TheFlightPathDirector.
TheFlightPathVector.
Thepitchbar.
A
22自动飞行
在主飞行显示器上显示的标记>----O----<表示
飞行轨迹指引仪
飞行轨迹矢量
俯仰操纵杆
22AutoFlight
THEFLIGHTPATHDIRECTOR:
ReplacesthebarsincaseofFlightDirectorfailure.
IstheonlypossibledisplayforaFlightDirector.
IsdisplayedwhenTRK/FPAhasbeenselectedontheFCU.
C
22自动飞行
飞行轨迹指引仪
如果飞行指引仪失效，替换指引杆
是飞行指引仪唯一可能的显示
会显示，如果航迹/飞行轨迹角已经在飞行操纵组件（FCU）上选择了
22AutoFlight
WITHANAPENGAGED,PRESSINGTHE"PRIORITYP/B"ONASIDESTICK:
DisengagestheAP.
OverridestheAPwithoutdisengagement.
Thereisnoeffect.
A
22AutoFlight
THECONSEQUENCEOFANALPHAFLOORDETECTIONIS:
TOGA（full）thrustontheengines.
AnosedownordertoreducetheaircraftAOA.
Anautothrustdisengagement.
A
22AutoFlight
ATANYTIME,TODISENGAGETHEA/THRSYSTEM:
Pushtheprioritypushbuttononeithersidestick.
PushtheInstinctiveDisconnectswitchoneitherthrustlever.
SetthethrustlevertotheTO/GAgate.
B
按下推力杆任一边的自动解脱电门按钮
22AutoFlight
BOTHFLIGHTDIRECTORSAREENGAGED:
BypressingeitherFDP/BontheFCU.
Automaticallyatsystempowerrise.
ByselectingamodeontheFCU.
B
22AutoFlight
THEFLIGHTPATHDIRECTOR（FPD）SYMBOLPOSITIONISCOMPUTEDBYTHE:
FlightAugmentationComputers（FACs）.
AirDataandInertialReferenceSystem（ADIRS）.
FlightManagementandGuidanceComputers（FMGCs）.
B
22AutoFlight
THEBASICFUNCTIONSOFTHEFACARE:
Flightmanagementandruddertrim.
Flightenvelopeandruddercontrol.
Flightenvelopeandflightmanagement.
B
22AutoFlight
THEMULTIPURPOSECONTROLANDDISPLAYUNIT（MCDU）DISPLAYS:
Airportsorwaypointsaroundtheaircraftposition.
Alldatarelatedtotheflightmanagementfunctions.
Thestatusofguidancefunctionsandtheirmodes.
B
22AutoFlight
THETHRUSTTARGETISCOMPUTEDBYTHE:
FlightManagementandGuidanceComputer（FMGC）.
FlightAugmentationComputer（FAC）.
EngineInterfaceUnit（EIU）.
A
22AutoFlight
THEBRAKING/STEERINGCONTROLUNIT（BSCU）:
AllowscontroloftheNoseWheelSteeringduringautomaticlandingwithordersfromtheFMGC.
AutomaticallydisengagestheAPat60kts.
AutomaticallydisengagestheA/THRat60kts.
A
22AutoFlight
THEFMGCFUNCTIONSARE:
FlightManagementandFlightEnvelopeProtection.
FlightManagementandFlightGuidance.
FlightEnvelopeProtectionandYawaxiscontrol.
B
22AutoFlight
THETRIMFUNCTIONOFTHEFACIS:
Pitchtrim.
Ruddertrim.
Ailerontrim.
B
22AutoFlight
THEFLIGHTGUIDANCEFUNCTIONSARE:
Autopilot,FlightPlanandAutothrust.
Autopilot,FlightDirectorandAutothrust.
FlightManagement,AutopilotandAutothrust.
B
22AutoFlight
THEFLIGHTCONTROLUNIT（FCU）ISNORMALLYUSED:
Foralong-termorderselection.
Forashort-termorderselection.
Fororderselection,iftheguidanceismanaged.
B
22AutoFlight
YOUCANACCESSTHEAUTOFLIGHTSYSTEM（AFS）TESTSFROMTHE:
FlightControlUnit（FCU）.
MCDU.
FlightAugmentationComputer1（FAC1）.
B
22AutoFlight
THEINTERFACEBETWEENTHEAUTOFLIGHTSYSTEM（AFS）COMPUTERSANDTHECENTRALIZEDFAULTDISPLAYSYSTEM（CFDS）IS:
TheFlightAugmentationComputer1（FAC1）.
TheMCDU.
TheFlightManagementandGuidanceComputer（FMGC）2.
A
22AutoFlight
THEAUTOMATICFLIGHTSYSTEM（AFS）COMPUTERSARETHEFLIGHTMANAGEMENTANDGUIDANCECOMPUTERS（FMGC）AND:
ELevatorAileronComputers（ELACs）.
SpoilerElevatorComputers（SECs）.
FlightAugmentationComputers（FACs）.
C
22AutoFlight
ONTHEFLIGHTCONTROLUNIT（FCU）THESPEED/MACHSWITCHING:
Isautomatic.
Mustbeperformedbythecrewfortheclimbphaseonly.
Mustbeperformedbythecrewbothfortheclimbanddescentphases.
A
22AutoFlight
PRESSINGTHEHEADING-VERTICALSPEED/TRACK-FLIGHTPATHANGLE（HDG-V/S/TRK-FPA）P/BONTHEFLIGHTCONTROLUNIT（FCU）:
ChangestheTRK-V/SintoTRK-FPAonthePFD.
ChangestheFlightDirector（FD）symbolsintoFlightPathVector（FPV）andFlightPathDirector（FPD）andviceversaonthePFD.
Hasnoeffectontheindications.
B
按下飞行控制组件（FCU）上的HEADING-VERTICALSPEED/TRACK-FLIGHTPATHANGLE（HDG-V/S/TRK-FPA）P/B按钮
在主飞行显示器上变TRK-V/S为TRK-FPA
改变飞行导向仪信号（FD）为飞行轨迹矢量（FPV）和飞行轨迹导向仪，在主飞行显示器上反之亦然
在显示上没有效果
22AutoFlight
THETHRUSTLIMITISCOMPUTEDBY:
TheFMGCaccordingtotheAP/FDmode.
TheECU（CFM）/EEC（V2500）accordingtotheThrustleverposition.
TheECU（CFM）/EEC（V2500）accordingtoAP/FDmode.
B
推力限制由
飞行管理导向计算机据自动飞行/飞行指引仪模式计算
ECU（CFM）/EEC（V2500）据推力杆位置计算
TheECU（CFM）/EEC（V2500）据自动飞行/飞行指引仪模式计算
22AutoFlight
WITHTHEA/CINFLIGHT,THEAPENGAGEDANDTHEA/THRACTIVE,THEA/THRMODE:
CanbechosendirectlybythepilotontheMCDU.
DependsontheAP/FDlateral（ROLL）mode.
DependsontheAP/FDvertical（PITCH）mode.
C
飞机在飞行中，实施了自动飞行，飞机推力活跃，飞机推力模式
飞行员可以直接在多功能控制显示组件上选择
取决于AP/FD横轴（横滚）模式
取决于AP/FD纵轴（俯仰）模式
22AutoFlight
WHENTHEFDTAKE-OFFMODEENGAGES,THEA/THR:
Automaticallyengagesandisactive.
Automaticallyengagesandisnotactive.
Doesnotautomaticallyengageandtheenginesarecontrolledbythethrustlevers.
B
22AutoFlight
WITHTHEA/CINFLIGHT,THEA/THRNOTENGAGED,THETHRUSTLEVERSINCLBGATE,ANALPHAFLOORISDETECTED:
TheA/THRwillnotengagebecausetheenginesarealreadyinCLBthrust.
TheA/THRautomaticallyengagesbutisnotactive.
TheA/THRautomaticallyengagesandcontrolstheengineswithaTOGAthrusttarget.
C
22AutoFlight
THEFCUALLOWS:
SelectionofFGmodes（functions）.
Selectionofradio-navfrequencies.
IRSalignment.
A
22AutoFlight
WHENFAC1P/B"FAULT"LIGHTIS"ON":
TheFAC1ruddercontrolfunctionshavefailed.
Thespeedlimitcomputationhasbeenlost.
FAC1hasfailed.
C
22AutoFlight
THECOMPUTERSCHECKEDDURINGAUTOFLIGHTSYSTEM（AFS）TEST,ARETHE:
FlightManagementandGuidanceComputers（FMGCs）only.
AFSLinearreplaceableUnits（LRUs）.
FMGCsandFlightControlDataConcentrators（FCDCs）.
B
22AutoFlight
WITHAP1ANDAP2NOTENGAGED,FD1ANDFD2ENGAGEDANDA/THRACTIVE:
FMGC1controlsengine1andFMGC2controlsengine2.
FMGC1controlsbothengines.
FMGC2controlsbothengines.
B
22AutoFlight
INNORMALOPERATION,WITHBOTHMCDUSSHOWINGTHESAMEPAGE,AMODIFICATIONMADEBYTHEPILOTONMCDU1ISSENTTOMCDU2:
Directly.
FromFMGC1throughFMGC2.
FromFMGC1,FMGC2andRMP2.
B
22AutoFlight
INCASEOFFMGC1FAILURE,FMGC2AUTOTUNES:
Side2NavReceiversthroughRMP2andside1NavReceiversthroughRMP1.
Side2NavReceiversthroughRMP2andside1NavReceiversdirectly.
Side1andside2NavReceiversdirectly.
B
22AutoFlight
WITHAPENGAGED,THEFLIGHTAUGMENTATIONCOMPUTER（FAC）COMPUTESTHETURNCOORDINATIONORDERFROMTHE:
A/Clateralacceleration.
FlightManagementandGuidanceComputer（FMGC）rollorder.
FMGCyaworder.
B
22AutoFlight
INFLIGHT,INCASEOFATEMPORARYLOSSOFELECTRICALPOWERTOFAC2,FAC2P/B"FAULT"LIGHTCOMESONAND:
FAC2canbemanuallyresetusingFAC1P/B.
FAC2canbemanuallyresetusingFAC2P/B.
ThereisnowaytoresetFAC2.
B
22AutoFlight
THEPOSITIONOFTHEAIRCRAFT,USEDINTHEFLIGHTPLAN,ISCOMPUTEDBY:
TheFGpartoftheFMGC.
TheFMpartoftheFMGC.
TheDMC.
B
22AutoFlight
THEFLIGHTPLANNINGIS:
Thefunctionthatintegratestheroutestheaircraftmustfollowandtheconstraintstoconstructaflightplan.
Thefunctionthatgivestheaircraftpositionandthefollow-upoftheflightplan.
Theratioofthecostoftimetothecostoffuel.
22自动飞行
A
飞行计划
其功能结合了飞机必须遵循的航路和制定飞行计划的约束
它的作用就是为飞机提供位置及此飞行计划的后续工作
是花费的时间与消耗的燃油之间的比率
22AutoFlight
ONTHENAVIGATIONDISPLAY（ND）,THEAIRCRAFTMODELISREPRESENTEDFIXED:
WhateverROSE-NAV,ARC,orPLANmodesareselectedontheFlightControlUnit（FCU）.
InPLANmodeonly.
AllthetimeexceptinPLANmode.
C
22AutoFlight
THEYAMDAMPERACTUATORSENDSAMECHANICALFEEDBACKTOTHEPEDALS:
Fordutchrolldamping.
Forenginefailrecovery.
Never.
C
偏航阻尼器作动筒发送一个机械的反馈到踏板上
为了阻尼荷兰横滚
为了恢复发生故障的发动机
从不发送反馈
22AutoFlight
WHENTHEAPISNOTENGAGED,THEYAWDAMPERORDERSARENORMALLYCOMPUTEDBYTHE:
ElevatorAileronComputer（ELAC）.
FlightManagementandGuidanceComputer（FMGC）.
SpoilerElevatorComputer（SEC）.
A
未使用自动驾驶时，偏航阻尼器指令正常情况下是由什么来计算的？
升降舵副翼计算机（ELAC）
飞行管理和导向计算机（FMGC）
扰流板升降舵计算机（SEC）
22AutoFlight
THEMANDATORYPARAMETERUSEDBYTHEALPHAFLOORDETECTIONIS:
A/Cselectedspeed.
A/Cweightandselectedspeed.
A/CAngleOfAttackandslat/flapconfiguration.
C
迎角基线探测所使用的强制性参数是
飞机选择的速度
飞机重量和选择的速度
飞机迎角和襟缝翼构型
22AutoFlight
ONTHEPFD,THEPREDICTEDVFE（MAXIMUMFLAPEXTENDEDSPEED）IS:
Onlydisplayedwhenaircraftaltitudeisbelow15000ft.
Shownbyanamberstripalongthespeedscale.
Thespeedcorrespondingtothebestlifttodragratio.
A
在主飞行显示器上（PFD），可预测的VFE（副翼最大可延展速度）是
只有当飞机高度低于15000英尺才显示
沿着速度标尺显示的琥珀色线条
对应于最大升力与阻力比率的速度
22AutoFlight
THETARGETAIRSPEEDSYMBOLISDISPLAYEDONTHEPFD:
InmagentawhenitismanuallyenteredontheFlightControlUnit（FCU）.
Eitherinmagentaorcyanorinnumericformwhenoutofthespeedscale.
Asacyandoublebar.
B
目标空速标记显示在主飞行显示（PFD）上
当它被人工录入飞行控制组件（FCU）时，是红紫色的。
当其超出速度刻度时，可呈现为红紫色，青色或以数字式方式。
作为一个青色的双条线
22AutoFlight
THESTALLWARNINGSPEED（VSW）ISCOMPUTED:
Continuously.
BytheFlightAugmentationComputers（FACs）inrollalternatelaw.
BytheFACsinpitchalternatelaworpitchdirectlaw.
C
失速警告（VSW）的速度
被连续地计算
由飞行增压计算机按照横滚转变规则计算
由飞行增压计算机按照横滚转变规则或俯仰引导规则计算
22AutoFlight
ON
升级会员 