Chapter 31Indicating.docx
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Chapter 31Indicating.docx
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Chapter31Indicating
Chapter31Indicating\RecordingSystems
31Indicating\RecordingSystems
INCASEOFFAILUREOFTWODMCs:
TheECAMSYSTEM/STATUSdisplayisnolongeravailable.
TheECAMSYSTEM/STATUSdisplayisstillautomaticallypresented.
TheECAMSYSTEM/STATUSdisplaycanbepresentedonlybymanualselection.
c
31Indicating\RecordingSystems
IFTHECAPTAINPRIMARYFLIGHTDISPLAY(PFD)FAILS:
ThePFDimageisautomaticallydisplayedonthefirstofficerPFDunit.
ThePFDimageisautomaticallydisplayedontheCAPTAINNavigationDisplayunit.
ThePFDimageislost.
b
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THEECAMSTATUS(STS)PAGE:
Isonlydisplayedautomatically.
Isautomaticallydisplayedinthecruiseflightphase.
Canbedisplayedmanuallyorautomatically.
c
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THEECAMSYSTEMDISPLAYSHOWS:
Systemandstatuspagesonly.
Statuspagesandpermanentdataonly.
Systemandstatuspagesandpermanentdata.
c
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ONTHEENGINE/WARNINGDISPLAY(EWD),AWARNINGMESSAGEAPPEARSON:
Ontheupperarea.
Leftmemoarea.
Rightmemoarea.
b
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THEELECTRONICINSTRUMENTSYSTEM(EIS)DISPLAYMANAGEMENTCOMPUTER(DMC)TRANSFERSWITCHISLOCATED:
OntheextremeLHsideandRHsideoftheCAPTandF/Oinstrumentpanels.
OntheCenterPedestal.
BetweentheEngineWarningDisplay(EWD)andtheNavigationDisplay(ND).
b
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WHENAWARNINGORCAUTIONOCCURS,AMESSAGEAPPEARSONTHE:
SystemDisplay(SD).
Engine/WarningDisplay(EWD).
Statusdisplay.
B
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THEONLYFUNCTIONAVAILABLEFORATYPE3SYSTEMMENUIS:
TheLASTLEGREPORT.
TheTEST(RESET).
CLASS3.
b
3类系统菜单唯一可用的功能是
最后航段报告
测试(复位)
3级
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WHENAWARNINGISCLEARED,THERECALL(RCL)PUSHBUTTONONTHEECAMCONTROLPANEL(ECP)ISUSEDFOR:
Warningsinhibition.
ThedisplayoftheSTATUSpage.
Thepresentationofwarning/cautionmessagesstart.
C
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THEFAILURESHAVINGANOPERATIONALCONSEQUENCEONTHECURRENTFLIGHTARE:
Class1failures.
Class2failures.
Class3failures.
a
什么故障对当前飞行有操作性的影响?
1级故障
2级故障
3级故障
31Indicating/RecordingSystems
THESTATUSPAGEDISPLAYS:
Memomessages.
Operationalstatusmessages.
Warningsmessages.
B
状态页面显示:
备忘信息
运行状态信息
警告信息
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ATYPE3SYSTEMISLINKEDTOTHECFDIUBY:
AnARINC429inputbusandanARINC429outputbus.
AdiscreteinputandanARINC429outputbus.
Adiscreteinputandadiscreteoutput.
c
3类系统通过什么连接到集中故障显示接口组件?
一条ARINC429输入总线和一条ARINC429输出总线
一条离散输入和一条ARINC429输出总线
一条离散输入和一条离散输出
31Indicating/RecordingSystems
THEUPANDDOWNDATALOADINGSYSTEMISDEFINEDAS:
AninterfacebetweentheaircraftcomputersandtheMultipurposeDiskDriveUnit(MDDU).
Aninterfacebetweentheaircraftsystemscomputersonly.
Aninterfacebetweentheonboardcomputersandtheground-basedataprocessingstations.
C
数据上传及下载系统的定义是:
飞机计算机与多功能磁盘驱动组件的界面
仅限于飞机系统计算机之间的界面
机载计算机与地面数据处理站的界面
31Indicating\RecordingSystems
THECFDSFUNCTIONSAVAILABLEINFLIGHTARE:
LASTLEGREPORTandLASTLEGECAMREPORT.
CURRENTLEGREPORTandCURRENTLEGECAMREPORT.
CURRENTLEGREPORTandPREVIOUSLEGSREPORT.
b
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THEPRINTERALLOWSPRINT-OUTOFTHECENTRALIZEDFAULTDISPLAYSYSTEM(CFDS)ANDADDITIONALREPORTSCOMINGFROM:
TheAircraftIntegratedDataSystem(AIDS)andtheEngineVibrationMonitoringUnit(EVMU).
TheAirTrafficServiceUnit(ATSU)andtheFlightManagementandGuidanceSystem(FMGS).
TheAIDS,theEVMU,theATSUandtheFMGS.
C
打印机接受来自于——的集中故障显示系统及附加报告?
飞机综合数据系统和和发动机振动监控组件
空中交通服务组件和飞行管理和引导系统
飞机综合数据系统和,发动机振动监控组件,空中交通服务组件和飞行管理和引导系统
31Indicating\RecordingSystems
ATYPE1SYSTEMISLINKEDTOTHECFDIUBY:
AnARINC429inputbusandanARINC429outputbus.
Adiscreteinputandadiscreteoutput.
AdiscreteinputandanARINC429outputbus.
a
一个1类系统通过什么连接到集中故障显示接口组件?
一条ARINC429输入总线和一条ARINC429输出总线
一条离散输入和一条离散输出
一条离散输入和一条ARINC429输出总线
31Indicating\RecordingSystems
THEPURPOSEOFTHE"GROUNDSCANNING"FUNCTIONISTO:
Establishtheavionicsstatuswhilethesystemisonground.
ListthefaultysystemsoftheA/Cwhileonground.
ForcetheoperationoftheBITEinsystemnormalmode.
c
"GROUNDSCANNING"的用途是
当此系统在地面时建立电子状态
在地面时列出飞机有故障的系统
使自测设备的运作处于系统的正常模式
31Indicating\RecordingSystems
THE"T.OINHIBIT",DISPLAYEDONTHEE/WDISPLAY,MEANSTHAT:
TheT.Oconfigurationtesthasfailed.
Mostwarningsareinhibitedduringthisflightphase.
TheT.Oconfigurationtesthastobeinitiated.
b
显示在发动机/警告显示上的"T.OINHIBIT"意味着
起飞构型测试失效
大部分的警告在这个飞行阶段被抑制
必须启动起飞构型测试
31Indicating\RecordingSystems
IFBOTHECAMDISPLAYUNITSFAIL:
TheE/WDisplaysarenolongeravailable.
TheE/WDisplaycanstillbepresentedontheNDDisplaywhenswitched,usingthe"ECAM/NDTRANSFER"switch.
OnlytheSYSTEMDisplaycanbepresentedontheNDDisplay,whenthe"ECAM/NDTRANSFER"switchisused.
b
31Indicating\RecordingSystems
EACHDMCPROCESSESSIMULTANEOUSLY:
2displays.
3displays.
4displays.
b
每个显示管理计算机同时处理
2个显示
3个显示
4个显示
31Indicating\RecordingSystems
THEINFORMATIONFORTHESYSTEMSYNOPTICSISACQUIREDBY:
TheSDACandFWCordirectlybytheDMC.
TheFWConly.
TheDMConly.
a
系统概述的信息通过什么获得?
SDAC和FWC或直接通过DMC.
只有FWC
只有DMC
31Indicating/RecordingSystems
ONEACHEIS2,EACHDMCPROCESSESSIMULTANEOUSLY:
2displays.
3displays.
4displays.
b
在每个电子仪表系统2上,每个显示管理计算机同时处理
2个显示器
3个显示器
4个显示器
31Indicating\RecordingSystems
THEECAMWARNINGMESSAGESAPPEARON:
TheSystemDisplay(SD).
Thestatuspage.
TheEngineWarningDisplay(EWD).
c
31Indicating\RecordingSystems
THEALTITUDEAPPEARSON:
ThePrimaryFlightDisplay(PFD).
TheSystemDisplay(SD).
TheNavigationDisplay(ND).
a
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THEDISPLAYMANAGEMENTCOMPUTER(DMC)1DRIVESTHECAPTAIN:
PrimaryFlightDisplay(PFD),theNavigationDisplay(ND)andtheEngine/WarningDisplay(E/WD).
PFD,theND.
PFD,thecaptainND,theE/WDandtheSystemDisplay(SD).
C
显示管理计算机1驱动机长——:
主飞行显示器,导航显示,和发动机/警告显示
主飞行显示器,导航显示
主飞行显示器,机长导航显示,发动机/警告显示及系统显示
31Indicating/RecordingSystems
THEBRIGHTNESSOFTHEECAMDISPLAYSCANBEMANUALLYADJUSTEDFROM:
TheEFIScontrolpanel.
TheECAMsystemcontrolpanel.
TheDisplayManagementComputers.
b
31Indicating/RecordingSystems
THEEISCOMPRISESSEVERALSYSTEMCOMPUTERS,THESECOMPUTERSARE:
DMC1,2,3;FWC1,2;SDAC1,2.
DMC1,2,3;FWC1,2;SDAC1,2ANDTHECFDIU.
DMC1,2,3;FWC1,2;SDAC1,2,3.
A
31Indicating/RecordingSystems
FORMAINTENANCEPURPOSES,THECFDIURECEIVESFAULTDATAFROM:
TheaircraftsystemcomputerBITEonly.
TheaircraftsystemcomputerBITEandtheFlightDataInterfaceUnit(FDIU)orFDIMU.
TheaircraftsystemcomputerBITEandtheECAM.
C
为了维修,集中故障显示接口组件(CFDIU)的故障数据从——获得?
飞机系统计算机自测设备(BITE)
飞机系统计算机自测设备(BITE),飞行数据接口组件(FDIU)或飞行数据接口及管理组件(FDIMU)
飞机系统计算机自测设备(BITE)和飞机电子中央监控(ECAM)
31Indicating\RecordingSystems
THECFDIULASTLEGREPORTISTRANSFERREDTOTHEPREVIOUSLEGREPORTMEMORYPARTOFTHECFDIUAT:
Aircrafttouchdown.
Secondengineshutdown.
Thebeginningofanewflight/firstenginestarted+3minutesandflightNo.entered.
c
CFDIU最后航段报告被传送给CFDIU以前航段报告的记忆部分
飞机一触地
2发一关闭
新飞行的开端/启动1发的开端+3分钟且飞行号录入
31Indicating\RecordingSystems
THEMULTIPURPOSECONTROLANDDISPLAYUNIT(MCDU)ALLOWSSOFTWARECROSSLOADINGTO:
TheDisplayManagementComputers(DMC)only.
TheDMCandtheDisplayUnits(DU).
TheECAMcontrolpanel.
b
多功能控制和显示组件允许软件交叉上传到
仅显示管理计算机
显示管理计算机和显示组件
ECAM控制面板
31Indicating/RecordingSystems
WHENALOSSOFMAINELECTRICALPOWERSUPPLYOCCURS:
AlltheclockdisplaysareblankedbutthetimeisstillcountedinmemorythankstotheAuxiliaryPowerUnit(APU)powersupply.
Alltheclockdisplaysareblankedbutthetimeisstillcountedinmemorythankstotheaircraftbatterypowersupply.
Alltheclockdisplaysareblankedandthetimeisnolongercountedinmemory.
B
当主电气电源丢失___会发生?
所有的时钟显示是空白的,但由于APU电源的作用时间的记数仍在存储器中继续着。
所有的时钟显示是空白的,但由于飞机电瓶电源的作用时间的记数仍在存储器中继续着。
所有的时钟显示是空白的,时间的记数也不在存储器中继续。
31Indicating\RecordingSystems
INTHECASEOFAIRCRAFTCLOCKFAILURE,GMTDATAIS:
ProvidedbyaseparatetimebaseintegratedintheFWC.
Definitelylost.
ProvidedbytheCFDIUinternalclock.
c
如果飞机时钟失效,格林尼治时间数据
由综合在FWC内的一个独立的时间库提供
一定丢失
由CFDIU内部的钟提供
31Indicating/RecordingSystems
WHENTHEANNUNCIATORLIGHTSWITCHISSETTOTEST
Allclockdisplaysturnintoblank.
Allclockdisplaysshowzeros.
Allclockdisplaysshoweights.
C
信号灯开关按下来是用来测试___
所有的时钟显示变成空白
所有的时钟显示器显示为零
所有的时钟显示器显示为八
31Indicating/RecordingSystems
FORANUPLOADINGPROCEDURE,THEMULTIPURPOSEDISKDRIVEUNIT(MDDU)READYMESSAGEISDISPLAYEDONTHEMDDUWINDOW:
Ifthereisnodiskinsertedinthedataloader.
Ifthereisadiskinsertedinthedataloader.
Assoonasadialogueisestablishedbetweenthecomputertobeloadedandthedataloader.
A
对于一个上传程序,___多功能磁盘驱动组件(MDDU)在MDDU的窗口上将显示READY信息
如果没有磁盘插入数据装载器
如果有磁盘插入数据装载器
一旦要被下载的计算机和数据盛载器的对话被建立
31Indicating/RecordingSystems
THEDATALOADINGSELECTOR(DLS)ANDTHEMULTIPURPOSEDISKDRIVEUNIT(MDDU)AREUSEDTOENSURE:
Theuploadingfunctiononly.
Thedownloadingfunctiononly.
Theupanddownloadingfunctions.
C
数据装载选择器(DLS)和多功能磁盘驱动组件(MDDU)用来确保:
上传功能
下载功能
上传功能和下载功能
31Indicating/RecordingSystems
DURINGPRINTERSERVICING,BEFOREOPEN,SAFETYANDTAGTHE6TWPRINTER/SUPPLY(PTR/SPLY)C/B,THESTEPCONSISTSIN:
Turningthelockingsystemtoopentheprinterd
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