FAA Approved Airplane Flight Manual Supplement

190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 43 of 141
Section 3A - Abnormal Procedures
Table of Contents
AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 45
AILERON MIS-TRIM ............................................................................................................................... 45
ELECTRIC PITCH TRIM INOPERATIVE ............................................................................................... 46
ELEVATOR MIS-TRIM ............................................................................................................................ 47
RUDDER MIS-TRIM ................................................................................................................................ 48
FLASHING AMBER MODE ANNUNCIATION ....................................................................................... 49
YAW DAMPER AUTOMATIC DISCONNECT (Amber Flashing ‘YD’) ................................................. 49
YAW AXIS FAILURE .............................................................................................................................. 50
ELECTRONIC STABILITY AND PROTECTION .......................................................... 50
MANUAL ESP DISENGAGEMENT ........................................................................................................ 50
G1000 INTEGRATED AVIONICS SYSTEM ................................................................. 51
ALTITUDE MISCOMPARE ..................................................................................................................... 51
AIRSPEED MISCOMPARE .................................................................................................................... 54
PITCH MISCOMPARE ............................................................................................................................ 55
ROLL MISCOMPARE ............................................................................................................................. 55
HEADING MISCOMPARE ...................................................................................................................... 56
LOSS OF ALTITUDE REPORTING IN RVSM AIRSPACE .................................................................... 56
LOSS OF ALTITUDE ERROR CORRECTION....................................................................................... 56
DISPLAY UNIT FAILURE ............................................................................................. 57
PFD FAILURE ......................................................................................................................................... 57
MFD FAILURE ........................................................................................................................................ 58
DUAL GPS/SBAS FAILURE (AMBER “DR” OR “LOI” ON HSI) ......................................................... 58
GPS APPROACH ALARM LIMITS EXCEEDED ................................................................................... 59
ILS DATABASE FREQUENCY AND/OR COURSE MISMATCH .......................................................... 60
LOSS OF RADIO TUNING FUNCTIONS ............................................................................................... 60
FAILED AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED ............................................................ 61
FAILED ATTITUDE AND/OR HEADING ................................................................................................ 62
ENGINE INDICATION SYSTEM (EIS) FAILURE ................................................................................... 64
LOSS OF NAVIGATION DATA .............................................................................................................. 64
INACCURATE FLIGHT DIRECTOR DISPLAY ...................................................................................... 64
BOTH ON ADC1, BOTH ON ADC2 ........................................................................................................ 65