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| | | 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 | | | | | |
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| | |serviceable components: | | | | | | 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 4
