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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | - the sidestay attachment fitting,| | | | | | | | | - the MLG support rib, | | | | | | | | | - the riblets, stringers and | | | | | | | | | brackets. | | | | | | | | | Make sure that: | | | | | | | | | - there are no cracks, | | | | | | | | | - there is no damage, | | | | | | | | | - the paint and the sealant are not | | | | | | | | | damaged, | | | | | | | | | - the fasteners are in the correct | | | | | | | | | condition. | | | | | | | | | | | | | | | | C.| | Close access to the wing tanks | | | | | | | | | (Ref. TASK 28-10-00-910-002). | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-11-210-097
H. Inspection of the Flaps
(Ref. TASK 27-54-00-710-001) (Ref. TASK 27-54-00-200-001)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the flaps | | | | | | | | | | | | | | | | A.| | Do a visual inspection of the upper | X | | | | | | | | and inner surfaces of the inner and | | | | | | | | | outer flaps for distortion | | | | | | | | | | | | | | | | B.| | Do fully the operational test of the | X | | | | | | | | flap system | | | | | | | | | (Ref. TASK 27-54-00-710-001). | | | | | | | | | If there are indications of damage: | | | | | | | | | (1) Do the detailed visual inspection | | X | | | | | | | of the transmission assembly | | | | | | | | | (Ref. TASK 27-54-00-200-001). | | | | | | | | | (2) Do the detailed inspection of the | | X | | | | | | | flap attachment parts (drive arms | | | | | | | | | and brackets). | | | | | | -------------------------------------------------------------------------------
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Subtask 05-51-11-210-100
J. Inspection of the Fuselage
NOTE : This inspection contains two inspection procedures:
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item 1. Inspection after a hard/overweight landing
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item 2. Inspection after a severe hard/overweight landing.
If you know the category of the landing, go directly to the
necessary inspection.
If you do not known the category, go directely to item 2.
Inspection after severe hard/overweight landing.
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the fuselage after | | | | | | | | |hard/overweight landing | | | | | | | | | | | | | | | | A.| |Fuselage section between FR20 and FR35:| | | | | | | | |- From the ground, examine the lower | X | | | | | | | | skin for loose fasteners, cracked | | | | | | | | | or flaking paint or distortion. | | | | | | | | | | | | | | | | B.| |Fuselage section between FR35 and FR47 | | | | | | | | |- Examine the belly fairing panels | X | | | | | | | | for loose fasteners, cracked or | | | | | | | | | flaking paint, incorrect attachment | | | | | | | | | or delamination. | | | | | | | | |If you find damage: | | | | | | | | |(1) Remove the panels and examine | | X | | | | | | | internally the belly fairing for: | | | | | | | | | - the correct attachment of all | | | | | | | | | the components or loose rivets. | | | | | | | | |(2) Examine the fuselage skin | | X | | | | | | | externally below the belly fairing | | | | | | | | | zone for: | | | | | | | | | - buckling, loose rivets, cracked | | | | | | | | | or flaking paint. | | | | | | | | | | | | | | | | C.| |Fuselage section between FR47 and FR70 | | | | | | | | |- From the ground, examine the lower | X | | | | | | | | skin for loose fasteners, cracked | | | | | | | | | or flaking paint or distortion. | | | | | | | | | | | | | | | | 2.| |Inspection of the fuselage after severe| | | | | | | | |hard/overweight landing | | | | | | 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 2(16)
