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Subtask 05-51-15-210-052
C. Inspection of the Fuselage (FR35 to FR50)
(Ref. TASK 32-11-00-200-001)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Belly Fairing | | | | | | | | | | | | | | | | A.| | Examine the belly fairing panels for | X | | | | | | | | holes, delamination, cracked or | | | | | | | | | flaking paint and loose fasteners. | | | | | | | | | Make sure that the panels are | | | | | | | | | correctly attached. | | | | | | R | | | If you find damage: | | | | | | | | | (1) Remove the panels and internally | | X | | | | | | | examine the belly fairing | | | | | | | | | structure for buckling, cracks and| | | | | | | | | damaged paintwork. | | | | | | R | | | (2) Examine: | | X | | | | | | | - the pipes | | | | | | | | | - the ducts | | | | | | | | | - the electrical looms | | | | | | | | | - the mounts | | | | | | | | | for fluid leakage, distortion, | | | | | | | | | rupture, breaks, cracks. | | | | | | | | | Make sure that the components are | | | | | | | | | correctly attached and examine the | | | | | | | | | condition of the safety devices. | | | | | | | | | | | | | | | |2. | | Main Landing-Gear Well | | | | | | | | | | | | | | | | A.| | In the main landing-gear well, examine| X | | | | | | | | the protective panels and the | | | | | | | | | structure for distortion, cracks, | | | | | | | | | pulled or torn fasteners, honeycomb | | | | | | | | | delamination, core damage. | | | | | | | | | | | | | | | | B.| | Examine the main landing gear and | X | | | | | R | | | specially: | | | | | | | | | - the pipes | | | | | | | | | - the ducts | | | | | | | | | - the electrical looms | | | | | | | | | - the mounts | | | | | | | | | - the control actuators | | | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | for fluid leakage, distortion, | | | | | | | | | rupture, breaks, cracks. | | | | | | | | | Make sure that the components are | | | | | | | | | correctly attached and examine the | | | | | | | | | condition of the safety devices | | | | | | | | | (Ref. TASK 32-11-00-200-001). | | | | | | | | | | | | | | | | 3. | | Main Landing-Gear Main-Doors | | | | | | | | | | | | | | | R | A.| | Examine: | X | | | | | | | | - the door | | | | | | | | | - the hinges | | | | | | | | | - the actuating cylinder attachments | | | | | | | | | - the sequence valve mounts | | | | | | | | | - the linkage | | | | | | | | | for distortion, cracks, pulled or torn| | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | | | | | | | | B.| | Examine the actuating cylinder, the | X | | | | | | | | sequence valve, the hoses and the | | | | | | | | | pipes for distortion, cracks, rupture | | | | | | | | | and fluid leakage. Also examine the | | | | | | | | | condition of the safety devices. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-15-210-053
D. Inspection of the Nacelles, Engines and Pylons R (Ref. TASK 71-13-11-200-001) (Ref. TASK 72-00-00-200-006)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Nacelles and Engine | | | | | | | | | | | | | | | | A.| | Externally examine the nacelle and the| X | | | | | R | | | primary nozzle for: | | | | | | | | | distortion, cracks, delamination, | | | | | | | | | cracked or flaking paint, loose rivets| | | | | | | | | and signs of shearing. | | | | | | | | | If you find damage: | | | | | | | | | (1) Open the cowls and internally | | X | | | |
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本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 2(41)
