英文维修记录填写参考ME.docx

1、英文维修记录填写参考ME第第一部分 航线维修记录常用语句检查发现/报告故障1. 航后：检查发现左后航行灯不亮。After Flight(AF )：Find L AFT position light is not on.2. 检查发现右前轮磨损超标。Check R tire of the nose landing gear is worn out of limits.3. 检查发现2号ATC故障。Check ATC system No.2 ATC fails.4. 检查发现左外刹车组件磨损超标。Check L outboard wear indicator pin of MLG brake as

2、sy is out of limits.航后检查发现：(AF Check)AF Check ：Check L outboard wear indicator pin of MLG brake assy is out of limits.Accomplish Task Card：TZ-AF-03，check L outboard wear indicator pin of MLG brake assy is out of limits.过站检查发现：(TR check)TR check : Check L outboard wear indicator pin of MLG brake assy

3、 is out of limits.Accomplish Task：TZ-TR-00，Check L outboard wear indicator pin of MLG brake assy is out of limits.5. 检查发现左主起落架一液压管漏油超标。Check the L MLG hydraulic tube leakage is out of limits.6. 检查发现13B座位小桌板不能收起，无法保持在收上位。Check the NO.13B passenger tray table could not be stowed and hold on the stow p

4、osition.Accomplish Task：xx-xx-xx，Check the NO.13B passenger tray table could not be stowed and hold on the stow position.（完成xx-xx-xx工卡发现）AF Check ：Check the NO.13B passenger tray table could not be stowed and hold on the stow position（航后检查发现）TR check : Check the NO.13B passenger tray table could not

5、 be stowed and hold on the stow position（过站检查发现）7机组报告空中右发燃油滤旁通灯亮。The flight crew reported right engine Fuel FILTER BYPASS Light came on in flight.8. 航后APU自检有49-41012故障信息.AF Check: maintenance message 49-41012 is displayed after APU BITE.9. 前洗手间“有人、无人”标牌松动。The “None/Occupied” placard in forward lavat

6、ory is loosening.参考/按.更换（件），检查 / 测试正常1. 过站：根据AMM32-45-21更换右前轮，并根据AMM 12-15-51/301检查轮胎气压正确。TR Check：Refer to AMM32-45-21 to replace the R nose wheel，and refer to AMM 12-15-51/301 to check the tire pressure，ensure the tire pressure is normal.2. 根据AMMXX-XX-XX更换2号ATC收发机，并根据AMMXX-XX-XX对系統完成测试，结果正常。Refer

7、to AMMxx-xx-xx to replace the No.2 ATC transceiver，and Refer to AMMxx-xx-xx to do a system function test，the result is normal.3. 航后根据AMM49-41-11更换APU起动机，启动测试APU工作正常。 AF: Refer to AMM49-41-11 to replace the APU starter，start APU and do an operation test，the result is normal.4. 过站根据AMM25-22-00折下第三排ABC

8、座椅，座椅随机放在前货舱。TR：Refer to AMM25-22-00 to remove the passenger seats 3A/3B/3C，and leave in the FWD cargo compartment.5. 根据工卡XXXX，更换时控件电瓶，根据AMMXX-XX-XX测试电瓶电压为XX伏，符合手冊要求。Refer to task card xxxx to replace the time control battery，AMMxx-xx-xx to test the voltage is XX volt，and satisfy to AMM requiements.

9、检查发现故障，按保留，号/类别，同意放行1. 过站检查发现前服务话筒失效，按MEL23-20放行飞机。 TR Check: Find the FWD attendant handset failed，refer to MEL23-20 to dispatch. 或：Accomplish Task card：TZ-TR-00，Find the FWD attendant handset failed，refer to MEL23-20 to dispatch.2. 航后检查发现右发PRSOV失效，因航材无料，根据MEL36-5完成M项工作，将右发PRSOV锁关位放行，在右发引气电门处贴不工作标牌

10、，并办理保留DD3000000。AF Check: Find the R engine PRSOV failed. Accomplish maintenance (M) items per MEL36-5 and lock the PRSOV in close position prior dispatch due to lacking of spare parts. Paste the“R ENGINE BLEED AIR SYSTEM INOP”tag next to the R engine bleed air switch，The deferred defect form NO. is

11、 DDXXXXXXX.按，更换件，测试正常，撤消 / 关闭保留1. 航后依据AMM23-20-00，更换前服务话筒，并完成功能测试结果正常，撤消DD/FCXXXXX。AF：Refer to AMM23-20-00 to replace the FWD attendant handset， Accomplish a function test and the result is normal，rescind deferred item DD/FCXXXXX.2. 航后根据AMM36-11-04, 更换右发PRSOV，并根据AMM36-11-04完成功能测试，结果正常，撤除DDXXXXXAF: R

12、eplaced the right engine PRSOV refer to AMM36-11-04, and accomplish the function test per AMM36-11-04, the result was normal, close the DDXXXXX.遭 遇 冰雹/鸟 击1. 过站检查发现雷达罩和右发进气道口有鸟击痕迹，根据AMM05-51-18完成冰雹/鸟击后的检查，并根据AMM27-81-00/27-51-00完成前/后缘襟翼的操作测试，结果正常。TR Check/ Do Task Card：TZ-TR-00，find a Bird/Hail Strik

13、e track on the radome and the R engine inlet cowl，refer to AMM05-51-18 to accomplish the Bird/Hail Strike Conditional Inspection，and refer to AMM27-81-00/27-51-00 to do a operation test of leading edge device and trailing edge flap，the result is normal.为判断故障/因为航材缺件，对串件，测试1. 为判断B-2652自动刹车故障，根据AMMXX-X

14、X-XX将P2-2面板与B-2650对串，并完成系统功能测试，结果正常。For troubleshooting of auto brake system of B-2652，refer to AMMxx-xx-xx to interchange the P2-2 with B-2650，and do a function test，the result is normal.2. 由于航材缺件，为判断右发引气故障，根据AMMXX-XX-XX对串左右发引气调节器，试车检查结果如下:左发:N1=XX 引气压力为XX PSI; N1=XX 引气压力为XX PSI; 右发:N1=XX 引气压力为XX P

15、SI; N1=XX 引气压力为XX PSI;引气压力正常。For troubleshooting of R engine bleed air system abnormal，refer to AMMxx-xx-xx to interchange bleed air regulator with L engine due to lacking of spare parts，do the engine running-up test，the test parameters are following：L Engine：N1=xx%，Bleed air pressure=xx PSI；N1=xx%，

16、Bleed air pressure=xx PSI；R Engine：N1=xx%，Bleed air pressure=xx PSI；N1=xx%，Bleed air pressure=xx PSI；bleed air pressure is normal.更换件，试车检查1. 根据AMMXX-XX-XX更换右发引气压力调节器，试车数据如下: N1=XX 引气压力为XX PSI; N1=XX 引气压力为XX PSI，结果正常。Replaced the R engine bleed air regulator according to AMMXX-XX-XX，and did the engin

17、e operation test, the data was: N1=XX, bleed air pressure= XX PSI; N1=XX bleed air pressure =XX PSI; the result was ok. Refer to AMMxx-xx-xx to repalce the R engine bleed air pressure regulator，the relative data parameters are following: N1=xx%，Bleed air pressure=xx PSI；N1=xx%，Bleed air pressure=xx

18、PSI；the bleed air pressure is normal.第二部分 飞机/故障基础语句飞 机 概 况排 row（如：第5排译作row 5）飞机 A/C（是aircraft 的英文缩写形式）机头 nose机腹 belly蒙皮 skin机身 airframe翼肋 rib翼梁 spar 机翼 wing翼尖 wing tip前缘 leading edge后缘 trailing edge客舱 cabin 或 passenger compartment货舱 cargo compartment轮舱 wheel well 缩写W/W驾驶舱 cockpit/ flight deck设备舱 equ

19、ipment bay窗 window滑窗 sliding window门窗 door mounted window旅客窗 passenger cabin window座位 seat过道 aisle地板 floor天花板 ceiling行李架 stowage bin杆 lever or stick or column操纵面 control surface操纵杆 control column控制面板 control panel手柄 handle开关/电门 switch正常位 NORM备用位 ALTN人工 manual自动 auto选择 select (注：通常也用缩写形式SEL）按钮 button

20、旋钮 knob 方 位 描 述左 left 缩写L 或 LH右 right 缩写R 或 RH前部 forward 缩写fwd后部 afterward 缩写aft上面 upper下面 lower左上 upper left右下 lower right左前 left forward右后 right afterward 内侧 inboard 缩写 I/B外侧 outboard 缩写 O/B 左内侧 left inboard在之间 betweenand航 材胶 adhesive销子 pin 例如 安全销safety pin插头 plug插座 socket插针 pin电阻 resistor线路 wire引

21、线 lead螺帽 nut螺栓 bolt螺钉 screw跳开关 circuit breaker继电器 relay隔离垫 spacer遮光板 glare shield消耗航材 consumable material故障描述航前检查 preflight (PF)check航后检查 after flight (AF)check过站检查 transit(TR) check定检 scheduled maintenance发现 find或reveal故障 trouble 或 failure 或 fault失效 fail 或 malfunction不能 fail to或 cant不灭 did not turn

22、/go off不亮 did not turn/come on不冲水 did not flush关不上 did not turn off不工作 inoperative 缩写 INOP不一致 disagree不对称 asymmetric不保持在应处位置 did not stay in position工作不稳定 rough工作稳定 smoothly难以读数 hard to read难以使用 hard to operate丢失 lost 或 missing雷击 lightning strike鸟击 bird strike卡阻 jammed松动 loose脱落 fall off剥落 delaminat

23、ed裂缝 cracked碎裂 chipped有裂纹 crack有刮痕 scratched起泡 has bubbles凹坑 dent损坏 damaged破损 broken烧蚀 burn through烧坏 burn out扎伤 punctured磨损 wearing 或 worn超标 out of limits见线 exposed threads泄露 leak（注：也常用名词leakage） 脏污 dirty压力大 high pressure压力小/量少 low pressure/quantity低压力/量小 low pressure/quantity无热水 no hot water无水 no

24、water过热 overheat关车 shutdown超速 overspeed断开 disconnected空瓶 empty堵塞 plugged溢出 overflowed气味难闻 smelled bad质量差 poor quality需调整 needed adjustment需修理 needs service密封圈破损/丢失 seal broken/missing支柱/吊舱拖地或损坏 strut / nacelle dragged or damaged已用过 used未收好 did not stow金属屑 metal particles测试电门 test switch电源测试 PWR TEST

25、灰尘过大状况 extreme dust condition方式控制面板 mode control panel人工活门指示器 manual valve indicator机长 captain副驾驶 first officer 缩写F/O观察员 observer乘务员 attendant解决故障排故 troubleshooting为了排故 for troubleshooting根据 refer to或 per 或 according to因为 due to或 because of更换 replaced拧紧 tighten拆下 removed 安装 installed 预置 preset调整 adj

26、ust 或 regulate重新调整 readjust重新设置 reset件号 part number 缩写P/N时控件 time control part上件 part on下件 part off维护手册 AMM放行标准 DDG（dispatch deviation guide）最低设备清单 MEL（minimum equipment list）同意放行 dispatch approved 或 released因停场时间不足 due to short time待件 wait for parts没有备件 lack of parts 或 no spare parts available 或 no

27、 parts in stock申请保留 apply for reservation保留故障 defer defect保留项目 defer item保留期限 due time关闭保留项目 close deferred item撤消保留项目 rescind deferred item按压 press把住 hold释放 release顺时针 clockwise逆时针 counterclockwise测试 test 通电测试 power-on test 安装测试 test for installation操作测试 operational test系统测试 test for system更新数据库 up

28、dated database在空中 in flight/ in the air在地面 on ground地面检查 GND check试车检查 running-up test（同机）对串件 interchangedwith（不同机间）对串件 exchangedwith / robbedfrom /swappedfrom正常 normal 或 OK异常 abnormal在范围内 within limits与一致/不一致 agree/ disagree with航材库 spare store现有的 existing=original=current采购部 PD=purchasing departme

29、nt工具间 tools room欧姆表 ohmmeter第三部分 各章节单词和故障描述ATA21空调空调 air-conditioning 缩写a/c（A/C是aircraft）空调舱 air-conditioning compartment空调舱灯 air conditioning compartment light空气循环机 air cycle machine 缩写ACM再循环风扇 recirculation fan出气活门 air outlet valve排气活门 exhaust valve外溢活门 outflow valve单向活门 check valve关断活门 shutoff va

30、lve释压活门 relief valve温度控制活门 TEMP CONT valve配平调节活门 trim modulating valve冲压空气作动器 ram air actuator排气活门位置指示器 outflow valve position indicator自动 automatic缩写AUTO人工 manual正常 normal 缩写NORM备用 alternate 缩写ALTN排气扇 exhaust fan 进气管 inlet duct供气扇 supply fan低流量 low flow主分配管 main distribution manifold头顶分配管 overhead

31、distribution ductAPU 进气口 air inlet for APU设备冷却 equipment cooling 增压 pressurization增压室 plenum压力控制 pressure control压力选择面板 press selector panel客舱压力控制组件 cabin press control module加热 heating过热电门 overheat switch压气机出口过热电门 compressor outlet overheat switch滤网 filter传感器 sensor水分离器 water separator主热交换器 primary heat exchanger次热交换器 secon