Model 560XL Section III – Operating Procedures
AFM Cross Reference
Textron Aviation Citation 560XL 190-02313-03 Rev. 8
3-8 FAA Approved
TL DEICE FAIL L or R .......................................................................................................... UNCHANGED
UNLOCK (In Flight) ............................................................................................................... UNCHANGED
W/S FAULT L or R ................................................................................................................ UNCHANGED
W/S O’HEAT L or R .............................................................................................................. UNCHANGED
WINDSHEAR ......................................................................................................................... G5000 AFMS
Windshear Caution
WING ANTI-ICE L or R ......................................................................................................... UNCHANGED
WING O’HEAT L or R ........................................................................................................... UNCHANGED
WSHR FAIL .................................................................................................................. NOT APPLICABLE
WHITE MESSAGE PROCEDURES
AC BEARING L or R ............................................................................................................. UNCHANGED
AHRS AUX PWR 1 or 2 ........................................................................................................ UNCHANGED
APU GEN OFF ...................................................................................................................... UNCHANGED
BLEED VAL OPEN ............................................................................................................... UNCHANGED
EEC MANUAL L or R ............................................................................................................ UNCHANGED
ENG VIB L or R ..................................................................................................................... UNCHANGED
FUEL XFEED ........................................................................................................................ UNCHANGED
GND IDLE ............................................................................................................................. UNCHANGED
RANGE MISMATCH ..................................................................................................... NOT APPLICABLE
READY TO LOAD ................................................................................................................. UNCHANGED
SPD BRK EXTEND ............................................................................................................... UNCHANGED
TERRAIN INHIBIT ................................................................................................................. G5000 AFMS
TAWS Inhibit
TL DEICE PRESS L or R ...................................................................................................... UNCHANGED
EMERGENCY/ABNORMAL PROCEDURES
ENGINE
Engine Failure or Other Emergency During Takeoff ............................................................ UNCHANGED
Engine Failure During Final Approach ................................................................................... G5000 AFMS
Dual Engine Failure .............................................................................................................. UNCHANGED
Engine Failure/Precautionary Shutdown .............................................................................. UNCHANGED
In-Flight Restart – One Engine ............................................................................................. UNCHANGED
Engine Display Failure (Blank Display Channel) .......................................................... NOT APPLICABLE
Engine Display Faults ............................................................................................................ G5000 AFMS
Engine Indication System (EIS) Failure
Airstart Envelope ................................................................................................................... UNCHANGED
Maximum Glide – Emergency Landing ................................................................................. UNCHANGED
Oil Pressure High .................................................................................................................. UNCHANGED