机务航线常用单词

1、nose wheel左外 left outboard 或 left outside 左内 left inboard 或 left inside右外 right outboard 或 right outside 右内 right inboard 或 right inside刹车 brake 刹车蓄压器brake accumulator主起落架main landing gear上锁作动器uplock actuator 下锁作动器downlock actuator前起落架nose landing gear 转弯 steering防滞 anti-skid 起落架锁定gear locked起落架舱门wh

2、eel door 轮舱 wheel well放轮 gear extension 收轮 gear retraction收放测试test for R/E（ retract/ extend 的缩写形式）起落架被卡阻gearjammed轮胎 tyre 爆胎 burst 瘪胎 deflated tyre 轮胎被扎破puncture轮胎 tyre 见线 exposed threads 磨损 wear 或 worn out 裂纹 cracks超限 out of limits 在范围内within limits 空 /地继电器air/ground relay 自动刹车 autobrake刹车保险brake f

3、use 人工释放manual extension 液压刹车压力指示器hydraulic brake pressure indicator 停留刹车parking brake 故障灯 fault light 解除预位灯 disarm light 不工作灯INOP light限流器 flow limiter 扭力杆 torsion link 人工放出机构manual extensionmechanism放下并锁上传感器down and locked sensor 收上并锁上传感器up and locked sensor下锁弹簧downlock spring 减振支柱shock strut 侧支柱

4、side strut 阻力支柱drag strut人工放出限制电门manual extension limit switch 刹车踏板电门brake pedalswitch前轮转弯电门nose wheel steering switch 防滞传感器antiskid transducer刹车调节活门brake metering valve 加注活门charging valve 选择活门selector valve转换活门transfer valve 隔离活门isolation valve 防滞活门antiskid valve往复活门shuttle valveATA33 灯灯 light 闪光灯

5、strobe light 航行灯 navigation light 缩写 NAV light防撞灯anti-collision light 着陆灯 landing light 信号灯 signal light下滑灯 approach light 机翼照明灯wing illumination light 标志灯 logo light滑行灯taxi light 应急照明灯emergency light 机身灯 fuselage light转弯灯 turnoff light 尾灯 tail light 窗灯 window light荧光灯 fluorescent lamp 地板灯 floor lig

6、ht 阅读灯 reading lamp灯座 lamp socket 或 lamp base 灯架 lampholder 地图灯 cap light 灯组件 light module明 bright 暗 dim 灯泡 bulb 烧坏 burn out 灯罩 lamp cover灯亮 on 或 illuminate 灯灭 off 或 turn offATA34导航导航 navigation 缩写 NAV 天线 antenna 数据库 database 顶端 top底端 bottom 下滑道 glide slope 指点信标marker beacon无线电高度接收机radio altitude re

7、ceiver 无线电高度发射天线radio altitudetransmitter antenna气象雷达weather radar 近地警告ground proximity warning 缩写 GND PROXWARN无线电导航radio navigation 姿态指示仪attitude indicator测距仪询问机DME interrogator 应答机 transponder 收发机 transceiver惯导 inertial reference 主注意 master caution氧气 oxygen 氧气面罩oxygen mask 流量控制flow control 充气控制inf

8、lation control氧气压力指示oxygen pressure indicator 旅客氧气面罩passenger oxygenmask机组氧气面罩crew oxygen mask 氧气系统组件oxygen system module氧气系统面板oxygen system panel 安全销 safety pin 压力调节器pressureregulator氧气指示继电器oxygen indicator relay 高度压力电门altitude press switch机组氧气传感器crew oxygen transducer 乘务员服务组件attendant serviceunit厕

9、所服务组件lavatory unit旅客服务组件passenger service unit超压释放活 门 overpressure relief valve ATA36OM系统气源 pneumatics 引气活门bleed air valve 双压力指示dual pressure indicator引气调节器bleed air regulator 预冷控制活门传感器precooler control valvesensor超温电门over temperature switch 恒温器 thermostat 总管压力传感器manifold press transmitter APU 引气活门A

10、PU bleed air valve 单向活门check valve引气隔离活门bleed air isolation valve预冷控制活门precooler control valve 地面气源ground pneumaticATA38水和废物水和废物water & waste 真空通风机vacuum blower 排放管 drain line水量指示water quantity indicator 空气过滤air filter 水服务面板waterservice panel真空马桶vacuum toilet 加注/溢流活门fill/overflow valve 球形活门ballv

11、alveATA49辅助动力装置辅助动力装置auxiliary power unit 缩写 APU 进气门作动器air inlet actuator导向叶片guide vane 燃油增压泵fuel boost pump 排气温度exhaust gastemperature 缩写 EGT 数据记忆组件data memory module 滑油位传感器oillevel sensor 滑油温度传感器oil temperature sensor 速度传感器speed sensor 进气门位置电门air inlet door position switch 热电耦 thermocouple燃油控制组件fu

12、el control unit 点火组件ignition unit 喘振活门surge valveATA52 门门 door 登机门 entry door 警告电门warning switch 平衡组件counterbalance assembly紧急出口emergency exit 货舱门闩cargo door latch 接近面板access panel门上锁面板door unlock panel 安定面配平stabilizer trimATA56 窗ATA71 动力装置风扇罩 fan cowl 铰链 hinge 风扇罩面板闩fan cowl panel latch 发动机架engine

13、mount附件齿轮箱 accessory gearbox传动齿轮箱 transfer gearbox 转子，叶轮 spinner发动机慢车位idle发动机喘振surge发动机停车engine shutdown发动机熄火 engine flame outATA73发动机燃油和控制发动机燃油和控制engine fuel & control 燃油系统fuel system 燃油箱 fueltank 通气孔 vent加油栓 fuel hydrant 燃油管路fuel line 放油活门dump valve 燃油泵 fuelpump燃油滤 fuel filter 接头 joint 燃油流量表fu

14、el flow indicator 导线束 wiringharness燃油总管fuel manifold 燃油喷嘴fuel nozzle 发动机控制面板engine controlpanel 插头 plug备用电源继电器alternate power relay 风扇进气温度传感器fan inlettemperature sensor压差电门differential pressure switch 电子发动机控制electronic enginecontrol 缩写 EEC燃油流量传感器fuel flow transmitterATA74点火点火 ignition 点火激励器ignition

15、exciter 发动机起动电门engine start switch发动机点火电门engine ignition switchATA75发动机空气发动机空气engine air 可变引气活门variable bleed valve 缩写 VBV高压涡轮间隙活门HP turbine clearance valve 缩写HPTCV低压涡轮间隙活门LP turbine clearance valve 缩写 LPTCV位置传感器position transducer 过渡引气活门transient bleed valveATA76发动机控制发动机控制engine control 起动杆 start l

16、ever 点火电门ignition switchATA77发动机指示发动机指示engine indicatingATA78排气排气 exhaust 反推 thrust reverser 套筒 sleeve 同步锁 SYNC lock顺序电门sequence relay 控制电门control switch 发动机附件组件engineaccessory unitATA79发动机滑油发动机滑油engine oil 润滑剂 lubricant 润滑 lubrication 滑油管路oil line探测器 detector 回油 scavenge 回油过滤scavenge filter 主滑油 /燃油

17、热交换器 main oil/fuel heat exchanger 滑油压力传感器oil pressure sensor 滑油压力表 oil pressure indicator 滑油温度表oil temperature indicatorATA80起动起动 stating 发动机起动活门engine start valve常用语句检查发现1 . 航后检查发现左后航行灯不亮。Postflight check found L AFT NAV light not on.2 .短停检查发现右前轮见线。Transit check found R nose wheel exposed threads.3

18、 .航前检查发现2号ATC故障。Preflight check found No.2 ATC fault.4 .航后检查发现左外刹车组件指示销磨损超标。Postflight check found L outboard brake ASSY indicating pin worn out of limits.5 .航后检查发现左起落架一液压管漏油超标。Postflight check found a hydraulic line of L LDG leakage out of limits.更换（件）;检查/测试正常1 . 短停更换前轮，检查正常。In transit replaced R n

19、ose whee，l check OK.2 .更换2号ATC收发机后，测试正常.After replaced No.2 ATC transceive，r test OK.3 .航后更换左主轮，检查正常。Replaced L main wheel in postflight， check OK.4 .更换左外刹车组件，增压检查正常。Replaced L outboard brake ASS，Y pressurization check OK.5 .更换xx点火导线，测试正常。Replaced L engine right ignition lead， test OK.6 .更换前起落架减振支柱充

20、气活门，地面检查无渗漏。Replaced nose gear shock strut charging valv， e no leakage in GND check.7 .更换左发17号风扇叶片，地面检查正常。下：M/W31162， xxM/W30966Replaced L engine No.17 fan blad，e 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 starte，r APU start OK.参考/按更换（件），测试1 . 根据工卡01，更换电子/电气冷却

21、供气风扇气滤，通电测试正常。Per job card 01， replaced E/E cooling fan air filter， test ok.2 .参考AMM33-43-11,更换左后航行灯灯泡，通电测试正常。Refer AMM33-43-11， replaced L AFT NAV light bul，b power-on test OK.3 .按工卡NR/1,更新FMC导航数据库。Per to job card N/R1， updated FMC NAV database.4 .参考AMM32-31-00,更换液压管，测试无渗漏。检查发现故障， 按保留，号/类别，同意放行1 .短

22、停发现前服务话筒失效，按 MEL23-20保留，保留号GY05-0040.Transit found FWD attendant microphone malfunction， ref MEL23-30 defer，No. GY05-0040.2 .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.按.更换件，测试正常，撤消/关闭保留1 .按AM

23、M23-20,更换前服务话筒，测试正常，撤消 GY05-0040保留。Refer AMM23-20， replaced fwd attendant microphone， test OK， rescind defer item GY05-0040.2 .更新FMC导航数据库，通电测试工作正常，右HIS地图方式正常，并关闭MEL保留。Update FMC NAV database， power-on test OK， R HIS map OK， closed defer item.3 .清洁并重装左GPS天线，地面测t正常，撤消 000573页上的GY050113 保留。Clean and re

24、install L GPS antenn，a GND test OK， rescind defer GY050113 on page000573.遭遇鸟击1 .xx 罩和右发进气道口有鸟击痕迹。Check found birdstrike on radome 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 radome & R engine norma， l engine fan blades & bypass normal.（件）不工作/故障/故障灯亮1 .xx 点火器不工作。L

25、engine igniter INOP.2 .右HIS地图显示故障。R HIS map display fault.3 .巡航过程发现左右管道压力相差过大。When cruised， found L & R duct pressure much different.4 .设备冷却系统供气正常位不工作。Equipment cooling system supply air INOP on NORM.5 .第二部应答机“ATC FAIL亮。No.2 transponder “ ATCFAIL” light on.6 .空中气象xx失效。In flight weather radar fai

26、led.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。Autopi lot channel B can t engage.9 .空调流量小，制冷效果差。11 / 13Air-conditioning flow small ， cooling poor.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。Postflight found nose gear mirror too low， check found due charging valve csn lock， leak air

27、.Transit check found R outboard gear exposed threads due wearing.4.航后检查发现左主轮磨损见线。Postflight check found L main gear exposed threads due wearing.为判断故障/因为航材缺件，对串件，测试1. 与 B-5041 飞机对串磁带放像机，通电测试正常。Exchange tape reproducer with A/C B-5041， power-on test normal.2 .为判断B-5067自动刹车故障，将P2-2面板与B-5041对串，通电测试正 常。For troubleshooting autobrake fault of A/C B-5067， robbed P2-2 from A/CB5041， 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 lack parts， for troubleshooti