常用维修手册及维修文件介绍VIP

ManualandDrawingUsageInstructor:ZouLimingZuBiao,GeneralClassificationforManuals,CustomizedManual,Non-CustomizedManual,AMMAIPCWDM(AWM,AWL)SSM(ASM)FIM(TSM),SRMSWPM(ESPM)SOPM(PMS)MPDNTMITEM(TEM)CML(Airbus),PART1BoeingManualSystem,MyBoeingFleet:,PART1BoeingManualSystem,DeltaWebpage:,PART1BoeingManualSystem/AMM,PART1BoeingManualSystem/AMM,PageBlock,PART1BoeingManualSystem/AMM,AMTOSS(AircraftMaintenanceTask-OrientedSupportSystem)/AMTOSSNumbersTASK29-11-05-400-801-002,PART1BoeingManualSystem/AMM,ATA100ChapterAircraftGeneralGroup/飞机概述05TIMELIMITS/MAINTENANCECHECKS时限/维护检查06DIMENSIONSANDAREAS尺寸和区域07LIFTING&SHORING顶起与支撑08LEVELING&WEIGHING校水平和称重09TOWING&TAXIING牵引和滑行10PARKING,MOORING,STORAGE&RETURNTOSERVICE停放和系留11PLACARDSANDMARKINGS标牌和标记SERVICING勤务AirframeSystemsGroup/飞机机体系统20STANDARDPRACTICES-AIRFRAME标准实施-机身21AIRCONDITIONING空调22AUTOFLIGHT自动飞行23COMMUNICATIONS通讯,PART1BoeingManualSystem/AMM,24ELECTRICALPOWER电源25EQUIPMENT/FURNISHINGS设备/装饰26FIREPROTECTION防火27FLIGHTCONTROLS飞行操纵28FUEL燃油29HYDRAULICPOWER液压30ICEANDRAINPROTECTION防冰和防雨31INDICATING/RECORDINGSYSTEMS指示/记录系统32LANDINGGEAR起落架33LIGHTS灯34NAVIGATION导航35OXYGEN氧气36PNEUMATIC气动系统38WATER/WASTE水/污水46INFORMATIONSYSTEMS信息系统49AIRBORNEAUXILIARYPOWER空运的辅助电源,PART1BoeingManualSystem/AMM,StructureGroup/结构51STANDARDPRACTICESANDSTRUCTURES-GENERAL标准施工与结构简介52DOORS舱门53FUSELAGE机身54NACELLES/PYLONS短舱/吊架55STABILIZERS安定面56WINDOWS窗57WINGS机翼,PART1BoeingManualSystem/AMM,PowerPlantGroup/动力装置70STANDARDPRACTICES-ENGINES标准实施-发动机71POWERPLANT动力装置72ENGINE发动机73ENGINEFUELANDCONTROL发动机燃油和控制74IGNITION点火75AIR空气76ENGINECONTROLS发动机控制器77ENGINEINDICATING发动机指示78EXHAUST排气79OIL滑油80STARTING起动,PART1BoeingManualSystem/AMM,PowerPlantGroup/动力装置70STANDARDPRACTICES-ENGINES标准实施-发动机71POWERPLANT动力装置72ENGINE发动机73ENGINEFUELANDCONTROL发动机燃油和控制74IGNITION点火75AIR空气76ENGINECONTROLS发动机控制器77ENGINEINDICATING发动机指示78EXHAUST排气79OIL滑油80STARTING起动,PART1BoeingManualSystem/AMM,FunctionCode,PART1BoeingManualSystem/AMM,Thesequencenumberisusedtoprovideauniquenumberwhenthefirstfourelementsarenotunique.(a)Thesequencenumberstartsat801fortasksandcontinuesthrough999.Iftherearemorethan200tasks,thenumbercontinueswithA01throughA99,B01throughB99,etc.(b)Thesequencenumberstartsat001forsubtasksandcontinuesthrough799.Theconfigurationnumberisusedtoindicateanengineorpageblockconfiguration.(a)Thefirstpositionistheengineprefix.(b)Thesecondandthirdpositionsarethepageblockconfiguration.(c)IfthepageblockisnotpartoftheenginechaptersordoesnothaveaCONFIGnumber(seeeffectivelyandconfigurationnumbering),thenthetasksandsubtaskswillnothavethiselement.(d)Ifthepageblockisnotpartoftheenginechaptersbutdoeshaveaconfigurationnumber,thenthefirstpositionwillhaveazeroandthelasttwowillindicatetheCONFIGnumber.,PART1BoeingManualSystem/AMM,PART1BoeingManualSystem/IPC,PART1BoeingManualSystem/IPC,如果已知件号，则由数码索引入手：在数码索引中找到此件号，并记下对应的章、节、组件、图和项目号。由图号可找到相应的图解。在图解中找到部件及项目号，并在清单中可找到相应的部件及相关的内容。,如果未知件号，则由目录内容表入手：在预想到的章节中找到内容目录表。参见零件所在的主组。图是按主要名称的字母顺序列出的，找到零件最有可能被显示的图解标题，记下图号。由图解和清单可找到相应的内容。,查找IPC的方法,PART1BoeingManualSystem/IPC,PART1BoeingManualSystem/IPC,PART1BoeingManualSystem/IPC,PART1BoeingManualSystem/IPC,1.FIGURENUMBER-Thefigurenumberidentifiestheillustrationandthepartlistdefiningaspecificportionoftheaircraftcoverage.Thefigurenumberappearsintheillustrationtitle,totheleftofthefirstitemnumberintheFIGUREITEMcolumnatthetopofeachpartslistpage,andinthefootingofeachapplicablepage.2.ITEMNUMBER-Theitemnumbercorrespondstothenumberonthepartintheillustrations.Adash(-)precedingtheitemnumberindicatesthatthepartisnotillustrated.AsnotedintheExplanationofCustomizingdescription,itemnumbersmissingfrompartslistsectionbutfoundontheillustrationarenotapplicable.3.NEXTHIGHERASSEMBLY(NHA)CROSSREFERENCE-Thereferencecataloglocationindicateswheretheusedoncomponentorassemblyisdefined.4.UNITSPERASSEMBLY(UPA)-ThequantityofthepartwhichisusedontheNHAassembly.ThefollowingentriesotherthananumericvaluemaybefoundintheIPCdata:RF(Reference)-IndicatestheitemislistedattheNHAlocationwhichcarriestheUPAquantity.TheNHAlocationisfoundthroughtheNHAcrossreference(See3.).AR(AsRequired)-Indicatesthepartisusedinaquantitydeterminedatthetimewhenthepartisinstalled.,PART1BoeingManualSystem/IPC,5.SUPPLIERCODE-The(5)digitcodewhichidentifiesthemanufacturerofthepart.TheSupplierCodeisfoundinthenomenclaturecolumnfollowingthesupplierpartnumberentry.TheSupplierCodeisextractedfromtheCatalogingHandbookH4/H8,CommercialandGovernmentEntity(CAGE),theNATOSupplyCodeforManufacturers(NSCM),oritisassignedbyBoeingifnotavailablefromtheCAGEorNSCMhandbooks.ThesuppliernameandaddresscorrespondingtoeachSupplierCodeisavailableintheSuppliersNameandAddressIndex.6.SPECIFICATIONNUMBERandQUALIFIEDPARTS-TheSpecificationNumberisaBoeingassignednumberwhichdefinesallofthenecessarypartperformancerequirementsasuppliermustcomplywithtobequalifiedtoproducethepart.TheBoeingSpecificationnumberisdocumentedinthePartNumbercolumnwhennosupplierparthasbeenqualified.WhenasupplierpartqualifiestoaBoeingSpecification,thesupplierpartnumberisshowninthePartNumbercolumnandthespecificationisplacedintheNomenclaturecolumn.Anyadditionalqualifiedsupplierpartsarecapturedasoptionalpartsinthenomenclaturecolumn.7.USEDON-AnoteintheNomenclaturecolumnwhichindicatestheappropriatenexthigherassemblywhenthepartisnotcommontoallofthenexthigherassemblieslistedprecedingthepart.,PART1BoeingManualSystem/IPC,8.FORDETAILSSEE-Areferencetoanotherlocationwheretheinstallationorassemblyisbrokendowninfurtherdetailtoitscomponentparts.9.POSITIONDATA-Extrainformationdefiningwherethepartisinstalled.Typicalinformationpresentedhereincludesstationorzonelocationinformationorphysicalinstalledpositioninformation.10.ALTEREDFROM-Anexistingcomponentthatwasalteredtocreateanotherpartnumber.Thereareonlyminormodificationdifferencesbetweentheoriginal(Alteredfrom)partnumberandthenewpartnumber.11.EFFECTTOFROM-Whereadesignchangeproducesaqualifiedorlimitedinterchangeabilitycondition,thedeliveredeffectivityisshownandanappropriatenoteisincludedinthenomenclaturecolumntodefinethiscondition.Therelationshipbetweenpartsshownininterchangeabilitynotesisdefinedbythefollowingterms:REPLACESORREPLBY-Indicatestheparts(orsets)arephysicallyandfunctionallyinterchangeable.MAYUSE-Indicatesaone-wayinterchangeabilityexists,eitherforwardorbackward,dependingonthepartsinvolved.T/W(togetherwith)-Indicatespartswhicharenecessarytobereplacedalongwiththemainpartforinterchangeability.Interchangeabilityisonlyaccomplishedasspecifiedbythenote.,PART1BoeingManualSystem/IPC,12.ILLUSTRATIONREFERENCE-Areferencenotetothefunctionallyrelatedfigurewhichdefinesthepart(s).ThepartisdrawnatthisfigureinphantomforidentificationofanIllustrationReferencecondition.TubingandductsareexampleusesforThisreference.13.OVERLENGTHPARTNUMBER-ABoeingCompanyReference(BCREF)numberisassignedtoalloverlengthpartnumberswhichexceed15digits.TheBCREFnumberisplacedinthePartcolumnandtheoverlengthnumberisinthenomenclaturecolumn.PNUNASSIGNED-BCREFnumbersarealsoassignedwhenthereisnopartnumberforacomponent.Thisconditionoccursforsupplierorcustomermodificationdata.14.MAINTENANCECOMPONENTSOFASSEMBLIES-DisassemblysequenceofintermediatesubassembliesmaynotbeincludedintheIPCiftheintermediatesubassembliesarenotconsideredlinemaintenancecomponents.TEMPORARYBREAKDOWN-AnotewhichisincludedintheIPCwhenadesignchangeproducesanassemblypartnumberforwhichbreakdowninformationisnotavailable.Breakdowncomponentsforthecurrentassemblyareextendedasaapplicableforthenewassembly.ThetemporarybreakdownnoteisremovedwhenactualbreakdowninformationisavailableandincorporatedintheIPC.,PART1BoeingManualSystem/IPC,15.ATTACHINGPARTS-Attachingpartsarelistedimmediatelyfollowingtheitemwhichtheyattach.TheyareprecededbythephraseAttachingPartsandarefollowedbythesymbol-*-.16.BOEINGSTANDARDPARTS-BoeingStandardPartsareidentifiedbyaBACprefix.TheBoeingStandardPartNumberappearsinthepartnumbercolumnwhennosupplierparthasyetbeenqualified.Whenanequivalentsupplierpartnumberisqualified,itwillappearinthepartnumbercolumnandtheBoeingStandardPartNumberandanyotherequivalentsuppliernumberswillappearinthenomenclaturecolumnasoptionalpartsIfnosupplierpartnumbersareincludedinthePartsListforaBoeingStandard,seetheBoeingStandardsVolumes(D-590),BoeingtoSupplierPartNumberCross-ReferenceIndexorthespecificstandardspageforprocurementsourceinformation.17.CHANGEINDICATORS-Changeindicatorsareappliedoppositethereviseddatalineentry.AnRinthemarginindicatesthelineoppositewasaddedorrevisedinthecurrentrevision.WhenthePartsListpageforafigureincludesAirlineStockNumbers,theletterSisshownoppositethelineentryWhenachangeintheAirlineStockNumberdataistheonlyChangetotheitementry.,PART1BoeingManualSystem/IPC,18.FUNCTIONALIZEDCOVERAGE-CertainitemscontaincomponentswhichareillustratedandlistedinvariouschaptersaccordingtotheirATASpecification100function.Thepresenceofthisconditionisindicatedbyshowingthefigurelocation(s)forthefunctionalizedcoverageintheNOMENCLATUREcolumnofthemajorinstallationorassemblylineentry.Intheexample,theportionoftheDoorInstal-lationcoveringLIGHTSisdisplayedinthefigureidentifiedinChapter33.TheportioncoveringNACELLES/PYLONSisshowninthefigureidentifiedinChapter54.19.BOEINGPROPRIETARYCOLORCODEDPARTS-BoeingProprietaryColorCodedParts,excludingBoeingspecificationpartnumbers10-XXXXX,SXXXNXXX,SXXXTXXX,SXXXUXXX,SXXXWXXXor60BXXXXX,areidentifiedwithanalphaSPsuffix.Thisentryrepresentsconsolidationofallcolorcodesapplicableforthegivenusage.Colorcodedpartsmaybeorderedwitheitherthespecificairline(alpha)colorcodesuffixortheconsolidatedSPsuffix.OrdersreceivedforSPpartswillbeconvertedandprocessedundertheairlines(alpha)colorcodedpartnumber.AreferencetotheappropriateaircraftregistrynumberorthecolornameonordersforSPpartswillfacilitatethecolorconversion.Note:Colorcodedoesnotaffectphysicalorfunctionalinterchangeabilityaspects.20.LOCALFABRICATIONPARTS-MaterialrequirementsforpartswhichcanbelocallyfabricatedareincludedintheNomen-claturecolumnwithina(MFDFROM-)note.,PART1BoeingManualSystem/IPC,21.FIGURETITLE-Wheremorethanoneleadentryorsubjectisincludedinafigure,afiguretitleisusedtofacilitatethepreparationandmaintenanceoftheChapterTableofContentsentries.TheEffectivitycolumnforthefiguretitleidentifiestheaircraftcoveredinthefigure.22.COMPONENTMAINTENANCEMANUALREFERENCE-TheapplicableComponentMaintenanceManualprovidingdetailcoverageofanassemblyisidentifiedina(REFCMM-)noteintheNomenclaturecolumn.ForSupplierAssembliestheapplicablesuppliercodeisshownfollowingthenomenclatureofthepartidentifiedinthePartNumberColumn.23.SERVICEBULLETINENTRIES-BoeingServiceBulletinsareincorporatedintheIPConlyuponnotificationfromtheairlinethattheintentoftheSBhasbeenaccomplished.ServiceBulletincoverageisincorporatedusingoneofthefollowingmethodsasspecifiedbytheairline:DualconfigurationreflectsboththebeforeandafterServiceBulletinincorporationcomponentsinaccordancewithSparesLetterNo.309,Option1.SingleconfigurationreflectsonlytheafterServiceBulletinincorporationcomponentsinaccordancewithSparesLetterNo.309,Option2.ArecordoftheServiceBulletinssubmittedforincorporationintheIPCisshownintheServiceBulletin/ModificationList.,PART1BoeingManualSystem/IPC,24.FILTERMAINTENANCEKITS-Boeingdefinesakitpartnumberwhichcontainsallofthepartsnecessarytosupporttheremovalandmaintenanceofafilterontheairplane.Thekitisaconveniencetotheoperatorandcontainsthefilter/moduleelement(s),packing(s)/O-ring(s),gasketsandallstandardpartsnecessaryformaintainingtheelement.ThefilterMaintenanceKitpartnumberisreferencedinthenomenclaturecolumnoftheelemententry.ThedefinitionoftheFilterMaintenanceKitcontentsaredetailedintheFilterMaintenanceKitsectionoftheIPC.25.ELECTRICALEQUIPMENTNUMBER-TheWiringDiagramequipmentnumbersarereferencedintheIPCnomenclatureasapplicabletoadocumentedpart.ElectricalEquipmentNumbersalsoappearintheIPConplacardsforidentifyingequipment.26.ETOPSENTRIES-TheIPCdefinespartswhicharerequiredtosupportExtendedTwinOperation(ETOPS)fortwo(2)engineaircraft.ETOPSnotesappearinthenomenclaturefieldoftheIPCunderthefollowingconditions:NotApprovedforETOPSMeansthatpartcannotbeinstalledtomeetETOPSflyingrequirements.NotApprovedForETOPSAfterServiceBulletinorServiceLetterIncorporationMeansthatthepartisnotcertifiedforETOPSifthereferencedServiceBulletinorServiceLetterisincorporatedontheairplane.,PART1BoeingManualSystem/IPC,27.MAINTENANCEMANUALREFERENCE-AcrossreferencetotheapplicableBoeingMaintenanceManuallocationwhichcontainstheprocedureforremovalandrepairofthatpart.EXPLANATIONOFILLUSTRATIONTECHNIQUETheillustrationportionofafigureintheIllustratedPartsCatalogpictoriallydisplaystherelationshipofthepartsidentifiedinthePartsList.Thefollowingisanexplanationofcertaintechniquesusedintheillustrationtopresenttherelationshipoftheseparts.Thenumberscorrespondtothoseshowninthefollowingsample.1.Detailcoverageofanyportionoftheillustrationisprovidedbyisolatingsectionsinspecificexplodedviewswithalphabeticdesignations.2.Componentsofassembliesareshowneitherwithinaspecificexplodedviewoftheassemblyortheitemnumbersofthecomponentsareincludedwithinabracketwhichisidentifiedbytheitemnumberoftheassembly.3.Whenacomponentisphysicallyillustratedsuchthataleadlinefromtheitemnumberwithinabrackettotheillus-trationofthepartwouldbeconfusingorindeterminate,anarrowisusedtopointinthedirectionoftheillustratedcomponent.4.Alternateconfigurationareindicatedbyadual-headedarrowrelatingtheillustrationoftheconfigurationinvolved.,PART1BoeingManualSystem/IPC,GENERALSYSTEMOFASSEMBLYORDER-DETAILEDPARTSLIST(DPL)TheindenturesystemusedinthePartsListsofthefiguresincludedwithinthiscatalogshowstherelationshipofoneparttoanother.Foragivenitem,thenumberofindenturesdefinestherelationshipoftheitemtotheassociatedinstallation,nexthigherassembly,orcomponentsoftheitemasfollows:,PART1BoeingManualSystem/WDM,查找WDM的方法：已知EquipmentNumber,WireNumber,根据EquipmentList或WireList索引到相应的电路图。未知EquipmentNumber,WireNumber,则需要设备所属章节，功能在WDM上找到相应的电路图。以WireNumberW0018-0001-22和EquipmentNumberC1434为例。,PART1BoeingManualSystem/WDM,PART1BoeingManualSystem/WDM,PART1BoeingManualSystem/WDM,PART1BoeingManualSystem/WDM,作用：进行系统排故时使用的辅助手册。,PART1BoeingManualSystem/SSM,SWPMStandardWirePracticeManual手册的用途：StandardPracticeProcedureWireMaterialTerminal/SplicePartNumberConnectorConfiguration/RepairContactPartNumberExample:LocatetheWireMaterialforW0018-0001-22andconfigurationforD40576P.,PART1BoeingManualSystem/SWPM,PART1BoeingManualSystem/SWPM,PART1BoeingManualSystem/SWPM,20-CrossReferenceIndex,PART1BoeingManualSystem/SWPM,PART1BoeingManualSystem/SWPM,PART1BoeingManualSystem/FIM,如果有故障码：,由第一个两位数找出对应的章，然后找到故障码索引；由索引可得到相应的条件或措施；如果有说明可能原因，即按要求排故；如果给出参考流程图，即按图索骥；如果故障码是X-字母，即有说明要求参考WDM或SSM。,PART1BoeingManualSystem/FIM,如果无故障码：,有EICAS信息：如果不知道属于哪一章，由EICAS信息入手；如果知道了哪一章，即由该章的信息表入手。,系统测试：找到相应系统的测试索引；由索引可得到相应的章节；在相应的小节内可找到测试步骤。,无EICAS信息，也无系统测试：由故障代码流程图入手。,PART2AirbusManualSystem,AirbusWorld:,PART2AirbusManualSystem,AirNV/Maintenance,PART2AirbusManualSystem,AirNV/MaintenanceAMMMaintenanceProcedure(MP)AMaintenanceProcedureismadeupofTask(s)andSubtasks.EachTaskisbrokendownintothefollowingparagraphs:-Title-ReasonfortheJob-JobSet-UpInformation-JobSet-Up-Procedure-Close-Up(Ifapplicable),PART2AirbusManualSystem,AirNV/MaintenanceAMM(a)TitleItisthetitleoftheTaskfollowedbytheFINNumber(s)ifapplicable.(b)ReasonfortheJobTheparagraphReasonfortheJobisusedtoexplainthereasonforthetask.Thisparagraphcanreferto:-anAirbusMMEL,CDLorMPDtask.NOTE:EachMPDtaskisidentifiedbyaspecificMPDtasknumber.TheMPDtasknumbercomprises9digitsorganizedasfollow:XXXXXX-XX-X(ATAreferenceorZone-sequencenumberidentifier-applicabilityindex).TheMPDapplicabilityindexdigitisnotshownintheAMMtask.-anFAAMMELtask,highlightedby(FAAonly),ifthistaskisnotincludedintheAirbusMMEL.NOTE:Non-FAAoperatorscanusetheAMMtaskrelatedtoanFAAMMELtaskiftheAMMtasksatisfiestheirMELrequirement.,PART2AirbusManualSystem,AirNV/MaintenanceAMMWhentheTasktitleisselfexplanatory,thisparagraphshowsSelfexplanatory(c)JobSet-UpInformationTheparagraphJobSet-UpInformationcancontainthefollowingdata:1Fixtures,Tools,TestandSupportEquipmentTheSpecialToolsandSupportEquipmentrequiredforthemaintenanceoperationsareidentified:-eitherbytheirPartNumberswhentheyarelistedintheIllustratedToolandEquipmentManual(TEM).-orbytheirmainfeatures.-Theusebytheairlineofequivalenttools/equipmentispermittedontheconditionthattheequivalenthasthetechnicalcharacteristicsrequiredtocorrectlyperformthemaintenanceproceduredescribed.Specialproceduresassociatedwiththeusebytheairlinesofequivalenttoolsfallundertheirownresponsibility.-Totalquantityofspecialtoolsforthetasksisindicated.,PART2AirbusManualSystem,2ConsumableMaterialsThistablegivesalistofallthematerialscalledupinthemaintenanceprocedure.TheyarerecordedintheConsumableMaterialList(CML)forgeneraluseonAirframe,inAMM20-34-00forAPU-specificmaterialsandinAMM70-30-00forengine-specificmaterials.ToknowthecharacteristicsoftheconsumablematerialsusedontheAirframe,refertotheCMLavailableinAirNav/AssociatedData.3WorkZonesandAccessPanelsThistablegivesalllocationandaccesspanelinformationrequiredtodothetask.Thezonesareidentifiedbyathree-digitnumericalcode(example:131).Theaccesspanelcodecontainszoneidentificationwithadditionalalphabeticalcharacters(example:131AMG).ZoneinformationisgivenintheAMMFrontMatter.Accesspanelinformationisgiv