Chapter 34 NavigationWord格式.docx

Chapter 34 NavigationWord格式.docx

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THECORRECTLOCATIONOFTHESENSORSFORTHEIRSECTIONOFTHEADIRUIS:

AllthesensorsareinsidetheADIRU.

TheaccelerometersareoutsidetheADIRU.

AllthesensorsareoutsidetheADIRU.

AIRDATAMODULES（ADM）SUPPLYPRESSUREINFORMATIONTOTHEADIRUSFROM:

AllPitotprobesandStaticports.

ThePitotprobesonly.

TheStaticportsonly.

INNORMALOPERATIONADIRU1SUPPLIESINFORMATIONTO:

sPFDandtheFirstOfficer'

sND.

sNDandtheFirstOfficer'

sPFD.

sPFDandND.

C

ILS1DATA,LOCANDGLIDESLOPEDEVIATIONS,FREQUENCYANDIDENTIFICATIONOFILSSTATIONARENORMALLYDISPLAYED:

OntheCaptain'

sPFDandF/O'

sPFDandCaptain'

OntheF/O'

THEBAROCORRECTIONORREFERENCESELECTEDISSENTTOEACHADIRUFROM:

ThemasterFlightManagementandGuidanceComputer.

TheFlightControlUnit.

TheRadioManagementPanels.

THEAIRDATAMODULES（ADM）INPUTSCONSISTIN:

Onepressureinputandonediscreteinput.

Onepressureinputandseveraldiscreteinputs.

Onepressureinputandonedigitalinput.

THEWEATHERRADAR（WXR）IMAGEANDTHERADARINFORMATIONSTATUSAREDISPLAYEDON:

TheNDsinalldifferentEFISmodes.

TheNDsinalldifferentEFISmodesexceptinPLANmode.

TheNDsinalldifferentEFISmodesexceptinROSEmode.

AIRDATAMODULES（ADM）SUPPLYPRESSUREINFORMATIONTOTHEADIRUsFROM:

WINDSHEARINDICATIONSANDWARNING/CAUTIONALERTSAREDISPLAYEDON:

TheNDsonly.

ThePFDsandtheNDs.

TheupperECAMdisplayunit.

EACHADIRURECEIVESTWOANALOGINPUTS:

AngleofAttack（AOA）andTotalAirTemperature（TAT）.

AngleofAttack（AOA）andbarocorrection.

FlightManagementandGuidanceComputerstatusandbarocorrection.

THERASYSTEMISUSEDTODETERMINETHEAIRCRAFT:

Altitudeinallcases.

Height,lessthanorequalto2.500ftabovetheground.

Height,aboveaflatgroundsurface.

THEINTEGRATEDSTANDBYINSTRUMENTSYSTEM（ISIS）REPLACESTHESTANDBY:

Altimeter,thestandbyhorizonandthestandbyairspeed.

Horizononly.

Compass.

THERASYSTEMISCONNECTED:

DirectlytothePFDsfordisplay.

DirectlytotheNDsfordisplay.

TotheDisplayManagementComputers（DMCs）fordisplay.

WHENTHEWEATHERRADARISON:

Personnelshouldnotbewithin2moftheradome.

Personnelshouldnotbewithin1.5moftheradome.

Personnelshouldnotbewithin1moftheradome.

THEAIRCRAFTHEIGHTPROVIDEDBYTHERASYSTEMISALWAYSSHOWN:

DigitallyonthePFDsformorethan2.500ftheights.

OnthePFDsbyaredribbonnexttothealtitudescale.

OnthePFDsbyalinerisingonthepitchdownareawhentheaircraftisbelow300ft.

ILS1（INSTRUMENTLANDINGSYSTEM1）DATAISDISPLAYEDON:

PrimaryFlightDisplay1（PFD1）andNavigationDisplay2（ND2）.

PFD1andND1.

PFD2andND2.

THETRAFFICALERTANDCOLLISIONAVOIDANCESYSTEM（TCAS）DETECTS:

Allaircraftsinitsdetectionrange.

OnlyAirTrafficControl（ATC）modeSequippedaircrafts.

ATCequippedaircrafts.

HEIGHTPROVIDEDBYRADIOALTIMETER1（RA1）ISDISPLAYEDON:

Thecaptain'

sPrimaryFlightDisplay.

TheNavigationDisplay.

THETRAFFICALERTANDCOLLISIONAVOIDANCESYSTEM（TCAS）COMPONENTSISMADEOF:

Twoantennas,oneTCASIIcomputerandoneTCAS/AirTrafficControl（ATC）controlpanel.

Twoantennas,twoTCASIIcomputersandoneTCAS/ATCcontrolpanel.

Fourantennas,twoTCASIIcomputersandtwoTCAS/ATCcontrolpanels.

IFFLIGHTMANAGEMENTANDGUIDANCECOMPUTER1（FMGC1）FAILSTOTUNEDISTANCEMEASURINGEQUIPMENT1（DME1）:

FMGC2tunesDME1（automaticswitch-over）.

NotuningofDME1possible.

FMGC2mustbemanuallyswitchedontotuneDME1.

THEENHANCEDGROUNDPROXIMITYWARNINGSYSTEM（EGPWS）COMPLETESTHEGROUNDPROXIMITYWARNINGSYSTEM（GPWS）BASICMODESWITH:

TerrainClearanceFloor（TCF）function.

TerrainAwarenessalertingandDisplay（TAD）function.

TCFandTADfunctions.

BOTHILSRECEIVERFREQUENCIESCANBECONTROLLEDBY:

RadiomanagementPanel（RMP）1,RMP2oreitheroftheFMGCs.

RMP1onlyorRMP2only.

FMGC1only.

THEENHANCEDGROUNDPROXIMITYWARNINGSYSTEM（EGPWS）COMPONENTSARE:

AnEnhancedGroundProximityWarningComputer（EGPWC）,acontrolpanelandoneTERRainONNDmodeP/BSW.

AnEGPWC,acontrolpanel,twowarninglightsandoneTERRONNDmodeP/BSW.

AnEGPWC,acontrolpanel,twowarninglights,andtwoTERRONNDmodeP/BSWs.

THEENHANCEDGROUNDPROXIMITYWARNINGSYSTEM（EGPWS）WARNINGSAREPROVIDEDBYTHE:

ND,PFD,GPWS-G/Spushbuttonandthecockpitloudspeaker.

ND,GPWS-G/Spushbuttonandthecockpitloudspeaker.

GPWS-G/Spushbuttonandthecockpitloudspeaker.

THEENHANCEDGROUNDPROXIMITYWARNINGSYSTEM（EGPWS）ALERTSARE:

Visual,syntheticwarningsandtheterrainhazardsdisplayonNDs.

Visualandsyntheticwarnings.

Syntheticwarningsonly.

THEADIRSCONTAINS:

InertialReferenceSystemonly.

AirDataDystemonly.

InertialReferenceandAirDataSystems.

DMEDISTANCECANBEDISPLAYEDON:

TheNDsandtheDigitalDistanceandRadioMagneticIndicator（DDRMI）.

ThePFDs,theNDsandtheDDRMI.

TheDDRMIonly.

THETRAFFICCOLLISIONAVOIDANCESYSTEM（TCAS）DISPLAYSALLPOSSIBLETHREATTOAIRCRAFTON:

sPrimaryFlightDisplay（PFD）.

s（F/O）NavigationDisplay（ND）only.

BothNDs.

THEPRINCIPLEOFTHEAIRTRAFFICCONTROL（ATC）SYSTEMIS:

Tomanagecommunicationsbetweenaircrafttransponders.

ToreplytothegroundradarandTrafficAlertandCollisionAvoidanceSystem（TCAS）equippedaircraftsinterrogationsthroughtheairbornetransponders.

Toreplytotheairbornetranspondersinterrogationsthroughagroundradarstation.

THEPRINCIPLEOFTHEADFNAVIGATIONSYSTEMISTODETERMINETHERELATIVEBEARINGOFASELECTEDGROUNDSTATIONBY:

Thetransmissiontimemeasurementofsignalsbetweentheaircraftandthegroundstation.

Thecombinationofsignalsreceivedfromtwoloopantennasandfromoneomni-directionalsenseantenna.

Thecombinationofsignalsreceivedfromoneloopantennaandthegroundstation.

ADUALADFSYSTEMISCOMPOSEDOF:

Onereceiverandtwoantennas.

Tworeceiversandoneantenna.

Tworeceiversandtwoantennas.

THEPRINCIPLEOFTHEVORNAVIGATIONSYSTEMISBASEDON:

Acomparisonbetweenareferencephasesignalandavariablephasesignal.

Atransmissiontimemeasurementofsignalsbetweentheaircraftandthegroundstation.

ThecombinationofsignalsreceivedfromtheVORantennaandtheADFantenna.

THEMKRSYSTEMISUSEDFOR:

Theradionavigationphase.

Thelandingapproachphase.

Thetake-offphase.

THEVOR/MKRSYSTEMSARECOMPOSEDOF:

INCASEOFILS1FAILURE:

ILS2dataisprovidedtotheCaptain'

ILS1deviationsdisappearandarereplacedbyaLOCandaGSredflagonCaptain'

LOCandG/Sscalesarereplacedbyambercrosses.

DMEDISTANCECANBEDISPLAYED:

OntheDigitalDistanceandRadioMagneticIndicators（DDRMIs）,only.

OnthePFDsandNDsinmagentaandontheDDRMI'

s.

OnthePFDsinmagenta,ontheNDsingreenandontheDDRMI'

THERED"

RA"

FLAGISDISPLAYEDONTHECAPTAIN'

sPFD:

IncaseofRA1failureandwhentheslat/flaphandleisinposition1ormore.

IncaseofdoubleRAfailure,whenAPPROACHhasbeenselected.

IncaseofdoubleRAfailure,whentheslat/flaphandleisnotinthezeroposition.

IN"

ROSENAV"

MODE,WITHVOR1SELECTED,THEVORINDICATIONSDISPLAYEDBYTHENDARE:

Thedeviationbar,theselectedcourseandthebearingpointer.

Thebearingpointeronly.

Thedeviationbarandselectedcourse,only.

INROSEILSMODE,THEILSINDICATIONSDISPLAYEDBYTHENDARE:

TheG/SandLOCscalesonly.

ThedeviationbarandtheG/Sscaleonly.

Thedeviationbar,selectedcourse,G/SandLOCscales.

ILSIDENTIFICATIONCODE,WHENDISPLAYEDONTHEPFDsORTHENDs:

ComesfromtheFMGCdatabase.

Isreceivedanddecodedbynavigationreceivers.

IsamanualentryfromtheMCDU.

ONTHEPFDsORNDs,NEXTTOTHEIDENTIFICATIONCODEORTHEFREQUENCYOFASELECTEDSTATION,AN"

M"

INDICATES:

ManualtuningfromtheMCDU.

ManualtuningfromtheRMP.

Manualtuning（eitherfromMCDU