常用维修手册及维修文件介绍

ManualandDrawingUsageInstructor ZouLimingZuBiao General ClassificationforManuals CustomizedManual Non CustomizedManual AMMAIPCWDM AWM AWL SSM ASM FIM TSM SRMSWPM ESPM SOPM PMS MPDNTMITEM TEM CML Airbus PART1 BoeingManualSystem MyBoeingFleet PART1 BoeingManualSystem DeltaWebpage PART1 BoeingManualSystem AMM PART1 BoeingManualSystem AMM PageBlock PART1 BoeingManualSystem AMM AMTOSS AircraftMaintenanceTask OrientedSupportSystem AMTOSSNumbersTASK29 11 05 400 801 002 PART1 BoeingManualSystem 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 PART1 BoeingManualSystem 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 PART1 BoeingManualSystem 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 PART1 BoeingManualSystem 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 PART1 BoeingManualSystem 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 PART1 BoeingManualSystem AMM FunctionCode PART1 BoeingManualSystem AMM Thesequencenumberisusedtoprovideauniquenumberwhenthefirstfourelementsarenotunique a Thesequencenumberstartsat801fortasksandcontinuesthrough999 Iftherearemorethan200tasks thenumbercontinueswithA01throughA99 B01throughB99 etc b Thesequencenumberstartsat001forsubtasksandcontinuesthrough799 Theconfigurationnumberisusedtoindicateanengineorpageblockconfiguration a Thefirstpositionistheengineprefix b Thesecondandthirdpositionsarethepageblockconfiguration c IfthepageblockisnotpartoftheenginechaptersordoesnothaveaCONFIGnumber seeeffectivelyandconfigurationnumbering thenthetasksandsubtaskswillnothavethiselement d Ifthepageblockisnotpartoftheenginechaptersbutdoeshaveaconfigurationnumber thenthefirstpositionwillhaveazeroandthelasttwowillindicatetheCONFIGnumber PART1 BoeingManualSystem AMM PART1 BoeingManualSystem IPC PART1 BoeingManualSystem 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 PART1 BoeingManualSystem IPC PART1 BoeingManualSystem IPC PART1 BoeingManualSystem IPC PART1 BoeingManualSystem IPC 1 FIGURENUMBER Thefigurenumberidentifiestheillustrationandthepartlistdefiningaspecificportionoftheaircraftcoverage Thefigurenumberappearsintheillustrationtitle totheleftofthefirstitemnumberintheFIGUREITEMcolumnatthetopofeachpartslistpage andinthefootingofeachapplicablepage 2 ITEMNUMBER Theitemnumbercorrespondstothenumberonthepartintheillustrations Adash precedingtheitemnumberindicatesthatthepartisnotillustrated Asnotedinthe ExplanationofCustomizing description itemnumbersmissingfrompartslistsectionbutfoundontheillustrationarenotapplicable 3 NEXTHIGHERASSEMBLY NHA CROSSREFERENCE Thereferencecataloglocationindicateswheretheusedoncomponentorassemblyisdefined 4 UNITSPERASSEMBLY UPA ThequantityofthepartwhichisusedontheNHAassembly ThefollowingentriesotherthananumericvaluemaybefoundintheIPCdata RF Reference IndicatestheitemislistedattheNHAlocationwhichcarriestheUPAquantity TheNHAlocationisfoundthroughtheNHAcrossreference See3 AR AsRequired Indicatesthepartisusedinaquantitydeterminedatthetimewhenthepartisinstalled PART1 BoeingManualSystem IPC 5 SUPPLIERCODE The 5 digitcodewhichidentifiesthemanufacturerofthepart TheSupplierCodeisfoundinthenomenclaturecolumnfollowingthesupplierpartnumberentry TheSupplierCodeisextractedfromthe CatalogingHandbookH4 H8 CommercialandGovernmentEntity CAGE theNATOSupplyCodeforManufacturers NSCM oritisassignedbyBoeingifnotavailablefromtheCAGEorNSCMhandbooks ThesuppliernameandaddresscorrespondingtoeachSupplierCodeisavailableintheSuppliersNameandAddressIndex 6 SPECIFICATIONNUMBERandQUALIFIEDPARTS TheSpecificationNumberisaBoeingassignednumberwhichdefinesallofthenecessarypartperformancerequirementsasuppliermustcomplywithtobequalifiedtoproducethepart TheBoeingSpecificationnumberisdocumentedinthePartNumbercolumnwhennosupplierparthasbeenqualified WhenasupplierpartqualifiestoaBoeingSpecification thesupplierpartnumberisshowninthePartNumbercolumnandthespecificationisplacedintheNomenclaturecolumn Anyadditionalqualifiedsupplierpartsarecapturedasoptionalpartsinthenomenclaturecolumn 7 USEDON AnoteintheNomenclaturecolumnwhichindicatestheappropriatenexthigherassemblywhenthepartisnotcommontoallofthenexthigherassemblieslistedprecedingthepart PART1 BoeingManualSystem 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 PART1 BoeingManualSystem IPC 12 ILLUSTRATIONREFERENCE Areferencenotetothefunctionallyrelatedfigurewhichdefinesthepart s ThepartisdrawnatthisfigureinphantomforidentificationofanIllustrationReferencecondition TubingandductsareexampleusesforThisreference 13 OVERLENGTHPARTNUMBER ABoeingCompanyReference BCREF numberisassignedtoalloverlengthpartnumberswhichexceed15digits TheBCREFnumberisplacedinthePartcolumnandtheoverlengthnumberisinthenomenclaturecolumn PNUNASSIGNED BCREFnumbersarealsoassignedwhenthereisnopartnumberforacomponent Thisconditionoccursforsupplierorcustomermodificationdata 14 MAINTENANCECOMPONENTSOFASSEMBLIES DisassemblysequenceofintermediatesubassembliesmaynotbeincludedintheIPCiftheintermediatesubassembliesarenotconsideredlinemaintenancecomponents TEMPORARYBREAKDOWN AnotewhichisincludedintheIPCwhenadesignchangeproducesanassemblypartnumberforwhichbreakdowninformationisnotavailable Breakdowncomponentsforthecurrentassemblyareextendedasaapplicableforthenewassembly ThetemporarybreakdownnoteisremovedwhenactualbreakdowninformationisavailableandincorporatedintheIPC PART1 BoeingManualSystem IPC 15 ATTACHINGPARTS Attachingpartsarelistedimmediatelyfollowingtheitemwhichtheyattach Theyareprecededbythephrase AttachingParts andarefollowedbythesymbol 16 BOEINGSTANDARDPARTS BoeingStandardPartsareidentifiedbyaBACprefix TheBoeingStandardPartNumberappearsinthepartnumbercolumnwhennosupplierparthasyetbeenqualified Whenanequivalentsupplierpartnumberisqualified itwillappearinthepartnumbercolumnandtheBoeingStandardPartNumberandanyotherequivalentsuppliernumberswillappearinthenomenclaturecolumnasoptionalpartsIfnosupplierpartnumbersareincludedinthePartsListforaBoeingStandard seetheBoeingStandardsVolumes D 590 BoeingtoSupplierPartNumberCross ReferenceIndexorthespecificstandardspageforprocurementsourceinformation 17 CHANGEINDICATORS Changeindicatorsareappliedoppositethereviseddatalineentry An R inthemarginindicatesthelineoppositewasaddedorrevisedinthecurrentrevision WhenthePartsListpageforafigureincludesAirlineStockNumbers theletter S isshownoppositethelineentryWhenachangeintheAirlineStockNumberdataistheonlyChangetotheitementry PART1 BoeingManualSystem IPC 18 FUNCTIONALIZEDCOVERAGE CertainitemscontaincomponentswhichareillustratedandlistedinvariouschaptersaccordingtotheirATASpecification100function Thepresenceofthisconditionisindicatedbyshowingthefigurelocation s forthefunctionalizedcoverageintheNOMENCLATUREcolumnofthemajorinstallationorassemblylineentry Intheexample theportionoftheDoorInstal lationcoveringLIGHTSisdisplayedinthefigureidentifiedinChapter33 TheportioncoveringNACELLES PYLONSisshowninthefigureidentifiedinChapter54 19 BOEINGPROPRIETARYCOLORCODEDPARTS BoeingProprietaryColorCodedParts excludingBoeingspecificationpartnumbers10 XXXXX SXXXNXXX SXXXTXXX SXXXUXXX SXXXWXXXor60BXXXXX areidentifiedwithanalpha SP suffix Thisentryrepresentsconsolidationofallcolorcodesapplicableforthegivenusage Colorcodedpartsmaybeorderedwitheitherthespecificairline alpha colorcodesuffixortheconsolidated SP suffix Ordersreceivedfor SP partswillbeconvertedandprocessedundertheairlines alpha colorcodedpartnumber Areferencetotheappropriateaircraftregistrynumberorthecolornameonordersfor SP partswillfacilitatethecolorconversion Note Colorcodedoesnotaffectphysicalorfunctionalinterchangeabilityaspects 20 LOCALFABRICATIONPARTS MaterialrequirementsforpartswhichcanbelocallyfabricatedareincludedintheNomen claturecolumnwithina MFDFROM note PART1 BoeingManualSystem IPC 21 FIGURETITLE Wheremorethanoneleadentryorsubjectisincludedinafigure afiguretitleisusedtofacilitatethepreparationandmaintenanceoftheChapterTableofContentsentries TheEffectivitycolumnforthefiguretitleidentifiestheaircraftcoveredinthefigure 22 COMPONENTMAINTENANCEMANUALREFERENCE TheapplicableComponentMaintenanceManualprovidingdetailcoverageofanassemblyisidentifiedina REFCMM noteintheNomenclaturecolumn ForSupplierAssembliestheapplicablesuppliercodeisshownfollowingthenomenclatureofthepartidentifiedinthePartNumberColumn 23 SERVICEBULLETINENTRIES BoeingServiceBulletinsareincorporatedintheIPConlyuponnotificationfromtheairlinethattheintentoftheSBhasbeenaccomplished ServiceBulletincoverageisincorporatedusingoneofthefollowingmethodsasspecifiedbytheairline Dualconfigurationreflectsboththe beforeandafter ServiceBulletinincorporationcomponentsinaccordancewithSparesLetterNo 309 Option1 Singleconfigurationreflectsonlythe after ServiceBulletinincorporationcomponentsinaccordancewithSparesLetterNo 309 Option2 ArecordoftheServiceBulletinssubmittedforincorporationintheIPCisshownintheServiceBulletin ModificationList PART1 BoeingManualSystem 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 NotApprovedforETOPS MeansthatpartcannotbeinstalledtomeetETOPSflyingrequirements NotApprovedForETOPSAfterServiceBulletinorServiceLetterIncorporation MeansthatthepartisnotcertifiedforETOPSifthereferencedServiceBulletinorServiceLetterisincorporatedontheairplane PART1 BoeingManualSystem IPC 27 MAINTENANCEMANUALREFERENCE AcrossreferencetotheapplicableBoeingMaintenanceManuallocationwhichcontainstheprocedureforremovalandrepairofthatpart EXPLANATIONOFILLUSTRATIONTECHNIQUETheillustrationportionofafigureintheIllustratedPartsCatalogpictoriallydisplaystherelationshipofthepartsidentifiedinthePartsList Thefollowingisanexplanationofcertaintechniquesusedintheillustrationtopresenttherelationshipoftheseparts Thenumberscorrespondtothoseshowninthefollowingsample 1 Detailcoverageofanyportionoftheillustrationisprovidedbyisolatingsectionsinspecificexplodedviewswithalphabeticdesignations 2 Componentsofassembliesareshowneitherwithinaspecificexplodedviewoftheassemblyortheitemnumbersofthecomponentsareincludedwithinabracketwhichisidentifiedbytheitemnumberoftheassembly 3 Whenacomponentisphysicallyillustratedsuchthataleadlinefromtheitemnumberwithinabrackettotheillus trationofthepartwouldbeconfusingorindeterminate anarrowisusedtopointinthedirectionoftheillustratedcomponent 4 Alternateconfigurationareindicatedbyadual headedarrowrelatingtheillustrationoftheconfigurationinvolved PART1 BoeingManualSystem IPC GENERALSYSTEMOFASSEMBLYORDER DETAILEDPARTSLIST DPL TheindenturesystemusedinthePartsListsofthefiguresincludedwithinthiscatalogshowstherelationshipofoneparttoanother Foragivenitem thenumberofindenturesdefinestherelationshipoftheitemtotheassociatedinstallation nexthigherassembly orcomponentsoftheitemasfollows PART1 BoeingManualSystem 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 PART1 BoeingManualSystem WDM PART1 BoeingManualSystem WDM PART1 BoeingManualSystem WDM PART1 BoeingManualSystem WDM 作用 进行系统排故时使用的辅助手册 PART1 BoeingManualSystem SSM SWPM StandardWirePracticeManual手册的用途 StandardPracticeProcedureWireMaterialTerminal SplicePartNumberConnectorConfiguration RepairContactPartNumberExample LocatetheWireMaterialforW0018 0001 22andconfigurationforD40576P PART1 BoeingManualSystem SWPM PART1 BoeingManualSystem SWPM PART1 BoeingManualSystem SWPM 20 CrossReferenceIndex PART1 BoeingManualSystem SWPM PART1 BoeingManualSystem SWPM PART1 BoeingManualSystem 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 PART1 BoeingManualSystem 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 PART2 AirbusManualSystem AirbusWorld PART2 AirbusManualSystem AirN V Maintenance PART2 AirbusManualSystem AirN V Maintenance AMMMaintenanceProcedure MP AMaintenanceProcedureismadeupofTask s andSubtasks EachTaskisbrokendownintothefollowingparagraphs Title ReasonfortheJob JobSet UpInformation JobSet Up Procedure Close Up Ifapplicable PART2 AirbusManualSystem AirN V Maintenance AMM a TitleItisthetitleoftheTaskfollowedbytheFINNumber s ifapplicable b ReasonfortheJobTheparagraph ReasonfortheJob isusedtoexplainthereasonforthetask Thisparagraphcanreferto anAirbusMMEL CDLorMPDtask NOTE EachMPDtaskisidentifiedbyaspecificMPDtasknumber TheMPDtasknumbercomprises9digitsorganizedasfollow XXXXXX XX X ATAreferenceorZone sequencenumberidentifier applicabilityindex TheMPDapplicabilityindexdigitisnotshownintheAMMtask anFAAMMELtask highlightedby FAAonly ifthistaskisnotincludedintheAirbusMMEL NOTE Non FAAoperatorscanusetheAMMtaskrelatedtoanFAAMMELtaskiftheAMMtasksatisfiestheirMELrequirement PART2 AirbusManualSystem AirN V Maintenance AMMWhentheTasktitleisselfexplanatory thisparagraphshows Selfexplanatory c JobSet UpInformationTheparagraph JobSet UpInformation cancontainthefollowingdata 1Fixtures Tools TestandSupportEquipmentTheSpecialToolsandSupportEquipmentrequiredforthemaintenanceoperationsareidentified eitherbytheirPartNumberswhentheyarelistedintheIllustratedToolandEquipmentManual TEM orbytheirmainfeatures Theusebytheairlineofequivalenttools equipmentispermittedontheconditionthattheequivalenthasthetechnicalcharacteristicsrequiredtocorrectlyperformthemaintenanceproceduredescribed Specialproceduresassociatedwiththeusebytheairlinesof equivalent toolsfallundertheirownresponsibility Totalquantityofspecialtoolsforthetasksisindicated PART2 AirbusManualSystem 2ConsumableMaterialsThistablegivesalistofallthematerialscalledupinthemaintenanceprocedure TheyarerecordedintheConsumableMaterialList CML forgeneraluseonAirframe inAMM20 34 00forAPU specificmaterialsandinAMM70 30 00forengine specificmaterials ToknowthecharacteristicsoftheconsumablematerialsusedontheAirframe refertotheCMLavailableinAirNav AssociatedData 3WorkZonesandAccessPanelsThistablegivesalllocationandaccesspanelinformationrequiredtodothetask Thezonesareidentifiedbyathree digitnumericalcode example 131 Theaccesspanelcodecontainszoneidentificationwithadditionalalphabeticalcharacters example 131AMG ZoneinformationisgivenintheAMMFrontMatter Accesspanelinfo