-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | NOTE : The subsequent tests are only | | | | | | | | | applicable if the inspection | | | | | | | | | showed damage to a flight | | | | | | | | | control surface, the landing | | | | | | | | | gears or doors or the | | | | | | | | | adjacent structure. | | | | | | | A. | | Do an operational test of the thrust | X | | | | | | | | reverser system as specified in the | | | | | | | | | inspection procedure | | | | | | | | | (Ref. TASK 78-31-00-710-042). | | | | | | | | | | | | | | | | B.| | Do an operational test of the aileron.| | X | | | | | | | Make sure that the travel is full and | | | | | | | | | that the related controls do not catch| | | | | | | | | or become blocked | | | | | | | | | (Ref. TASK 27-14-00-710-001). | | | | | | | | | | | | | | | | C.| | Do an operational test of the flaps | | X | | | | | | | and the slats. Make sure that the | | | | | | | | | travel is full and that the related | | | | | | | | | controls do not catch or become | | | | | | | | | blocked | | | | | | | | | (Ref. TASK 27-54-00-710-001) | | | | | | | | | (Ref. TASK 27-84-00-710-001). | | | | | | | | | | | | | | | | D.| | Do an operational test of the | | X | | | | | | | spoilers. | | | | | | | | | Make sure that the travel is full and | | | | | | | | | that the related controls do not catch| | | | | | | | | or become blocked | | | | | | | | | (Ref. TASK 27-64-00710-001). | | | | | | | | | | | | | | | | E.| | Do a retraction test of the landing | | X | | | | | | | gear. Make sure that the travel is | | | | | | | | | smooth and that the related controls | | | | | | | | | do not catch or become blocked | | | | | | R | | | (Ref. TASK 32-30-00-867-001) | | | | | | | | | (Ref. TASK 32-30-00-867-002). | | | | | | -------------------------------------------------------------------------------
INSPECTION AFTER BRAKE EMERGENCY APPLICATION OR OVERHEAT - INSPECTION/CHECK___________________________________________________________________________
TASK 05-51-16-200-001
Inspection After Brake Overheat
R R R R WARNING : DO NOT GO NEAR A HOT WHEEL FOR ONE HOUR AFTER A BRAKE OVERHEAT IF THE_______ TIRE IS INFLATED, EXCEPT TO PUT THE WHEEL CHOCKS IN POSITION. IF YOU MUST GO NEAR THE WHEEL, GO FROM THE FRONT OR THE REAR BUT NOT FROM THE SIDE OF THE WHEEL. THERE IS A RISK OF A TIRE BURST.
WARNING : LET THE BRAKES AND THE WHEELS BECOME COOL BEFORE YOU GO NEAR THE_______ LANDING GEAR. DO NOT APPLY A LIQUID OR GAS FIRE EXTINGUISHER DIRECTLY ON A HOT WHEEL OR BRAKE UNIT. THIS COULD CAUSE AN EXPLOSION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______ GEAR.
WARNING : DO NOT RECOMMEND THE USE OF POWDER EXTINGUISHANTS. THE DEPOSITS_______ SMOTHER THE FIRE BUT THEY ALSO LIMIT THE DISSIPATION OF THE HEAT AND THIS CAN CAUSE PERMANENT STRUCTURAL DAMAGE TO : - BRAKE - WHEEL - AXLE YOU MUST NOT APPLY THE EXTINGUISHANT (EVEN WATER MIST) WITH A SPRAY GUN DIRECTLY ON THE CARBON HEAT PACK OF THE BRAKE. THIS CAN CAUSE THERMAL SHOCK.
1. Reason for the Job__________________
R R R R R R R This inspection is necessary after a crew report of: - a brake temperature of more than 900 deg.C, - wheel fuse plug(s) melt. The temperature of the brakes can be too high after: - an acceleration-stop, - the emergency application of the brakes, - frequent use of the brakes, - a failure of the braking control. If the temperature of the brakes is too high, one or more of the fuse plugs can melt. This causes: - damage to the tire, - possible damage to the wheel, - too much load on the opposite tire. This can cause damage to the tire.
2. Job Set-up Information 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 时间限制/维护检查 4(36)
