| | | inspection of the side-stay | | | | | |
| | | attachment fitting. | | | | | |
| | | | | | | | |
| F.| |Examine the lockstay assembly and | X | | | | |
| | |lockstay actuator for distortion, | | | | | |
| | |cracks and damaged paintwork and chrome| | | | | |
| | |plating. | | | | | |
| | |If you find damage: | | | | | |
| | |(1) Remove the lockstay assembly and | | X | | | |
| | | lockstay actuator for overhaul | | | | | |
| | | (Ref. TASK 32-11-17-000-001) | | | | | |
| | | (Ref. TASK 32-11-21-000-001) | | | | | |
| | | (refer to the manufacturer's | | | | | |
| | | instructions for the overhaul | | | | | |
| | | procedure). | | | | | |
| | |(2) On the aircraft, continue the | | X | | | |
| | | inspection of the attachment | | | | | |
| | | fittings for damage. | | | | | |
| | | | | | | | |
| G.| |Examine the MLG retraction actuator and| X | | | | |
| | |its attachment fittings for distortion,| | | | | |
| | |cracks and damaged paintwork and chrome| | | | | |
| | |plating. | | | | | |
| | |If you find damage: | | | | | |
| | |(1) Remove the retraction actuator for | | X | | | |
| | | strip-down inspection | | | | | |
| | | (Ref. TASK 32-31-46-000-001) | | | | | |
| | | (refer to the manufacturer's | | | | | |
| | | instructions for the | | | | | |
| | | strip-down procedure). | | | | | |
| | |(2) On the aircraft, continue the | | X | | | |
| | | inspection of the attachment | | | | | |
| | | fittings for damage. | | | | | |
| | | | | | | | |
| H.| |Examine the MLG well for distortion, | X | | | | |
| | |cracks, pulled or torn fasteners and | | | | | |
| | |damaged paintwork. | | | | | |
| | | | | | | | |
| I.| |Examine the electrical conduits, | X | | | | |
| | |connections, connectors and flexible | | | | | |
| | |conduits for damage. | | | | | |
| | | | | | | | |
| J.| |If you removed components, install | | | | | |
R 1EFF : ALL 1 05-51-11Page 656 1 1 Nov 01/01 1 1 1CES 1
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
| |CODE| | 1 | 2 | 3 |SIGN|FIG.|
|----|----|---------------------------------------|-----|-----|-----|----|----|
| | |serviceable components: | | | | | |
| | |- for the retraction actuator | | | | | |
| | | (Ref. TASK 32-31-46-400-001) | | | | | |
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 2(8)
