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* Slat 1...........................................................................................................................CONDITION
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 5/12
FCOM 19 AUG 10
Applicable to: ,
, MSN,,
RH CENTER WING
Yellow hydraulic bay door....................................................................................................CLOSED
Fuel panel...........................................................................................................................CLOSED
Magnetic fuel level.................................................................................................................. FLUSH
Fuel water drain valve tank................................................................................................ NO LEAK
Landing light....................................................................................................................CONDITION
* Slat 1...........................................................................................................................CONDITION
Applicable to: ALL
ENG 2 LH SIDE
Oil fill access door (CFM and IAE only).............................................................................. CLOSED
Master magnetic chip detector access door (IAE only)....................................................... CLOSED
* Thrust Recovery Nozzle (PW only)................................................................CLOSED/LATCHED
Hydraulic filter visual access door (PW only)...................................................................... CLOSED
* Fan cowl doors...............................................................................................CLOSED/LATCHED
* Drain mast..................................................................................................CONDITION/NO LEAK
* Engine inlet and fan blades............................................................................................... CHECK
Applicable to: ALL
ENG 2 RH SIDE
Vent inlet (CFM only)..............................................................................................................CLEAR
Pressure-relief/Start valve handle access door (CFM and IAE only).................................................
............................................................................................................................................CLOSED
Nose cowl pressure relief door (PW only)...........................................................................CLOSED
Engine oil fill access/starter air valve override access door (PW only)..............................................
............................................................................................................................................CLOSED
Master chip detector access door (PW only).......................................................................CLOSED
IDG servicing access door (PW only)..................................................................................CLOSED
Turbine exhaust .....................................................................................................................CLEAR
Pylon/access panel......................................................................................... CONDITION/CLOSED
Applicable to: ,
, MSN,,
RH WING LEADING EDGE
* Slats 2, 3, 4, 5............................................................................................................CONDITION
Magnetic fuel level.................................................................................................................. FLUSH
Fuel water drain valve........................................................................................................ NO LEAK
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 6/12
FCOM 19 AUG 10
Refuel coupling.....................................................................................................................CLOSED
Surge tank air inlet................................................................................................................. CLEAR
* Fuel ventilation overpressure disc..................................................................................... INTACT
Navigation..................................................................................................................... CONDITION
* Wing tip.......................................................................................................................CONDITION
　
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