A320飞机维护手册 AMM 时间限制/维护检查 3(105)

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Subtask 05-51-11-210-055
 F. Inspection of the Engine (Ref. TASK 72-00-00-200-008) (Ref. TASK 71-00-00-710-008) (Ref. TASK 79-00-00-281-002) (Ref. TASK 71-00-00-000-042)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Examine the engine | | | | | | | | | | | | | | | |  A.| | Turn the fan rotor by hand. Make sure |  X  | | | | | | | | that there is no bearing roughness, | | | | | | | | | unusual noises and bindings (high | | | | | | | | | rubbing of the seals and the shrouds | | | | | | | | | is normal). | | | | | | | | | | | | | | | |  B.| | Examine the primary nozzle. Make sure |  X  | | | | | | | | that : | | | | | | | | | - it is correctly attached to the | | | | | | | | | engine | | | | | | | | | - there are no distortion or cracks, | | | | | | | | | no loose rivets, no signs of | | | | | | | | | shearing or delamination. | | | | | | | | | | | | | | | |  C.| | Examine the nose cowl attachments to  |  X  | | | | | | | | the fan case. Make sure that there are| | | | | | | | | no distortion, delamination, cracks, | | | | | | | | | pulled or torn fasteners. | | | | | | | | | If you find damage : | | | | | | | | | (1) Do an inspection of the engine | |  X  | | | | | | | after rough landing | | | | | | | | | (Ref. TASK 72-00-00-200-008). | | | | | | | | | (2) If you find seal or shroud | |  X  | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | interference and you think it is | | | | | | | | | minor : | | | | | | | | | - the engine is serviceable after | | | | | | | | | you do a satisfactory power | | | | | | | | | assurance check | | | | | | | | | (Ref. TASK 71-00-00-710-008). | | | | | | | | | (3) After the test, examine the | |  X  | | | | | | | magnetic chip detectors and the | | | | | | | | | elements of the scavenge oil | | | | | | | | | filter. | | | | | | | | | Make sure that there are no sign | | | | | | | | | of bearing distress | | | | | | | | | (Ref. TASK 79-00-00-281-002). | | | | | | | | | If you find damage : | | | | | | | | | (a) Remove the engine | | |  X  | | | | | | (Ref. TASK 71-00-00-000-042). | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-11-210-056
 G. Landing Gear Inspection (Ref. TASK 32-11-00-200-001) (Ref. TASK 05-56-00-200-001) (Ref. TASK 07-11-00-581-001) (Ref. TASK 32-11-13-000-001) (Ref. TASK 32-21-13-000-001) (Ref. TASK 12-14-32-614-004) (Ref. TASK 32-41-00-210-002)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Main Landing Gear | | | | | | | | | | | | | | | |  A.| | Do an inspection of the MLG |  X  | | | | | | | | (Ref. TASK 32-11-00-200-001). | | | | | | | | | | | | | | | |  B.| | If there are signs of damage, do an | |  X  | | | | | | | alignment check of the MLG, the axles | | | | | | | | | and the main fitting | | | | | | | | | (Ref. TASK 05-56-00-200-001). | | | | | | | | | | | | | | | |  C.| | If the dimensions are more than | | |  X  | | | | | | given in TASK 05-56-00-200-001 : | | | | | | | | | | | | | | | | | | (1) Lift the aircraft | | | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
 | |CODE| |  1  |  2  |  3  |SIGN|FIG.|
 |----|----|---------------------------------------|-----|-----|-----|----|----|

 |  |  |  (Ref. TASK 07-11-00-581-001).  |  |  |  |  |  |
 |  |  | (2) Remove the shock absorber from  |  |  |  |  |  |
 |  |  |  the main fitting  |  |  |  |  |  |
 |  |  |  (Ref. TASK 32-11-13-000-001).  |  |  |  |  |  |
 |  |  | (3) Remove and examine these items:  |  |  |  |  |  |
 |  |  |  - the retainer pin,  |  |  |  |  |  |
　
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