飞行记录本中英文对照Word下载.docx
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飞行记录本中英文对照Word下载.docx
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ATA28燃油33
ATA29液压35
ATA30防冰/防雨37
ATA31指示/记录系统38
ATA32起落架45
ATA33灯49
ATA34导航53
ATA35氧气59
ATA36气源系统61
ATA38水和废物62
ATA44客舱系统64
ATA49辅助动力装置66
ATA52门68
ATA55安定面71
ATA71动力装置71
ATA73发动机燃油和控制73
ATA74点火74
ATA75发动机空气74
ATA76发动机控制74
ATA77发动机指示78
ATA78排气79
ATA79发动机滑油79
ATA80起动80
……检查发现/报告故障……
1.航后:
检查发现左后航行灯不亮。
AF:
CheckedandfoundLAFTNAVlightwasnoton.
DoAFCheckandfindLaftpositionlightdoesnotwork.
DoAFCheckandfindLaftnavigationlightdoesnotwork.
DoTask:
TZ-AF-01,findLaftpositionlightdoesnotwork.
TZ-AF-01,findLaftnavigationlightdoesnotwork.
2.检查发现右前轮销磨损超标。
CheckedandfoundRnosewheelwaswornoutoflimits.
ChecknosewheelandfindRnosetirewearingisoutoflimits.
3.检查发现2号ATC故障。
CheckedandfoundNo.2ATCwasfailed.
CheckATCsystemandfindNo.2ATCfails.
4.检查发现左外刹车组件指示销磨损超标。
CheckandfindLoutboardbrakeASSYwaswornoutoflimits.
ChecktheMLGbrakeunitandfindLoutboardbrakeunitwearingisoutoflimits.
航后检查发现:
DoAFCheckandfindLoutboardbrakeunitwearingisoutoflimits.
TZ-AF-01,findLoutboardbrakeunitwearingisoutoflimits.
过站检查发现:
DoTRCheckandfindfindLoutboardbrakeunitwearingisoutoflimits.
TZ-TR-00,findLoutboardbrakeunitwearingisoutoflimits.
5.检查发现左主起落架一液压管漏油超标。
CheckedandfoundtheleakageofahydraulictubeofLMLGwasoutoflimits
ChecktheLMLGandfindtheleakageofahydraulictubeisoutoflimits.
6.检查发现13B座位小桌板不能收起,无法保持在收上位。
Checkedandfoundseat13Btraytablecouldnotbestowedandcouldnotbeheldatstowposition.
xx-xx-xx,find13Bfoodtablecannotbestowedandcannotbeheldinstowposition.(完成xx-xx-xx工卡发现…)
DoAFCheckandfind13Bfoodtablecannotbestowedandcannotbeheldinstowposition.(航后检查发现…)
DoTRCheckandfind13Bfoodtablecannotbestowedandcannotbeheldinstowposition.(过站检查发现…)
7.机组报告空中右发燃油滤旁通灯亮。
ThecrewreportedtheFuelFILTERBYPASSLightoftherightenginewasOnduringflight.
ThecrewreportedthattheFuelFILTERBYPASSLightoftherightenginecameOnduringflight.
8.航后APU自检有49-41012故障信息。
AF:
therewasa49-41012faultmessageafterAPUBITEProcedure.
APUBITEandfind49-41012faultmessage.
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AMM12-15-51/301检查轮胎气压正确。
TR:
ReplacedtheRnosewheelaccordingtoAMM32-45-21andcheckedthepressureofthetireaccordingtoAMM12-15-51/301,thepressurewascorrect.
TRCheck:
RefertoAMM32-45-21toreplacetheRnosewheel,andrefertoAMM12-15-51/301tocheckthetirepressure,thetirepressureisnormal.
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。
ReplacedtheNo.2ATCtransceiveraccordingtoAMMXX-XX-XX,anddidthesystemfunctionaltestaccordingtoAMMXX-XX-XX,theresultwasok.
RefertoAMMxx-xx-xxtoreplacetheNo.2ATCtransceiver,andRefertoAMMxx-xx-xxtodoasystemfunctionaltest,theresultisnormal.
3.航后根据AMM49-41-11更换APU起动机,启动测试APU工作正常。
AF:
ReplacedtheAPUstarteraccordingtoAMM49-41-11,anddidtheAPUStartandOpeationtest,theresultwasok.
RefertoAMM49-41-11toreplacetheAPUstarter,anddoaAPUstartandoperationtest,theresultisnormal.
4.过站根据AMM25-22-00折下第三排ABC座椅,座椅随机放在前货舱。
TR:
removedthepassengerseatsA/B/Cofthe3rdlineaccordingtoAMM25-22-00.TheseatswerestoredintheFWDcargo.
RefertoAMM25-22-00toremovethepassengerseats3A/3B/3C,andstoreintheFWDcargo.
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。
RefertojobcardXXXX,replacedthebattery,anddidtheinstallationtest,thevoltagewasXXvolt,meetthemanual’sdemand.
Refertojobcardxxxxtoreplacethebattery,andrefertoAMMxx-xx-xxtodoatest,thevoltageofthebatteryisXXvolt,ConformtoAMM’sdemand.
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。
TRfoundtheFWDattendantmicrophonewasfailed,releasedtheaircraftaccordingtoMEL23-20.
DoTRCheckandfindtheFWDserviceinterphonefails,refertoMEL23-20todispatchtheaircraft.
TZ-TR-00,findtheFWDserviceinterphonefails,refertoMEL23-20todispatchtheaircraft.
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,并办理保留DD3000000。
checkedandfoundtheprsovoftherightenginewasfailed.Becauseoflackingofspare,releasedtheaircraftaccordingtoMEL36-5,anddidthejobofitem“M”—lockedthePRSOVatclosedposition.Installedthe“RIGHTENGINEBLEEDAIRSYSTEMINOP”tagatrightenginebleedairswith.ThedeferreddefectformNO.isDDXXXXXXX
DoAFCheckandfindthePRSOVvalveoftheRenginefails.Duetolackingofspareparts,RefertoMEL36-5todispatchtheaircraft,andfinishthejobofitem(M)-lockthePRSOVvalveinclosedposition,pastethe“RENGINEBLEEDAIRSYSTEMINOP”tagnexttotheRenginebleedairswitch,re.DD3000000
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。
RefertoAMM23-20,replacedtheFWDattendantmicrophone,didthefunctionaltest,theresultwasOK,withdrewDD/FCXXXXX.
RefertoAMM23-20-00toreplacetheFWDserviceinterphone,anddoafunctiontest,theresultisnormal,closetheDD/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DDXXXXX
replacedtherightenginePRSOVaccordingtoAMM36-11-04,anddidthefunctionaltestaccordingtoAMM36-11-04,theresultwasok,withdrewDDXXXXX.
RefertoAMM36-11-04toreplacethePRSOVvalveoftheRengine,andrefertoAMM36-11-04todoafunctiontest,theresultisnormal,closetheDDXXXXX.
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。
CheckedandfoundtherewasBird/HailStrikeConditionontheradiomeandtheRengineairinlet.AccomplishedtheBird/HailStrikeConditionalInspectionaccordingtoAMM05-51-18,anddidthefunctionaltestoftheLeadingEdgeFlapandSlatOperationalTestinPrimaryModeandTrailingEdgeFlapSystemOperationalTestaccordingtoAMM27-81-00andAMM27-51-00,theresultwasok.
DoTRCheck/DoTask:
TZ-TR-00,findaBird/HailStrikeconditionontheradomeandtheRengineinletcowl,refertoAMM05-51-18tofinishtheinspectionofBird/HailStrike,andrefertoAMM27-81-00/27-51-00todoaoperationtestofleadingedgedeviceandtrailingedgedevice,theresultisnormal.
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-XX-XX将P2-2面板与B-2650对串,并完成系统功能测试,结果正常。
AsapurposeoftroubleshootingfortheautobrakefaultofB-2652,swappedtheP2-2panelwithB-2650accordingtoAMMXX-XX-XX,andcarriedoutthesystemfunctionaltest,theresrulwasok.
FortroubleshootingofautobrakesystemofB-2652,refertoAMMxx-xx-xxtointerchangetheP2-2withB-2650,anddoafunctiontest,theresultisnormal.
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XXPSI;
N1=XX引气压力为XXPSI;
右发:
引气压力正常。
Duetolackingofparts,asapurposeoftroubleshooting,interchangedbleedairregulatorofRenginewithLengineaccordingtoAMMXX-XX-XX,anddidtheengineoperationtest,thedatawas:
Lengine:
N1=XX,bleedairpressure=XXPSI;
N1=XXbleedairpressure=XXPSI;
Rengine:
N1=XXbleedairpressure=XXPSI;
theresultwasok.
Duetolackingofspareparts,fortroubleshootingofRenginebleedairsystem,refertoAMMxx-xx-xxtointerchangebleedairregulatorwithLengine,dotheenginerunningtest,thetestdataisasfollows:
LEngine:
N1=xx%,Bleedairpressure=xxPSI;
REngine:
thebleedairpressureisnormal.
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XXPSI,结果正常。
ReplacedtheRenginebleedairregulatoraccordingtoAMMXX-XX-XX,anddidtheengineoperationtest,thedatawas:
N1=XX,bleedairpressure=XXPSI;
theresultwasok.
RefertoAMMxx-xx-xxtointerchangetheRenginebleedairregulator,thetestdataisasfollows:
飞机概况
排row(如:
第5排译作row5)
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wingtip
前缘leadingedge
后缘trailingedge
客舱cabin或passengercompartment
货舱cargo
轮舱wheelwell缩写W/W
驾驶舱cockpit/flightcompartment
设备舱bay
窗window
滑窗sliding
门窗doormountedwindow
旅客窗passengercompartmentwindow
座位seat
过道aisle
地板floor
天花板ceiling
行李架stowagebin
杆lever或stick或column
操纵面controlsurface
操纵杆controlcolumn
控制面板controlpanel
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
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upperleft
右下lowerright
左前leftforward
右后rightafterward
内侧inboard缩写I/B
外侧outboard缩写O/B
左内侧leftinboard
在…之间between…and…
航材
胶adhesive
销子pin例如安全销safetypin
插头plug
插座socket
插针pin
电阻resistor
线路wire
引线lead
螺帽nut
螺栓bolt
螺钉screw
跳开关circuitbreaker
继电器relay
隔离垫spacer
遮光板glareshield
消耗航材consumablematerial
故障描述
航前检查preflight(PF)check
航后检查afterflight(AF)check
过站检查transit(TR)check
定检scheduledmaintenance
发现find或reveal
故障trouble或failure或fault
失效fail或malfunction
不能failto…或can’t
不灭didnotturn/gooff
不亮didnotturn/come
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