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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.
R 1EFF : ALL 1 05-51-11Page 659 1 1 Nov 01/01 1 1 1CES 1 If you do not known the category, go directely to item 2. Inspection after severe hard/overweight landing.
R (Ref. TASK 78-36-00-010-040) (Ref. TASK 78-31-00-710-042) R (Ref. TASK 71-13-00-010-040)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the nacelles after | | | | | | | | |hard/overweight landing | | | | | | | | | | | | | | | | A.| |Examine externally the thrust reverser | X | | | | | | | |cowls for distortion, delamination, | | | | | | | | |cracks, cracked or flacking paint, | | | | | | | | |loose rivets and signs of shearing. | | | | | | | | |If you find damage: | | | | | | | | |(1) Open the thrust reverser cowls | | X | | | | | | | (Ref. TASK 78-36-00-010-040) | | | | | | | | |(2) Examine internally the thrust | | X | | | | | | | reverser cowls for damage. | | | | | | | | |(3) Examine all the thrust reverser | | X | | | | | | | cowl hinge fittings for distortion | | | | | | | | | cracks and damage. | | | | | | | | |(4) Examine all the thrust reverser | | X | | | | | | | cowl latches for damage and make | | | | | | | | | sure that operation is correct. | | | | | | | | |(5) Do an operational test of the | | X | | | | | | | thrust reverser system. Make sure | | | | | | | | | that the thrust reversers | | | | | | | | | move fully and freely | | | | | | | | | (Ref. TASK 78-31-00-710-042). | | | | | | | | | | | | | | | |2. | |Inspection of the nacelles after severe| | | | | | | | |hard/overweight landing | | | | | | | | | | | | | | | | A.| |Do the inspection of the nacelles after| X | | | | | | | |hard/overweight landing (Ref. item 1.) | | | | | | | | | | | | | | | | B.| |Examine externally the fan and air | X | | | | | | | |intake cowls for distortion, | | | | | | | | |delamination, cracks, cracked or | | | | | | | | |flacking paint, loose rivets and signs | | | | | | | | |of shearing. | | | | | | | | |If you find damage: | | | | | | | | |(1) Open the fan cowls | | X | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | (Ref. TASK 71-13-00-010-040) | | | | | | | | |(2) Examine internally the fan cowls | | X | | | | | | | for damage. | | | | | | | | |(3) Examine all the fan cowl hinge | | X | | | | | | | fittings for distortion and damage.| | | | | | | | |(4) Examine all the fan cowl latches | | X | | | | | | | for damage and make sure that | | | | | | | | | operation is correct. | | | | | | | | |(5) Examine the air intake cowl for | | X | | | | | | | distortion and damage. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-11-210-094
E. Inspection of the Pylons
(Ref. TASK 71-13-00-010-040) (Ref. TASK 78-36-00-010-040)
(Ref. TASK 71-00-00-000-042) (Ref. TASK 54-51-17-000-001)
(Ref. TASK 54-51-17-000-002) (Ref. TASK 54-51-17-200-001)
(Ref. TASK 54-51-17-200-002) (Ref. TASK 28-25-00-650-001)
(Ref. TASK 28-10-00-910-002) (Ref. TASK 54-51-17-400-001)
(Ref. TASK 54-51-17-400-002) (Ref. TASK 71-00-00-400-042)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Examine externally the pylon secondary | X | | | | | | | |structure and pylon box primary | | | | | | | | |structure (all the items you can see) | | | | | | | | |for buckling, cracks, pulled or missing| | | | | | | | |fasteners and other damage. | | | | | | | | |If you find damage: | | | | | | | A.| |Open the fan and the thrust reverser | | X | | | | | | |cowls | | | | | | | | |(Ref. TASK 71-13-00-010-040) | | | | | | | | |(Ref. TASK 78-36-00-010-040) | | | | | | | B.| |Examine externally the lower spar and | | X | | | | | | |pylon lower area (all the items you can| | | | | | | | |see) for shearing, distortion, cracks, | | | | | | | | |damaged paintwork and pulled or missing| | | | | | | | |fasteners. | | | | | | | | |If you find damage: | | | | | | | | |(1) Remove the pylon box access panels | | | X | | | 中國(guó)航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM 時(shí)間限制/維護(hù)檢查 2(11)
