FAA Approved Airplane Flight Manual Supplement

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air
FAA APPROVED Page 39 of 124
Section 3A - Abnormal Procedures
Table of Contents
AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 41
AILERON MIS-TRIM ............................................................................................................................... 41
ELECTRIC PITCH TRIM INOPERATIVE ............................................................................................... 41
ELEVATOR MIS-TRIM ............................................................................................................................ 42
RUDDER MIS-TRIM ................................................................................................................................ 43
FLASHING AMBER MODE ANNUNCIATION ....................................................................................... 44
YAW DAMPER AUTOMATIC DISCONNECT (Amber Flashing ‘YD’) ................................................. 44
ELECTRONIC STABILITY AND PROTECTION .......................................................... 44
MANUAL ESP DISENGAGEMENT ........................................................................................................ 44
G1000 INTEGRATED AVIONICS SYSTEM ................................................................. 45
ALTITUDE MISCOMPARE ..................................................................................................................... 45
AIRSPEED MISCOMPARE .................................................................................................................... 47
PITCH MISCOMPARE ............................................................................................................................ 48
ROLL MISCOMPARE ............................................................................................................................. 48
HEADING MISCOMPARE ...................................................................................................................... 48
DISPLAY UNIT FAILURE ............................................................................................. 49
PFD FAILURE ......................................................................................................................................... 49
MFD FAILURE ........................................................................................................................................ 50
DUAL GPS/SBAS FAILURE (AMBER “DR” OR “LOI” ON HSI) ......................................................... 51
GPS APPROACH ALARM LIMITS EXCEEDED ................................................................................... 52
ILS DATABASE FREQUENCY AND/OR COURSE MISMATCH .......................................................... 53
LOSS OF RADIO TUNING FUNCTIONS ............................................................................................... 53
FAILED AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED ............................................................ 54
FAILED ATTITUDE AND/OR HEADING ................................................................................................ 54
ENGINE INDICATION SYSTEM (EIS) FAILURE ................................................................................... 56
LOSS OF NAVIGATION DATA .............................................................................................................. 56
INACCURATE FLIGHT DIRECTOR DISPLAY ...................................................................................... 56
BOTH ON ADC1, BOTH ON ADC2 ........................................................................................................ 57
BOTH ON AHRS 1, BOTH ON AHRS 2 ................................................................................................. 57
BOTH ON GPS 1, BOTH ON GPS 2 ...................................................................................................... 57
USING ADC1 or ADC2 or XSIDE ADC .................................................................................................. 58