常用維修手冊及維修文件介紹ppt課件

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/飛機概述05TIMELIMITS/MAINTENANCECHECKS時限/維護檢查06DIMENSIONSANDAREAS尺寸和區(qū)域07LIFTING&SHORING頂起與支撐08LEVELING&WEIGHING校水平和稱重09TOWING&TAXIING牽引和滑行10PARKING,MOORING,STORAGE&RETURNTOSERVICE停放和系留11PLACARDSANDMARKINGS標(biāo)牌和標(biāo)記SERVICING勤務(wù)AirframeSystemsGroup/飛機機體系統(tǒng)20STANDARDPRACTICES-AIRFRAME標(biāo)準(zhǔn)實施-機身21AIRCONDITIONING空調(diào)22AUTOFLIGHT自動飛行23COMMUNICATIONS通訊,PART1BoeingManualSystem/AMM,24ELECTRICALPOWER電源25EQUIPMENT/FURNISHINGS設(shè)備/裝飾26FIREPROTECTION防火27FLIGHTCONTROLS飛行操縱28FUEL燃油29HYDRAULICPOWER液壓30ICEANDRAINPROTECTION防冰和防雨31INDICATING/RECORDINGSYSTEMS指示/記錄系統(tǒng)32LANDINGGEAR起落架33LIGHTS燈34NAVIGATION導(dǎo)航35OXYGEN氧氣36PNEUMATIC氣動系統(tǒng)38WATER/WASTE水/污水46INFORMATIONSYSTEMS信息系統(tǒng)49AIRBORNEAUXILIARYPOWER空運的輔助電源,PART1BoeingManualSystem/AMM,StructureGroup/結(jié)構(gòu)51STANDARDPRACTICESANDSTRUCTURES-GENERAL標(biāo)準(zhǔn)施工與結(jié)構(gòu)簡介52DOORS艙門53FUSELAGE機身54NACELLES/PYLONS短艙/吊架55STABILIZERS安定面56WINDOWS窗57WINGS機翼,PART1BoeingManualSystem/AMM,PowerPlantGroup/動力裝置70STANDARDPRACTICES-ENGINES標(biāo)準(zhǔn)實施-發(fā)動機71POWERPLANT動力裝置72ENGINE發(fā)動機73ENGINEFUELANDCONTROL發(fā)動機燃油和控制74IGNITION點火75AIR空氣76ENGINECONTROLS發(fā)動機控制器77ENGINEINDICATING發(fā)動機指示78EXHAUST排氣79OIL滑油80STARTING起動,PART1BoeingManualSystem/AMM,PowerPlantGroup/動力裝置70STANDARDPRACTICES-ENGINES標(biāo)準(zhǔn)實施-發(fā)動機71POWERPLANT動力裝置72ENGINE發(fā)動機73ENGINEFUELANDCONTROL發(fā)動機燃油和控制74IGNITION點火75AIR空氣76ENGINECONTROLS發(fā)動機控制器77ENGINEINDICATING發(fā)動機指示78EXHAUST排氣79OIL滑油80STARTING起動,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,如果已知件號，則由數(shù)碼索引入手：在數(shù)碼索引中找到此件號，并記下對應(yīng)的章、節(jié)、組件、圖和項目號。由圖號可找到相應(yīng)的圖解。在圖解中找到部件及項目號，并在清單中可找到相應(yīng)的部件及相關(guān)的內(nèi)容。,如果未知件號，則由目錄內(nèi)容表入手：在預(yù)想到的章節(jié)中找到內(nèi)容目錄表。參見零件所在的主組。圖是按主要名稱的字母順序列出的，找到零件最有可能被顯示的圖解標(biāo)題，記下圖號。由圖解和清單可找到相應(yīng)的內(nèi)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,根據(jù)EquipmentList或WireList索引到相應(yīng)的電路圖。未知EquipmentNumber,WireNumber,則需要設(shè)備所屬章節(jié)，功能在WDM上找到相應(yīng)的電路圖。以WireNumberW0018-0001-22和EquipmentNumberC1434為例。,PART1BoeingManualSystem/WDM,PART1BoeingManualSystem/WDM,PART1BoeingManualSystem/WDM,PART1BoeingManualSystem/WDM,作用：進行系統(tǒng)排故時使用的輔助手冊。,PART1BoeingManualSystem/SSM,SWPMStandardWirePracticeManual手冊的用途：StandardPracticeProcedureWireMaterialTerminal/SplicePartNumberConnectorConfiguration/RepairContactPartNumberExample:LocatetheWireMaterialforW0018-0001-22andconfigurationforD40576P.,PART1BoeingManualSystem/SWPM,PART1BoeingManualSystem/SWPM,PART1BoeingManualSystem/SWPM,20-CrossReferenceIndex,PART1BoeingManualSystem/SWPM,PART1BoeingManualSystem/SWPM,PART1BoeingManualSystem/FIM,如果有故障碼：,由第一個兩位數(shù)找出對應(yīng)的章，然后找到故障碼索引；由索引可得到相應(yīng)的條件或措施；如果有說明可能原因，即按要求排故；如果給出參考流程圖，即按圖索驥；如果故障碼是X-字母，即有說明要求參考WDM或SSM。,PART1BoeingManualSystem/FIM,如果無故障碼：,有EICAS信息：如果不知道屬于哪一章，由EICAS信息入手；如果知道了哪一章，即由該章的信息表入手。,系統(tǒng)測試：找到相應(yīng)系統(tǒng)的測試索引；由索引可得到相應(yīng)的章節(jié)；在相應(yīng)的小節(jié)內(nèi)可找到測試步驟。,無EICAS信息，也無系統(tǒng)測試：由故障代碼流程圖入手。,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.AccesspanelinformationisgiveninAMMChapter6.,PART2AirbusManualSyste