A320飞机维护手册 AMM 时间限制/维护检查 3(120)_航空信息_民用航空_通用航空

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Subtask 05-51-11-210-103
B. Inspection of the NLG Section of the Fuselage
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Fuselage-Nose/landing-gear section | | | | | | | | | between FR9 and FR20. | | | | | | | | | NOTE : This inspection is necessary if| | | | | | | | | you found damage during the | | | | | | | | | phase 1 checks of the NLG. | | | | | | | | | | | | | | | | A.| | Nose-gear upper-strut attachments | | | | | | | | | (FR14). | | | | | | | | | (1) Examine: | | X | | | | | | | - the area around the bearing, | | | | | | | | | - the attachment of the fitting on| | | | | | | | | FWD frame and roof of the nose | | | | | | | | | wheel well, | | | | | | | | | - the link rods. | | | | | | | | | | | | | | | | B.| | Nose-gear actuating cylinder | | | | | | | | | attachment-fitting (FR20). | | | | | | | | | (1) Examine the attachment of the | | X | | | | | | | actuating cylinder fitting to the | | | | | | | | | upper link at FR19 and FR20. | | | | | | | | | | | | | | | | C.| | Nose-gear leg attachments (FR19). | | X | | | | | | | (1) Examine the attachments at FR19 | | | | | | | | | and FR20 and the longitudinal | | | | | | | | | beams. | | | | | | -------------------------------------------------------------------------------
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C. Inspection of the Main Landing Gears
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.

(Ref. TASK 12-14-32-614-003) (Ref. TASK 32-41-00-210-002)
(Ref. TASK 32-11-00-200-006) (Ref. TASK 32-11-13-000-001)
(Ref. TASK 32-11-16-000-001) (Ref. TASK 32-11-00-200-004)
(Ref. TASK 32-11-11-000-001) (Ref. TASK 32-11-17-000-001)
(Ref. TASK 32-11-21-000-001) (Ref. TASK 32-31-46-000-001)
(Ref. TASK 32-31-46-400-001) (Ref. TASK 32-11-21-400-001)
(Ref. TASK 32-11-17-400-001) (Ref. TASK 32-11-11-400-001)
(Ref. TASK 32-11-16-400-001) (Ref. TASK 32-11-13-400-001)
(Ref. TASK 07-11-00-581-001) (Ref. TASK 32-11-00-200-005)
(Ref. TASK 32-31-00-720-002) (Ref. TASK 32-33-00-720-001)
(Ref. TASK 05-56-00-200-001) (Ref. TASK 07-11-00-586-002)

-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | |Inspection of the MLG after | | | | | | | | |hard/overweight landing | | | | | | | | |NOTE : You can do this inspection with | | | | | | | | | the aircraft on its wheels or on| | | | | | | | | jacks. | | | | | | | | | | | | | | | | A.| |Do a check of the pressure in the MLG | X | | | | | | | |shock absorber | | | | | | | | |(Ref. TASK 12-14-32-614-003) | | | | | | | | | | | | | | | | B.| |Do a visual inspection of the wheels | X | | | | | | | |for distortion, cracks, damaged | | | | | | | | |paintwork and correct installation. | | | | | | | | |Examine the side walls of the tires for| | | | | | | | |damage | | | | | | | | |(Ref. TASK 32-41-00-210-002) | | | | | | | | |If you find damage. | | | | | | | | |(1) Do the inspection of the axle and | | X | | | | | | | the axle sleeve for damage and | | | | | |
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