维修中英文填写.docx

……检查发现……1. 航后：检查发现左后航行灯不亮AF ：checked and found L AFT NAV light not on.2. 右前轮销磨损超标 R nose wheel worn out of limits.3. 检查发现2号ATC故障No.2 ATC fault.4. 左外刹车组件指示销磨损超标L outboard brake ASSY indicating pin worn out of limits.5. 左主起落架一液压管漏油超标a hydraulic tube of L MLG leakage out of limits.6. 13B 座位小桌板不能收起,无法保持在收上位seat 13B tray table could not be stowed and could not leave at stow position.更换（件）……，检査/测试正常1. 过站：更换右前轮，检查正常TR：Replaced R nose wheel，check OK.2. 更换2号ATC收发机后，测试正常检查正常replaced No.2 ATC transceiver，test OK. check OK.4. 更换左外刹车组件，增压检查正常。

Replaced L outboard brake ASSY， pressurization check OK.5. 更换左发右点火导线 Replaced L engine R ignition lead，6. 更换前起落架减振支柱充气活门，地面检查无渗漏 Replaced nose gear shock strut charging valve， no leakage in GND check.7. 更换左发17号风扇叶片，地面检查正常拆下：M/W31162,装 上 M/W30966Replaced L engine No.17 fan blade， GND check OK. part off：M/W31162， part on：M/W309668. 更换APU起动机，启动APU工作正常Replaced APU starter， APU start OK.9. 按照 MCC 要求，为了满足运输病人/残疾人要求，临时拆下第 3 排 ABC 座位座椅随机放在前货舱.According to MCC, for the requirement of patient/handicapped operation, remove seats A/B/C. The seats stored in FWD cargo in this flight.参考/按……更换……（件），测试……1. 根据工卡XXXX，更换电子/电气冷却供气风扇气滤，Per job card XXXX， replaced E/E cooling fan air filter，2. 更换左后航行灯灯泡，通电测试正常。

replaced L AFT NAV light bulb， power-on test was OK.3. 按工卡XXXX，更新FMC导航数据库Per job card XXXX， updated FMC NAV database.4. 参考AMM32-31-00，更换液压管，测试无渗漏Ref toX， replaced hydraulic tube， no leakage found in test.5. 更换时控件电瓶，安装固定测试工作正常replaced battery， test for installation OK.6. 根据波音标准线路施工手册 SWPM20-10-11 安装导线,检查测试正常 Refer to SWPM20-10-11 for wire installation procedures, check and test ok.7. 根据波音标准线路施工手册 SWPM20-10-19 分离导线,检查测试 正常 Refer to SWPM20-10-19 for wire separation procedures, check and test ok.检查发现…故障，按…保留，…号/类别，同意放行1. 过站发现前服务话筒失效，按 MEL23-20 保留，保留号 XXX。

TR found FWD attendant microphone malfunction， deferred referring toMEL23-30， No. XXX.2. 按 MEL34-36 保留， C 类，同意放行Per MEL34-36 defer ,category C， released.3. 按航线维护手册，操纵测试正常，渗油量符合放行标准，同意放 行Per AMM， control test OK， leakage within limits， released.4. 拔出P6面板上XX跳开关，并在上面安装固定卡子，挂好“INOP” 标牌后按MEL XXXX放行Pulled the circuit breaker XX in the P6 panel, installed a collar and a “INOP” label on circuit breaker XX, dispatched referring to MELXXXX.按…，更换…件，测试正常，撤消/关闭…保留1. ，撤消 XXXDD/FC rescind DD/FCXXX.2. 更新FMC导航数据库，通电测试工作正常，右HWAS地图方式 正常，并关闭MEL保留。

Update FMC NAV database， power-on test OK， R HWAS map OK， closed MEL defer item.3. 清洁并重装左GPS天线，地面测试正常，撤消XXXXX页上的 XXXXXX 保留Cleaned and reinstalled L GPS antenna， GND test OK， rescinded deferXXXXXX on page XXXXX.1. 雷达罩和右发进气道口有鸟击痕迹 Checked and found bird strike on radiome and R engine air inlet.2. 地面检查雷达罩和右发进气道正常，右发风扇叶片正常，涵道正常 GND check found radidme & R engine normal， engine fan blades & bypass normal.……（件）不工作/故障/故障灯亮1. 左发右点火器不工作 L engine R igniter INOP.2. 右 HWAS地图显示故障R HWAS map display fault.3. 巡航过程左右管道压力相差过大。

Much difference between L & R duct pressure during cruising4. 设备冷却系统供气正常位不工作 Equipment cooling system supply air INOP on NORM position.5. 第二部应答机 “ATC FAIL” 灯亮No.2 transponder “ATC FAIL ” light on.6. 空中气象雷达失效 Weather radar failed in flight.7. 副翼操纵作动筒漏油 Aileron control actuator leaked fluid.8. 自动驾驶 B 通道无法接通 Autopilot channel B couldn't engage.9. 空调流量小，制冷效果差 o Small air-conditioning flow, poor cooling.发现故障原因1. 航后发现前起落架镜面太低，结果发现是充气活门锁不死漏气所 致AF： found nose gear mirror too low， checked and found charging valve could't lock ,leaked air.2. 航后发现左外主轮扎伤见线。

AF： checked and found L outboard main wheel punctured out of limits3. 过站发现右外主轮磨损见线 TR： checked and found R outboard gear worn out of limits .为判断…故障/因为航材缺件，对串…件，测试…1. 与 B-2652 飞机对串磁带放像机，通电测试正常 Exchange tape reproducer with A/C B-2652， power-on test normal.2. 为判断B-2652自动刹车故障，将P2-2面板与B-2650对串，通电 测试正常 Troubleshooting for auto brake fault of A/C B-2652， robbed P2-2 from A/C B-2650， power-on test OK.3. 由于航材缺件，为判断故障，左右发对串引气调节器，试车检查 右发引气压力正常 Due to lacking of parts， for troubleshooting， interchanged bleed air regulator of R engine with L engine ， running-up test normal.4. 根据非例行工卡，将APU滑油量传感器与B-2652飞机对串，测 试正常。

Refer to NRC， exchanged APU oil QTY sensor with A/C B-2652， test OK.更换……件，试车检查……1. 更换右发引气调节器，试车正常，左右压力一致 Replaced R engine bleed air regulator， running-up test OK， pressure the same.1. 清洗设备冷却供气低流量传感器及插头，测试正常 Cleaned equipment cooling supply air low flow sensor & plug， test OK.2. 地面对DFCS做系统测试正常，清洁MCP板后插头，测试B通 道正常GND test for DFCS OK，cleaned MCP aft plug，test for channel B OK.3. 地面对ATC通电测试工作正常oGround power-on test for ATC OK.1. 接生产调度通知，B-2652飞机起落次数多/少记2个，现已更正Production notified two cycles reduced/ added on A/C B-2652.2. 接生产调度通知，机身加58分，左发减2分，右发减2分。

Production notified fifty-eight minutes added on airframe ， two minutes reduced On L and R engine.3. 接生产调度通知，正常起落减1个Production notified one cycle reduced.碎裂chipped有裂纹crazed飞机概况起泡has bubbles凹坑dent排r。