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Surge tank air inlet................................................................................................................. CLEAR
Fuel water drain valves (3).................................................................................................NO LEAK
Static dischargers (elevator rudder).......................................................................................CHECK
* Lower fuselage structure (tail impact on runway).......................................................CONDITION
Flight records access door...................................................................................................CLOSED
* Fuel ventilation overpressure disc..................................................................................... INTACT
Applicable to:
APU
Access door..........................................................................................................................CLOSED
Air intake.........................................................................................................................CONDITION
Exhaust..................................................................................................................................CLEAR
Navigation light............................................................................................................... CONDITION
Fire extinguishing overpressure indication (red disc).........................................................IN PLACE
Applicable to: ,
APU
Access door..........................................................................................................................CLOSED
Air intake.........................................................................................................................CONDITION
Exhaust..................................................................................................................................CLEAR
Navigation light............................................................................................................... CONDITION
Fire extinguishing overpressure indication (red disc).........................................................IN PLACE
Applicable to:
LH AFT FUSELAGE
* Stabilizer, elevator, fin and rudder..............................................................................CONDITION
Outflow valve.................................................................................................................. CONDITION
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - EXTERIOR INSPECTION
A330/A340 FLEET PRO-NOR-SOP-05 P 12/16
FCOM 19 AUG 10
Applicable to: ,
LH AFT FUSELAGE
* Stabilizer, elevator, fin and rudder..............................................................................CONDITION
Outflow valve.................................................................................................................. CONDITION
Applicable to:
LH LANDING GEAR AND FUSELAGE
* Chocks......................................................................................................................... REMOVED
* Wheels and tires.........................................................................................................CONDITION
Brakes and brake wear indicator....................................................................................CONDITION
Hydraulic lines .......................................................................................................................CHECK
Landing gear structure........................................................................................................... CHECK
Downlock spring..................................................................................................................... CHECK
Safety pin..........................................................................................................................REMOVED
Applicable to: ,
LH LANDING GEAR AND FUSELAGE
* Chocks......................................................................................................................... REMOVED
* Wheels and tires.........................................................................................................CONDITION
Brakes and brake wear indicator....................................................................................CONDITION
Hydraulic lines .......................................................................................................................CHECK
Landing gear structure........................................................................................................... CHECK
Downlock spring..................................................................................................................... CHECK
　
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