曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
| | | (b) On the aircraft, inspect the | | X | | | |
| | | attachment fittings for damage| | | | | |
| | | if you find damage: | | | | | |
| | | - tell Airbus Industrie about | | | X | | |
| | | the results | | | | | |
| | | (7) Examine the NLG actuating cylinder| X | | | | |
| | | and its attachment fittings for | | | | | |
| | | distortion, cracks, pulled or torn| | | | | |
| | | fasteners and damaged paintwork. | | | | | |
| | | If you find damage: | | | | | |
| | | (a) Remove the actuating cylinder | | X | | | |
| | | for strip-down inspection | | | | | |
| | | (Ref. TASK 32-21-22-000-001) | | | | | |
| | | (refer to the manufacturer's | | | | | |
| | | instructions for the | | | | | |
| | | strip-down inspection). | | | | | |
| | | (b) On the aircraft, continue the | | X | | | |
| | | inspection of the attachment | | | | | |
| | | fittings for damage. | | | | | |
| | | If you find damage: | | | | | |
| | | - tell Airbus Industrie about | | | X | | |
| | | the results. | | | | | |
| | | (8) In the avionics compartment, | X | | | | |
| | | examine: | | | | | |
| | | - the gear-well roof, | | | | | |
| | | - the roof-to-sidewall joint, | | | | | |
| | | - the floor support-strut | | | | | |
| | | attach-fittings for distortion, | | | | | |
| | | cracks, pulled or torn fasteners| | | | | |
| | | and damaged paintwork. | | | | | |
| | | If you find damage: | | | | | |
| | | - tell Airbus Industrie about the | | X | | | |
-------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | |----|----|---------------------------------------|-----|-----|-----|----|----|
| | | results. | | | | | |
| | | (9) If you removed components, install| X | | | | |
| | | serviceable components: | | | | | |
| | | - for the actuating cylinder | | | | | |
| | | (Ref. TASK 32-21-22-400-001) | | | | | |
| | | - for the lockstay assembly | | | | | |
| | | (Ref. TASK 32-21-17-400-001) | | | | | |
| | | - for the NLG | | | | | |
| | | (Ref. TASK 32-21-11-400-002) | | | | | |
| | | - for the drag strut assembly | | | | | |
| | | (Ref. TASK 32-21-16-400-002) | | | | | |
| | | - for the shock absorber | | | | | |
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM 时间限制/维护检查 2(85)
