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Safety pin..........................................................................................................................REMOVED
Applicable to:
LH WING TRAILING EDGE
Jettison outlet......................................................................................................................NO LEAK
* Flaps and fairings....................................................................................................... CONDITION
* Control surfaces..........................................................................................................CONDITION
Static dischargers...................................................................................................................CHECK
Applicable to: ,
LH WING TRAILING EDGE
* Flaps and fairings....................................................................................................... CONDITION
* Control surfaces..........................................................................................................CONDITION
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - EXTERIOR INSPECTION
A330/A340 FLEET PRO-NOR-SOP-05 P 13/16
FCOM 19 AUG 10
Static dischargers...................................................................................................................CHECK
Applicable to:
LH WING TIP
Navigation light............................................................................................................... CONDITION
* Slats 7, 6, 5................................................................................................................ CONDITION
Surge tank air inlet................................................................................................................. CLEAR
Fuel water drain valve (surge tank)....................................................................................NO LEAK
Magnetic fuel levels L8 and L7...............................................................................................FLUSH
Wing fence......................................................................................................................CONDITION
* Fuel ventilation overpressure disc..................................................................................... INTACT
Applicable to: ,
LH WING TIP
Navigation light............................................................................................................... CONDITION
* Slats 7, 6, 5................................................................................................................ CONDITION
Surge tank air inlet................................................................................................................. CLEAR
Fuel water drain valve (surge tank)....................................................................................NO LEAK
Magnetic fuel levels L8 and L7...............................................................................................FLUSH
Wing fence......................................................................................................................CONDITION
* Fuel ventilation overpressure disc..................................................................................... INTACT
Applicable to:
ENG 1 LH SIDE
Oil fill access door .............................................................................................................. CLOSED
* Fan cowl door.................................................................................................CLOSED/LATCHED
* Drain mast..................................................................................................CONDITION/NO LEAK
* Engine inlet and fan blades............................................................................................... CHECK
Applicable to:
ENG 1 RH SIDE
ECU cooling air inlet...............................................................................................................CLEAR
Start Valve handle access and pressure relief door............................................................CLOSED
Turbine exhaust...................................................................................................................... CLEAR
Applicable to:
LH WING LEADING EDGE
Magnetic fuel levels L6, L5, L4 and L3.................................................................................. FLUSH
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
NORMAL PROCEDURES
STANDARD OPERATING PROCEDURES - EXTERIOR INSPECTION
A330/A340 FLEET PRO-NOR-SOP-05 P 14/16
FCOM 19 AUG 10
Fuel water drain valve (outer tank).....................................................................................NO LEAK
　
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