A320飞机维护手册 AMM 时间限制/维护检查 2(69)

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**ON A/C ALL
 Subtask 05-51-18-210-086
 Q. Check after Damage on the Fuselage Skin
 NOTE : If there is damage to the aircraft structure, refer to the
____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures.
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Refer to the flow chart for the | |  X  | | | | | | | allowable damage and repair | | | | | | | | | (Ref. SRM). | | | | | | | | | (2) If you find a through hole: | |  X  | | | | | | | (a) Examine internally the | | | | | | | | | adjacent area of the damage | | | | | | | | | specially the components, the | | | | | | | | | pipes and the electrical looms| | | | | | | | | for damage. | | | | | | | | | If you find damage: | | | | | | | | | - repair or replace the | | |  X  | | | | | | related component. | | | | | | -------------------------------------------------------------------------------
R 1EFF : ALL 1 05-51-18Page 637 1 1 Aug 01/05 1 1 1CES 1

 **ON A/C 001-049, 101-105, 151-199, 201-210,

 Subtask 05-51-18-210-087-A
 R. Check of the APU after Damage on the APU Exhaust (Ref. TASK 49-00-00-710-010)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the APU exhaust | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the operational test of the | |  X  | | | | | | | APU | | | | | | | | | (Ref. TASK 49-00-00-710-010). | | | | | | -------------------------------------------------------------------------------
**ON A/C 051-099,
 Subtask 05-51-18-210-087
 R. Check of the APU after Damage on the APU Exhaust (Ref. TASK 49-00-00-710-004)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the APU exhaust | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the operational test of the | |  X  | | | | | | | APU | | | | | | | | | (Ref. TASK 49-00-00-710-004). | | | | | | -------------------------------------------------------------------------------
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 05-51-18Page 638 1201-210, 1Aug 01/05 1 1 1CES 1

 

R **ON A/C 106-149, 211-299, 301-399, 401-499,

 Subtask 05-51-18-210-087-B
 R. Check of the APU after Damage on the APU Exhaust (Ref. TASK 49-00-00-710-008)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the APU exhaust | | | | | | | | | during the inspection: | | | | | | | | | (1) Do the operational test of the | |  X  | | | | | | | APU | | | | | | | | | (Ref. TASK 49-00-00-710-008). | | | | | | -------------------------------------------------------------------------------
**ON A/C ALL
 Subtask 05-51-18-210-088
 S. Check after Damage on the Wings
 NOTE : If there is damage to the aircraft structure, refer to the
____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures.
 (Ref. TASK 27-84-00-710-001) (Ref. TASK 27-54-00-710-001) (Ref. TASK 27-64-00-710-001) (Ref. TASK 27-14-51-000-001)
 (Ref. TASK 27-14-51-400-001) (Ref. TASK 27-14-00-710-001)

 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the top or | | | | | | | | | bottom of the wings: | | | | | | | | | (1) Refer to allowable damage and | |  X  | | | | | | | repair (Ref. SRM) | | | | | | | | | | | | | | | | B.| | If you find damage on the slats: | | | | | | | | | (1) Refer to allowable damage and | |  X  | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Do the operational test of the | |  X  | | | |

　
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