND/OR COURSE MISMATCH .......................................................... 58
LOSS OF RADIO TUNING FUNCTIONS ............................................................................................... 58
FAILED AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED ............................................................ 59
FAILED ATTITUDE AND/OR HEADING ................................................................................................ 60
ENGINE INDICATION SYSTEM (EIS) FAILURE ................................................................................... 62
LOSS OF NAVIGATION DATA .............................................................................................................. 62
INACCURATE FLIGHT DIRECTOR DISPLAY ...................................................................................... 62
BOTH ON ADC1, BOTH ON ADC2 ........................................................................................................ 63