曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

* Lower fuselage structure (tail impact on runway).......................................................CONDITION
Applicable to: ALL
APU
Access doors........................................................................................................................CLOSED
Air intake.........................................................................................................................CONDITION
Drain...............................................................................................................CONDITION/NO LEAK
Oil cooler air outlet ................................................................................................................ CLEAR
Exhaust..................................................................................................................................CLEAR
Navigation light............................................................................................................... CONDITION
Fire extinguisher overpressure indication (red disc).......................................................... IN PLACE
Applicable to: ALL
LH AFT FUSELAGE
* Stabilizer, elevator, fin, and rudder.............................................................................CONDITION
* Potable water service door.............................................................................................. CLOSED
Ground hydraulic connection blue and green doors............................................................CLOSED
Hydraulic reservoir filling door............................................................................................. CLOSED
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - EXTERIOR INSPECTION
A318/A319/A320/A321 FLEET PRO-NOR-SOP-05 P 8/12
FCOM 19 AUG 10
Applicable to:
MSN,
LH LANDING GEAR
* Chocks......................................................................................................................... REMOVED
* Wheels and tires.........................................................................................................CONDITION
Brakes and brake wear indicator....................................................................................CONDITION
Torque link damper �� .................................................................................................CONDITION
Hydraulic lines........................................................................................................................ CHECK
Landing gear structure........................................................................................................... CHECK
Downlock springs................................................................................................................... CHECK
Safety pin..........................................................................................................................REMOVED
Applicable to: ,
, MSN,,
LH LANDING GEAR
* Chocks......................................................................................................................... REMOVED
* Wheels and tires.........................................................................................................CONDITION
Brakes and brake wear indicator....................................................................................CONDITION
Torque link damper.........................................................................................................CONDITION
Hydraulic lines........................................................................................................................ CHECK
Landing gear structure........................................................................................................... CHECK
Downlock springs................................................................................................................... CHECK
Safety pin..........................................................................................................................REMOVED
Applicable to: ALL
LH WING TRAILING EDGE
* Flaps and fairing......................................................................................................... CONDITION
* Control surfaces..........................................................................................................CONDITION
Static dischargers...................................................................................................................CHECK
Applicable to:
MSN,
LH WING LEADING EDGE
* Wing tip.......................................................................................................................CONDITION
Navigation light............................................................................................................... CONDITION
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320機組操作手冊FLIGHT CREW OPERATING MANUAL 11(125)