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| | | tears, rupture, leakage and damaged | | | | | |
| | | paintwork (carefully examine the drag| | | | | |
| | | stay blend and the forward pintle pin| | | | | |
| | | areas). | | | | | |
| | |- the attachment fittings of the MLG | | | | | |
| | | | | | | | |
| D.| |Examine the shock absorber sliding rod | X | | | | |
| | |(the part you can see) for blue color, | | | | | |
| | |signs of bronze, chrome damage or | | | | | |
| | |external oil leaks. | | | | | |
| | |If you find damage: | | | | | |
| | |(1) Remove the shock absorber for | | X | | | |
| | | overhaul: | | | | | |
| | | (Ref. TASK 32-11-13-000-001) | | | | | |
| | | (refer to the manufacturer's | | | | | |
| | | instructions for the overhaul | | | | | |
| | | procedure). | | | | | |
| | | | | | | | |
| E.| |Examine the side stay assembly and its | X | | | | |
| | |attachment fittings for distortion, | | | | | |
| | |cracks and damaged paintwork and chrome| | | | | |
| | |plating. | | | | | |
| | |If you find damage: | | | | | |
| | |(1) Remove the side-stay assembly for | | X | | | |
| | | overhaul. | | | | | |
| | | (Ref. TASK 32-11-16-000-001) | | | | | |
| | | (refer to the manufacturer's | | | | | |
| | | instructions for the overhaul | | | | | |
| | | procedure). | | | | | |
| | |(2) Do the dimensional inspection of | | X | | | |
| | | the side-stay cardan pin-joint lugs| | | | | |
| | | on MLG leg. | | | | | |
| | | (Ref. TASK 32-11-00-200-004) | | | | | |
| | | If you find damage: | | | | | |
| | | - remove the MLG | | | X | | |
| | | (Ref. TASK 32-11-11-000-001) | | | | | |
| | |(3) On the aircraft, continue the | | X | | | |
R 1EFF : ALL 1 05-51-11Page 655 1 1 Nov 01/01 1 1 1CES 1
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A320飛機維護手冊 AMM 時間限制/維護檢查 3(121)
