改装-手册737-300机组辅助

飞行回起飞回氧气测试 增压方式选择器自 发动机起动手柄切 (RVSM5000英尺--误差≤45 组件自 起落架收上并中 襟翼收上，无 过渡高（度）高度表标准气压并交叉检 RVSM空域两个主高度表指示误差不大于±200英尺(60米TCAS正 起动回 燃油起动回 燃油＿磅，＿泵接 MCPV2＿、航向＿、高度 起飞速度V1＿、VR＿、 起飞前CDU输入完 方向舵和副翼配平灵活和 滑行和起飞简令完 应答机按需.. 防冰 发动机起动电门连 自动刹车 发动机起动手柄慢车卡 飞行检 起飞回 着陆回 板预位，绿 起落架放下，绿 襟翼＿，绿灯燃油泵全关 襟翼收 气象关 离机安全检回IRS方式选择器关 组件关 由机组完成航后工作 APU引气关 计时1APU或地面电源关 电瓶关 侧窗(两侧)关 Left（左座）R

PM：Pilot （驾驶员0 下回0 下回增压着陆高度 再现检 着陆数据ＶREF＿，最低高（度 进回高度表调＿＆交叉检 航道和频率检 ：批准人批准人生效日期：2013/11/25737-300/400

（简令应该尽快完成 起飞简进近简…飞机状况（MEL）使用跑道（状况）…特殊单发离场程序（如适用应遵循该程序的要求和预计滑行、进跑道路线；低能见程序（如需扇区安全高度…机场标高…过渡高度层…进港程 核实进近方式及进近图…航道（向台航向图起飞使用襟翼…配平；假设温度…推力…组件、引V1…VR…其他必需复习或机组责任分工（包括观察员）任务DA(H)或复飞点（MAP）着陆重量…襟翼…任何有关程序的相应信息及其他特殊要求机组AFDS临时更改跑道及离场临时更改跑道及进场跑道、离场程序（SID）…DA(H)MDA(H)导航调谐频率（ILS、VOR、NDB）…导航台识别码：生效日期：B737-300/400NORMALCHECKLIST AFTEROxygen Instrumentstransferswitchs Windowheat PressurizationMode FlightinstrumentsHeading Parkingbrake Enginestartlevers RVSMFLIGHTPLAN (RVSMThedifferencebetweeneachprimaryaltimeterandairportelevationisnomorethan75FT)Thedifferencebetweentwoprimaryelevationatsealevel--difference≤40elevationat5000feet--difference≤45-elevationat10000feet--difference≤50Enginebleeds Packs LandinggearUPand FlapsUP，no TRANSITIONALTITUDE(HEIGHT)AltimetersSTD＆CROSSCHECK BEFOREENTERINGRVSMAIRSPACE--Twoprimaryaltimetersindicateadifferenceofnomore±200feet(60TCAS A/P BEFORE Stabilizertrim PressurizationLAND PressurizationLAND Landingdata Landingweight Approachbriefing BEFOREPapers FlightdeckdoorClosedand FuelLBS，PUMPS Windows CDUpreflight Rudder&ailerontrimFreeand Taxiandtakeoff Anticollisionlight TransponderAS AltimetersSET＆CROSS CourseandFrequency ENGINESTARTswitches SpeedbrakeArmed，green LandinggearDown,green ，green Fuelpumps Probeheat Hydraulicpanel Parking Enginestartlevers Weatherradar BEFOREGenerators Probeheat Anti- Packs Isolationvalve ENGINESTARTswitches Recall Autobrake EnginestartleversIDLE Flightcontrols Groundequipment

PF：PilotIRSs IRSs Window Packs Emergencyexitlights -IFFLIGHT FLIGHTCHECKSExteriorLights APU Timing1APUorground Timing20Batteries Windows（both 737-300/400TakeoffApproachAIRCRAFTSTATUS（MEL）…adverseTakeoffApproachAIRCRAFTSTATUS（MEL）…adverseWEATHER altitude…TerrainandAirspaceRunwayinuse(conditions)... InitialNAVAIDstuning.NoiseAbatementSpecialengineoutprocedurefordeparture(followthespeedandflightpathrequirementsifapplicable)Expectedtaxi,lineuproute;Lowvisibilityprocedures(asneeded)Actions&dutiesforrejecttakeoffbeforeActions&proceduretocontinuetake-offafterReturntoland?Divert Thrust...Packs…;Bleed…;Anti-V1…VR…Anyotheritemsthatmustbereviewedrelatedtothedutydivisionbetweenflightcrew(includingobserver)SupplementaryBriefingtoTemporaryRunwayChangeandDepartureRunway…,SID..initialheading…,initialCDUinput:modifyrunwayanddeparture.;Takeoffspeeds...NAVAIDSExpectedtaxi,andlineupNote:taxiandtakeoffbriefingshouldbe beforeenginestart,andcanbeupdatedduringstraighttaxiingorstoptaxiifnecessary. conditions(destination, TheeffectivenessofallthechartstobeMinimum Procedure….Runwayinuse…surfaceconditions…Verifyapproachmodeandcharts…course(inboundheading)A/Pandcorrespondingnagivationfrequency….NAVAIDsidentificationcodeorMorseCode…Verticalprofileofminimumaltitude,crossingaltitudeandapproachaltitudeDA(H)orMDAMAPandMissedapproachReviewgoaroundAuto Landingweight...Flaps...Expectedlandingdistance…vacateandtaxiroute.lowvisibilityprocedure…SpecialEngineoutprocedureAlternateairport….diversionAnyinformation,procedureandrequirementrelatedtonon-normalsituation…FlightcrewAFDSmanagementandobserver’sSupplementaryBriefingtoTemporaryRunwayChangeandArrivalArrivalprocedure…,runwayinuse…FinalCDUinput:modifyrunwayandDA(H)orMDANAVAIDstuning(ILS,VOR, code...morseExpectedrunwayvacateand,taxiMissedapproachNote:approachbriefingshallbe plished40nmbeforetheTopofDescent,andupdatedabove10000ftifTableof标B737- 自动着B737-300WindLimitationsforAutoland、CrosswindLimitationsforTakeoffLanding、LowVisibilityCrosswindWINDCORRECTIONFORB737-300机体触B737-300GroundContactUNPRESSURIZEDTAKEOFF、TAKEOFFWITHOUTENGINE地面除冰/防冰程De-iceandanti-iceonColdWeatherRVSM操作的高度显示限AltitudeDisplayLimitduringRVSMRVSM运行紧急程序检查 RVSMOperationEmergencyProcedureRVSMRVSMOPERATIONNORMALB737机型RNAV标准运行程FlapManeuver 机型Non-PrecisionApproach海南航空机长/驾驶舱广播HNACAPTAIN/COCKPIT民用航空机长职责和稳定进ResponsibilityandAuthorityofPilotinCommand&StabilizedPAPERSONBOARD梯度与爬升/下降率TableofComparingGradientandClimb/descentMeterstoFeetB737CATⅡ运行简易检查单和

页1-2-2-3-4-4-5-6-7-8-9-10-11-12-13-14-14-15-16-0-B737-300B737-300windLimitationsfor单位：节/米/UNIT:knot/VerticalB737-B737-300侧风起降标B737-300CrosswindLimitationsforTakeoffand单位：节/米/UNIT:knot/DryWet结冰、积冰/在滑溜跑道上，侧风能力取决于道面条件、飞机载荷和的技术。pilotskill.B737LowVisibilityCrosswind单位：节/米/UNIT:knot/注口标高200英尺以下，若机载设备探测侧风分量或塔台报告稳定风分量超过Thecrosswindlimitstandardisbasedonthecrosswindcomponentofthestablewindincaseofastronggust.Go-aroundshallbeinitiatedimmedia yiftheairborneequipmentdetectedcrosswindorthetowerreportedstablewindcomponentisoverthecrosswindlimitstandardatanaltitudeoflessthan200feetawayfromtheairportthresholdelevation.2、若使用不对称反推，在湿或污染的跑道上侧风指南减小5KTsThecrosswindinstructionshallbereducedby5knotsonthewetorcontaminatedrunwayiftheasymmetryreversethrustisused.3、在滑溜跑道上，侧风能力取决于道面条件、飞机载荷和的技术。Crosswindabilitydependsontherunwaycondition,aircraftloadingandpilot’stechniqueonslipperyrunway.Forautolanding,V(target)=V(ref)+5,nowind5、使用人工油门着陆时，V目标=VrefFormanuallanding,V(target)=V(ref)+wind6、风修正值=1/2稳定顶风分量+（阵风值-全稳定风值Windcorrection=1/2stableheadwindcomponent+(gustvalue-fullstablewind7、注：风速单位为海里/小时（1米/秒≈2海里/小时Note:theunitofwindspeedisnm/h8、风修正值最大为20KTs，最小为Theumwindcorrectionis20KTs,theminimumis59ThewinddirectionisbasedonthelandingrunwayThewindmustbecorrected(thesameas4)iftheautothrustisnotusedwhenthelandingspeedisadjustedaccordingtothenon-normalchecklist.UsethelowercrosswindstandardiflowvisibilityandrunwayconditionlimitsexistWINDCORRECTIONFORLANDING一、使用自动油门着陆时，V目标=Vref+5，不做风值修Whenautothrottleisusedforlanding,Vtarget=Vref+5,windcorrectionnot二、使用人工油门着陆时，V目标=Vref+风值修正Whenmanualthrottleisusedforlanding,Vtarget=Vref+wind风修正值=1/2稳定顶风分量+（阵风值-全稳定风值Windcorrection=1/2constantheadwindcomponent+(gustcomponent–fullconstantwindcomponent)注：风速单位为节（1米/秒≈2Note:Windspeed–knot(1meter/second≈2风修正值最大为20Kt，最小为umwindcorrectionis20Ktandminimumis风向以着陆跑道方向为基准 WinddirectionisbasedonthelandingrunwayWhenlandingspeedisadjustedaccordingtotheabnormalchecklist,windcorrectionmustbemadeifautothrottleisnotused.(Referto2forwindcorrectioncalculation)B737-300机体触地极B737-300GroundContactPithAttitudeLimitoftheAftFuselageGroundContactParkingLandingCondition(0Wingstrike,EngineBank11.1°（以典型的5°姿态接地）11.1°(touchdownwithtypicalattitudeof5°)Vref5Kt，姿态增大1°。延长拉平将增加机身姿态2-3°。Note:1、TouchdownwiththelandingspeedofVref+anygustcorrectionand4-6°pitch.Increasepitchfor1°withevery5KtbelowVrefExtensionofflarewillincrease2-3°ofpich.2、Bandofwingstrikewillincreasewithlesslandingpitchattitude,higheraltitudeaboveground,andlessLandingflaps.非增压起飞（UNPRESSURIZEDTakeofforlandwithoutenginebleedwhenAPUisnot起飞组件电 自Pack 活门电 Isolationvalve 发动机引气电 Enginebleed Airplanewithcabinpressurizationcontrol机舱高度指示 设定为高于机场标高2000英Cabinaltitude set2000feetabovelanding机舱速率选择 索Cabinrate 增压方式选择 备Pressurizationmode 飞行/地面电 飞Flight/ground 起飞后（AFTERNote：Ifenginefailureoccurs,donotpositionengineBLEEDairswitchesONuntilreaching1500feetoruntilobstacleclearanceheighthasbeenattained.Atorabove400feetandbeforereaching2000feetabovelandingelevation:2号发动机引气电 No.2enginebleed 当机舱爬升率指示器稳定时(whenCABINrateofCLIMBindicator1号发动机引气电 No.1enginebleed 活门电 自Isolationvalve Airplanewithcabinpressurizationcontrol增压方式选择 自Pressurizationmode 无发动机引气的起飞（TAKEOFFWITHOUTENGINETakeofforlandwithoutenginebleedwhenAPUis起飞Note：Ifanti-iceisrequiredduringtaxing,airplaneshouldbeconfiguredas“takeoffwithoutenginebleed”beforetakeoff.Note：Ifanti-iceisnotrequiredduringtaxing,airplanemaybeconfiguredas“takeoffwithoutenginebleed”afterenginestart.右组件电 自Rightpack 活门电 Isolationvalve 左组件电 自Leftpack 1号发动机引气电 No.1enginebleed APU引气电 APUbleed 2号发动机引气电 No.2enginebleed 配平空气电 Trimair 机翼防冰电 WINGANTI-ICE TheWINGANTI-ICEswitchmustremainOFFuntiltheengineBLEEDairswitchesarerepositionedtoONandtheISOLATIONVALVEswitchisrepositionedtoAUTO.起飞后（AFTERNote：Incaseofenginefailure,switchonenginebleedtillreaching1500feetorobstacleclearance2号发动机引气电 No.2enginebleed APU引气电 APUbleed 当机舱爬升率指示器稳定时(whenCABINrateofCLIMBindicator1号发动机引气电 No.1enginebleed 活门电 自Isolationvalve 发动机交输起动（ENGINESTARTUSINGVerifythattheengineisclearedbeforeapplyingthisNo.1enginestartis发动机引气电 Enginebleed APU引气电 APUbleed 空调组件电 Air-conditioningpack 活门电 自Isolationvalve Verifybleedsupplyforengine发动机推力手柄（工作的发动机 前推手柄直到引气管道压力指示Enginethrustlever(engine Advancetillbleedductpressureindicates30不工作的发动 起Enginenot ApplynormalcrossbleedstartAfterstartercutoff,adjustthrustofbothenginesas起飞决断示地面设 移起飞决断示地面设 移正常程 重新开除非飞机受与批准的地面除冰程序相一致的II和IV型使用除冰液所地面地面除冰/——程序结警警刹住机长安定面配 全机头向下机长发动机和APU引气电门……….关 副驾驶空调组件（双组）………………关断副驾驶

按需副驾驶雨情况下滑行时，要将襟翼收起。襟翼放下滑行时主起落架溅起的积

霜雪霜雪

除冰防冰报除冰防冰报 收到并记液体类型；浓度（仅对II和IV型）；最后运用防冰液的当地时间；APU引气电门按需副驾驶发动机引气电门空调组件自动副驾驶安定面 单位机长保持时 确

襟襟 起飞位安定面配平 单位机长保持时 执行除冰防冰程序，向ATC报告情况，必要时滑回停机位。

III类 IV 机长3030更小的间隔时间增加推力到70%N1。起飞前检 执保持时 重新确定或证

干 不干55分钟之内起飞，否则重新除冰/4- 生效日期：Note:RefertoFCOMsupplementaryprocedure“AdverseWeather”SPsection16Checkthefollowingbeforede-iceandanti-iceoperationonground:

mended30Note:Whenoperatinginconditionsoffreezingrain,freezingdrizzle,freezingfogorheavysnow,additionalmomentaryrun-upsto70%N1atintervalsof10minutesorlessshouldbebeforetakeoff holdover reconfirmorIfrequired,crewmembershouldjudgeaccordingtocockpitandcabinchecksandweatherconditionchanges,thefinaldecisionshouldbemadebythecaptain.eificeadiagramHoldovertimeDe-ice/anti-iceto asneededIftaxiHoldovertimeDe-ice/anti-iceto asneededIftaxirouteisthroughslushorstandingwaterinlowtemperaturesorifprecipitationisfallingwithtemperaturesbelowfreezing,taxiwithflapsup.Taxiingwithflapsextendedsubjectstheflapsandflapdrivestosnowandslushaccumulationsfromthemaingearwheels.Leadingedgedevicesarealsosusceptibletoslushaccumulations.air/groundcommunication(useVHFasestablishcaptain(C),firstofficerparking set upthrust idlestabilizer FullAPLNOSEDOWNTrimtheairplanetotheelectricalAPLNOSEDOWNlimit.ThencontinuetrimmingmanuallytothemanualAPLNOSEDOWNlimit.Thefullnosedownpositionpreventsde-icingfluidandslushrun-offformenteringthestabilizerbalancepanel.engineandAPUbleedair holdover Refertoholdovertimeonthereversesideofthischecklist.CaptaindecidesholdovertimeaccordingtoATIScrewobservationandexperiencejudgementafterdiscussionwithcrewmembers.ground normal engineanti- asneededDuringallgroundoperations,engineanti-icemustbeturnedonificingconditionexistorisanticipated.winganti- asneededUsewinganti-iceduringallgroundoperationsbetweenenginestartandtakeoffwhenicingconditionsexistorareanticipated,unlesstheairplaneisprotectedbytheapplicationofTypeIIorTypeIVfluidincompliancewithanapprovedgroundde-icingprogram.De-iceandanti-iceonOncede-iceoperationbegins,anyairplanemovementorconfigurationchangemustbecommandedbygroundcrew.FlightcrewmustimmediayshutdownenginesandturnonalllightingsystemwhentheycannotuseVHFtoestablishcommunicationwithdeicingcommanderwhiledeicingatidle.de-iceandanti-ice receivedde-iceandanti-ice receivedandtypeofconcentration(onlyforIIandIVtypefluid)localtimeforfinalapplyinganti-icefluidverifyorally:“de-iceandanti-icecheckAPUbleedair asneededWaitapproximateoneminuteaftercompletionofdeicingtoturnengineBLEEDairswitchesontoensurealldeicingfluidhasbeenclearedfromengine.Enginebleedair on auto UnitsVerifytrimhasbeensettotakeoff

HoldoverHoldovertime

5minutes,orrepeatbeforetakeoffcheckFreezingFreezingFreezingLightfreezingRainoncoldFlap setFlap settakeoffStabilizer UNITS(C)Holdover verifyvalid(C)Ifwithinholdovertime,executede-iceandanti-icebeforetakeoffcheck,andrefertotakeoffdecisionschematicdiagramtodecidewhethertotakeoffornot.Ifbeyondholdovertime,decidewhethertotakeoffornotaccordingtocockpit,cabinandexteriorinspectionandbeforetakeoffcontaminationcheck,whichshouldbeassistedbyqualifiedgroundcrew.Ifthereisicecontaminationonairplaneandwing,contactmaintenanceorflightoperationdepartmenttoaskforanotherde-iceandanti-iceprocedureexecution.ReporttoATCandtaxibacktoapronifnecessary.4- effective：

EngineEnginerun- DoasneededRun-up

TypeIIorIVcheckbeforeTypeofcheckbeforeTypeofcheckbeforeTakeoffTakeoffwithin5minutes,orrestartde-ice/anti-iceB737-300B737-300如果需要缘和后缘襟翼放下的情况下在结冰条件下长时间操作襟翼…………15 在完成除冰或地面检查之前,建议不要将襟翼收到小于15。结冰条件下着陆之后安定面配平……调到0-2单位副驾驶防止溶雪或冰流入平衡区,并防止安定面限制电门冻结襟翼收上后,人工配平大约需要8圈。警告:为了避免人员,在使用电动配平之前,确保安定面配平轮手柄收进放好。发动机防冰………………按需副驾驶（F/O）发动机暖车…………………按需完成机长暖车过程中尽可能地使用高推力调定，推荐使用70%N1（但不超过）。一次大约运转30秒钟,间隔为30分钟。如果机场道面情况和飞机情况不允许推力手柄增加到70%,则定时尽可能使用高推力调定。注：当存在冻雨、冻雾、大雪的情况，应当额外考虑10分钟或更短瞬间地增加推力到70%N1。B737-300B737-300ColdWeatherTaxiinandIfprolongedoperationinicingconditionswiththeleadingandtrailingedgeflapsextendedwasneeded:: Retractiontolessthanflaps15isnot mendeduntilicehasbeenremovedoragroundinspectionhasbeenmade.AfterlandinginicingStabilizertrim……set0-2 Preventslushoriceleakintothecavertandfrozenofthelimitingswitchofthestabilizer.Whenflapsretracts,itneeds8cyclesforthemanualtrim.Warning:Toavoidinjuryof nel,ensuringstabilizertrimwheelisstowedbeforeelectrictrimisused.Engineanti-ice……asneeded Ificingconditionsexist,engineanti-icemustbeON.Enginerun-up…………….Doas butnothigherabove70%N1)at30minuteintervalsfor y30secondsIfairportsurfaceconditionsandtheconcentrationofaircraftdonotpermittheenginethrustleveltobeincreasedto70%N1,thensetathrustlevelandtimeatthatthrustlevelashighaspractical.NOTE：whenoperatinginconditionsoffreezingrain,freezingfog,orheavysnow，run-upsto70%N1atintervalsnolongerthan10minutesshouldbe（有意空白de-iceandanti-icefluidisnotused dforanti-iceintheholdovertimevarieswiththesituationchangesfrommediumtolight,anditislessthantheminimumtimeinrangeundersevereweathertheholdovertimewillbereducedincaseofthejetstream,highwindspeed,highmoistureandthetemperatureoftheairplaneskinisbelowoutsideairtheholdovertimeforlightfreezingrainshouldbeusediffreezingdrizzleraincannotbeproperlythereisnoholdovertimeforicecrystal,snowcrystalorsnowballweatherconditions,andbeforetakeoffcontaminationcheckinthecabinshouldbecompletedwithin5minutesbeforetakeoff;don’ttakeoffinhailormediumtoseverefreezingrainthistableisonlyusedfordeparturescheduleandshouldbeusedwithde-ice/anti-icechecklist,andthefinaldecisionforholdovertimeshouldbedecidedbytheThetimeofprotectionwillbeshortenedinheavyweatherconditions.Heavyprecipitationratesorhighmoisturecontent,highwindvelocity,orjetblastmayreduceholdovertimebelowthelowesttimestatedintherange.HoldovertimemaybereducedwhenaircraftskintemperatureislowerthanOAT.（IntentionallyB737-300机组辅助资 海南航 操作的高度显示备用高度表不满足RVSM空域的精确度RVSM运行时机长和副驾驶飞行中高度显示允许的最大差值为200英尺；在RVSM运行中，地面上高度显示允许的最大差值见下表：机场之间显示允许的最40755，000457510，0005075注：如计划在RVSM空域飞行，使用限制章节RVSM高度 调此检查的基准气压设定是场压或标准气压（29.92英尺柱或1013毫巴）中首先顺时针旋转气压调定旋钮至高于此基准值的气 高度表读数之间的最大容差值列于下表高电/电/5,00010,00015,00020,00025,00030,00035,00040,00050506070801001201401605080叉检查变成无确切结果。在10，000英尺到29，000英尺之间，怀疑差异大于400英尺时，应通过地面维修检查来核实。在29，000英尺到最大使用高度之间，怀疑差异大于500英尺时，应通过地面维修检查来核实。B737-300 AltitudeDisplayLimitduringRVSMTheaccuracyofthestandbyaltimetercannotachievethatrequiredinRVSMDuringflightusingRVSM,theumallowabledifferenceofthevaluesofaltitudedisplaysbetweenthecaptain’sandthefirstofficer’sis200feet.WhenusingRVSM,the umallowabledifferenceofthegroundaltitudedisplaysumAllowableDisplaysBetweenCaptain’sandFirstumDifferenceBetweentheDisplaysoftheCaptain’sortheOfficer’sandtheAirportSeaDifferenceAmongNOTE：ifplannedtoflyinRVSMairspace,useRVSMchartintheLimitationAtsteadylevelflightorontheground,dothisprocedurewhenobviousdifferenceoccursamong ThereferenceairpressuresettingofthischeckistheQFEorthestandardairpressure(29.92feetHgor1013millibar),whicheverisappropriate.Dothefollowingproceduretoallaltimeters:Firstly,rotatetheairpressuresettingknobclockwisetoairpressuresettinghigherthanreferenceThenrotatetheairpressuresettingknobanticlockwisetothereference umallowanceamongaltimeterSeaSeetheSeetheSeetheSeetheSeetheSeetheNOTE：Whenthealtitudeisabove10,000FTandspeedisabove0.4Mach,locationerrorwillleadtohigherallowancerapidlyanditcannotbedeterminedthroughdirectcrosscheck.Whenthealtitudeisbetween10,000FTand29,000FTandthedifferenceishigherthan400FT,errorshouldbeedandverifiedthroughgroundmaintenance.Whenthealtitudeisbetween29,000FTandumoperationaltitudeandthedifferenceishigherthan500FT,errorshouldbeedandverifiedthroughgroundmaintenance.左右左机组辅助资料[ALL] 海南航RVSM运行紧急程序中国区域严重颠簸/山地波导致约200要求引导指令避开附近高度上的空通ICAO区域飞机不能继续按照ATC飞行/飞机不能保持空域要求的导航性能精度,又不能获飞机需要绕飞天气,又不能得到事 RVSMOperationEmergencyProcedureChinaUnabletoconfirmthealtitudemaintainingabilityofaircraft/unabletomaintainclearedaltitude,initialactionsare:ReportATCwithdetailedinformationandintentionofMaintainclearedaltitudeasmuchaspractical,andassesstheImprovethevisualandTCASobservationofairtraffic,turnonexteriorlightstoalertvicinityaircraft;Notifythesquawking,altitude,positionandintentionviacurrentfrequencyand121.5/123.45asappropriate.WithonlyoneprimaryaltimeteroperatingCrosscheckstandbyInformATCcurrentlytheoperationisbasedononeprimaryTakeactionsaccordingto“Allprimaryaltimetersfailure”procedureiftheaccuracyofprimaryaltimeterscannotbeconfirmed.Automaticaltitudecontrolsystem,altitudealertsystemorallprimaryaltimetersEUIPMENT，consideroftheaircraft.IfATCprovideslateralandverticalseparation,flightandmaintainATCclearedIfATCisunabletoassignenoughseparationwithotheraircraft,requestATCtoleaveRVSMairspace.Severeturbulence/mountainwaveleadstoanaltitudedeviationofapproxima RequestATCvectorclearancetoavoidotherairtrafficonvicinityRequestATCtochangealtitudeifEmergencyoraltitudechangeisReportATCandrequesttoassignanotherflightIfunabletocontactATC,ThemethodofchangingFLis:rightturn30degreesfromtheaircraftcurrent;heading;andproceedwiththenewheading20kilometers,andthenleftturntoparalleltheoriginalroute,climbordescendtoanewaltitude,thenreturntotheoriginalroute.AlertvicinityaircraftviaWhentheaircraftcannotproceedwithATCclearance/maintainairspacerequirednavigationperformance,andunabletoobtainaclearancebeforehand.A.Turnleftorright90degreesawayfromassignedrouteortrackwhenMinimizethedescentrateasmuchaspossibleifunabletomaintainclearedOffset15Climbordescendtoanaltitudewith500ftdifferencewithnormaloperationAlertvicinityaircraftviabroadcasting,observe trafficwithvisualandreferenceACAS,turnonexteriorlights.Theaircraftneedstocircumnavigatefordangerousweather,butwithoutclearanceIfpossible,deviatefromtheorganizedtrackorrouteAlertvicinityaircraftviabroadcastingobserve trafficwithvisualandreferenceACAS,turnonexteriorlights.Offsetwithin10nm,maintainATCclearedD、Offsetmorethan10nm,changealtitudeasthefollowingtablewhentheaircraftiscloseto10nm.Descend300Climb300Climb300Descend300E.Whentheoffsetisbackwithin10nm,returntoassigned 得到ATC关于与指定高度的偏差超过90米（300英尺） 得到ATC关于与指定高度的偏差超过90米（300英尺） 的飞行高度层CFL。 超过150英尺（45米。在RVSM区域飞行推荐尽可能使用自动驾驶。由于设备失效，不能继续执行确认RVSM空域飞行所需设确认RVSM空域飞行所需设（高度表自动驾驶仪高度测量和告警系统，TCAS等，按MEL放行的项目不得影响RVSM飞行所需设备的使用良好状况，并对照最低设备（MEL）相关项目检查机组应注意的事项。起飞前，RVSM飞行所需 高度表指示误差检查：将高度表的拨正值按当地机场当时QNH表指示的标高值。当地机场已知标高和高度表显示高度之间的差值不得超过23米（75QFEQFE23（75。高度表指示 2.24SMS及时反馈，RVSM空域《大高度偏差报告》。8- ININDuringtheoperationinsideChinaarea,pilotsshouldchecktheChinaAreaCruiseLevelbeforesettinganaltitudewhentheyareclearedforanaltitudeinmeter.IfpilotsareinformedbyATCthatthereisadeviationofmorethan90meters(300feet)fromclearedaltitude,theyshouldtakeanactionimmediaytoreturntoclearedflightlevel.Whenthereisachangeofclearedflightlevel,theaircraftshouldleveloffattheclearedflightlevel,withadeviationnomorethan150feet(45meters)aboveorbelow.Itis mendedtouseautopilotduringoperationinRVSMarea.StrictlycarryoutTCASfalsewarningpreventionReportlateraloffsetasrequired.Crosscheckaltimetersonceevery60minutesatleast,andchecktheoperationstatusofotherequipmentrequiredforRVSMoperation.Fillincomputerflightplanthealtimeterrequiredvalue.TheflightcrewmustreporttoATCwhentherearefollowingsituationsUnabletocontinueRVSMoperationdueequipmentLossofredundancyofaltitudemeasurementEncounteredturbulenceaffectingaltitudemaintainingPrimaryaltimetersindicateadifferenceof200DeviatedfromATCclearedflightlevel300Theflightcrewmustreportthespecificconditiontothecompanywithin24hours.Befamiliarwithemergenciesanddisposalprinciple,andkeepgoodcrewRVSMOPERATIONNORMALINTHEINTHEVerifyequipmentrequiredforRVSMoperation(altimeters,AP,altitudemeteringandwarningsystem,TCAS,etc.).ItemsreleasedperMELshouldnotaffectthewelloperativestatusofequipmentrequiredforRVSMoperation.CheckflightcrewnoticesperMELrelateditems.IfthereisanyfailureindicationofequipmentrequiredforRVSMoperationbeforedeparture,actionsmustbetakentosolvetheproblem（returntoapron,contactmaintenanceanddispatch）. Altimeterindicationerrorcheck：setaltimetersettingtolocalairportcurrentQNH，checktheelevationvalueindicatedbyaltimeter.Ifthedifferencebetweenlocalairportactualelevationandaltimeterindicatedaltitudeshouldnotbemorethan23meters(75feet);inQFEreferencedairports,altimetersettingremainslocalairportcurrentQFE,altimetershouldindicatezero,theindicationerrorshouldnotbemorethan23meters(75feet).Altimeterindicationmustbeinlinewithrequirementsinaircraft’sOperationManual.Fillincomputerflightplanthealtimeterrequiredvalue. CheckpapersonboardfortheChinaAreaCruiseLevelandRVSMOperationEmergencyProcedureChecklist.RemembertochecktheredrectangularRVSMcriticalareamarkedaroundstaticportsonfuselage.CheckcarefullyanyrecordintheFlightTechnicalLogBookandreporttocaptain,verifytheequipmentstatusandmaintenanceactionstakenrelatedtoRVSMoperation.POSTReportanyfailurethatmayaffectRVSMoperation,fillinTechnicalLogBookcarefullyifnecessary.Whentherewasaseverealtitudedeviationinflight,flightcrewshouldreportittimelythroughSMSwithin24hours,andfillinRVSMAirspaceSevereAltitudeDeviation B737机组辅助资料 海南航RNAV标准运行程序RNAV飞行计 批飞机机载导航设备…RNAV机载导航数据 有GPS(如安装)和惯 核实工作正常、位置正RNAV航路和离场程 检ATC的RNAV航 核地图显示与文字显示一致，以确认航路的导航精度（GPS主功能可用 检GPS主功能不可用要求导航性能 检ND显示方 飞行指引 接水平导 预飞机位 检地图显示与飞机和跑道位置关系一致，航路显示与航图一跑道头位置更新（如可用 执 B737Supplementary RNAVStandardOperationPre-RNAVflight NavigationEquipments…CompliancetoRNAVRequirementsFlightData GPS(asinstalled)andIRS………VerifyoperativeandcorrectpositionRNAVRouteandSID ATCClearedRNAV ChecktheMAPdisplaysagreewiththescheduledflightplan,andverifytherouteiscorrect.NAVAccuracy(GPS IfGPSisnotavailable: BeforeNDDisplay Aircraft ChecktheMAPdisplaysagreewithairplaneandrunwaypositions,verifytheMAPiscompliancetothecharts.RunwayUpdates（if B737机组辅助资 海南航甚高频导航（自动／人工）电门（如安装 自水平导 核实接自动驾 核实接导航精度…随时机载导航数据 有如数据库FMC航路数据与纸质航图数 一如不一致…RNAV进场程序和跑 检查并正确显ND方 飞行指引 核实接水平导 核实接自动驾 核实接甚高频导航（自动／人工）电门（如安装 人任何影响RNAV飞行的事 报9 B737 AfterVHF（AUTO／MANUAL）Switches（as LNAV…………VerifyONAP……………VerifyONNAVAccuracy…………………MonitorMomentarilyBeforeDescentandFlightData IfthedatabaseisnotFMCRouteData………………compliancetotheChartIfnotcompliant………UseNon-RNAVSTARandRunway…………………VerifyCorrectND FDs…………VerifyONAP……………VerifyONInitialApproachFix(IAF)VHF（AUTO／MANUAL）Switches（as Post-AnyAffectedRNAV B737-300机组辅助资 海南航襟翼机动速FlapManeuver非ILSILS进近总（AC-121/135FS-2013-46在非ILS进近中使用CDF（CDFA：一种与稳定进近相关的飞行技术，在非ILS仪表进近程序的最后进近陆跑道大约15米（50英尺）的点或者到该机型开始拉平操作的点。使用CDFA技术进近时，为确保航空器在复飞过程中不低于公布的最低下降高度/高，我公司确定的在公布的最低下降高度/高以上白天增加50 间增加220英尺，当下降至此高度/高时，如果不具备着陆条件，应开始 为公布的最低下降高度/DDA/HMDA/H+50英尺（白天）或MDA/H+220英尺（夜间B737-700/800机组辅助资 海南航VNAV使用VNAV仪表进在进近中使用自动驾驶仪可自动驾驶仪提示和方式失效指更精确的航道和下滑道更低的RNP此程序不允许QFE要求FMCU7.1或更新的版自动飞行是非ILS进近的最好飞行方法在五边进近建立合适的目视参考之前，根据放襟翼计划，宣布“襟 在进行非精密进近时，可使用LNAVVOR/LOCHDGSEL方式，同时必须使用原核实航段（LEGS）页五边进近部分VNAV核实已经调谐并识别预期的导航台（莫尔斯电码或识别码下降至VNAVHOLDVNAVPTHVNAVALTMCP根据原始仪表指示核实高度位置，报：“XXXXVNAV方式生效后报出“VNAV“放轮“报“接近下滑轨迹 B737-700/800机组辅助资 海南航下，三个绿灯；襟翼15绿灯将发动机起动电门放到连续（CONT）动飞行指引系统）VNAVPTHLVLCHG。机组需要及时发现并修正以机组应该立即起始复飞调定板手柄到预位”宣布“着陆检查单越时实际高度并核实与进近图上所规定的高度是否一致或符合垂直剖面：“XXX点（点标或最后进近定位点等，高度检查，XXX（高度MCP高度应调到适当的高度限制（通常指下一个航路点的，保证进近下降时满足进近最低高度。为了防止非预期的改平，下一个航路点高度限制一旦满足，可立即将MCP重调到再下“100到最低“继续进近MDA上建立了足够的目视参考，“继续”断开A/P、A/T，飞机按照目视下滑线继按需下口令“关、开飞行指引MDA高度未建立目视参考喊出“襟翼15”，飞机复MDA高度未建立目视参考“MDA，不能见注意 B737-700/800机组辅助资 海南航上文中提到的MDA均为按照的要求调定昼间飞行：公司规定机EFIS面板上调定的最低高度使用公布的MDA英尺向上取整英尺的高度作为起始复飞或决定继续进近着陆的高度，此高度等同于在MCP板上调定的高度值。夜间飞行：公司规定机EFIS面板上调定的最低高度使用公布的MDA+50英尺+170英尺=MDA+220英尺，所计算出来的数值向100英尺昼间：最低高度MDA+50英夜间：最低高度MDA+50英尺+170英尺MDA英尺以上高度均需要向上取整英尺。注：对CL飞机，使用高度表游标MDA，不得以EFIS控制面板上调定的DHREF（决断高参考）为基准。喊话必须基于气压式高度表！，在接近公司规定的最低下降高度时有且只有两种选择清楚看到和，当在复飞点之前执行复飞并且未取得空通的指令时应按照公布的VNAV进近FMCArrivals页面选择进近程序调谐并识别相应的助航设不要人工输入进近或给程序增加航路点。如需额外的航路点参考，使用FIX页。当引导到五边时，选择直接切入航FAF，这样可以开始正LNAV航路点排序。核实/输入适当RNP，并用气压最低高度选择钮调定我公司规定的MDA。确保一旦复飞，复飞期间不会下降低于CAAC公布的MDA。速度如飞机没有速度干预功能，可在CDU里改变所需速度。同时必须严格空速的改变，按照飞机的自动的要求放出相应所需的襟翼（飞机自动计算当时性能，根据剖面自动）最后进近速度可按需在CDU里改变。使用VNAV进行最后的五边进近，机组必须严格垂直轨迹，任何时候不允降V/S B737-700/800机组辅助资 海南航满足稳定进近的情况时必须立刻近过程出现UNABLEREQDNAVPERF信息，机组应终止使用该进近方法模拟的 仪表进近（推荐在建立非精密进近经历时使用此方式（2）.为保持机组操作的熟练度，可在VMC条件下，选择使用飞行指引（3）.为了保持熟悉程序组可以按下列方法在飞ILS进近时用VNAV程序来确定ILS调