常见缺陷及处理---起落架和轮舱区域.doc轮舱区域和起落架区域常见损伤:1舱门上的裂纹,凹坑,凿痕,穿刺,穿孔。损伤标准见SRM52-80-01和SRM52-80-022前起落架门封严组件,过站缺失或损坏可以按照CDL32-10-15放行飞机,航后更换;主起落架的刀型封严和封严组件详见CDL32-10-^73刹车止动片4收放作动筒传压筒锁作动筒转弯计量活门等的渗漏,各种管路接头,液压保险的渗漏,可以依据AMM29-00-00table601确定渗漏标准Table601/230<X)・993"PONENTSNORMALOPERATIONLIMITST】DISPATCHLIMITSTOAVOIDDELAY7】⑵⑶⑸Engine-DrivenPumpElectricMotor-.(Correctatthefirsttimepossible)(PONENTSNORMALOPERATIONLIMITS111DISPATCHLIMITSTOAVOIDDELAYR】,atanypressure•⑹1dropin10min.(Norepairisnecessary)30dropsin1min.(Correctatthefirsttimepossible)(WheelInstalledontheAirplane),TASK32-41-41・700-802*(1]entimeteror75600dropsinagallon.*(2]Makesuretheconnectionistightenedtothecorrecttorque.*[3]Astaticsealisasealbetweentwopartsthatdonotmoverelativetoeachother(Example:manifoldcovepumphousingcover).・[4]Leakagemaybecheckedwhiletheairplaneispark
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