工包航空股份工程技术维修管理部编制

第3任务号/TASKNO:不指 塞不指 按 安全护不指 按 跳开关不指 按 警告 力矩扳手:0.67至13.50m.daN(4.94至99.57lbf.ft) GAGE-GO/NO Fixtures,Tools,TestandSupport Nospecific GAGE-SET,FEELERNospecific SAFETYBARRIER(S)No SAFETYCLIP-CIRCUITNo WARNINGNospecific Torquewrench:rangetobetween0.67and13.50m.daN(4.94and99.57lbf.ft) GAGE-GO/NOGO LOCKINGTOOL-FLAPSLATLEVER,INT.参 说11- 15- 19- 19- 0.8MMDIA不锈钢B.Consumable CLEANINGAGENTSSOLVENTGENERALPURPOSE15- STORAGECORROSIONPREVENTIVECOMPOUND,19- LINT-COTTON19- LOCKWIRESTAINLSSSTLANNEALED0.8MMC. 说 IPC- 第4任务号/TASKNO: 开口 51-05-01-C.Expendable IPC- cotter 51-05-01-D.参 说 SYSTEMREPORT/TESTF/CTLFlapInterconnectingStrut-Inspection/CheckSHEET1FlapInterconnectingStrut-RadialySHEET1D.Referenced RemovaloftheFlap/SlatControl-LeverLocking InstallationoftheFlap/SlatControl-LeverTool ExtensionoftheFlapsonthe27-50-00-866-008-A-01ExtensionoftheFlaps/SlatsontheGround RetractionoftheFlapsontheGround27-50-00-866-009-A-01RetractionoftheFlaps/Slatsonthe OperationalTestoftheFlapInterconnectingandtheFlap-AttaentFailure-DetectionSensors TodoaCheckoftheFlapRiggedPosition(withtheSharks RecementoftheFlapInterconnectingStrutRod-andLocking OperationalTestoftheFlap 第5任务号/TASKNO: RemovaloftheFlapKink-SealsandCushion- InstallationoftheFlapKink-SealsandCushion-Seals ProceduretoGetAccesstotheSYSTEMREPORT/TESTF/CTLFlapInterconnectingStrut-Inspection/CheckSHEET1FlapInterconnectingStrut-RadialySHEET13机电工作准备JobSet-(Ref.Fig.FlapInterconnectingStrut-Inspection/CheckSHEETA.Subtask27-51-44-941-058-AA.SafetyPutthesafetybarriersinPutaWARNINGNOTICE(S)inpositiontolsnottooperatetheflapcontrols.27-51-44-860-059-B.飞机状(参考.AMM.TASK27-00-00-480-002)(参考.AMM.27-54-61-000-(参考.AMM.TASK27-00-00-080-002)。AMM.TASK.27-50-00-866-(参考.AMM.TASK27-00-00-480-002).Subtask27-51-44-860-059-B.AircraftMaintenanceWARNING:MAKESURETHATTHETRAVELRANGESOFTHEFLIGHTCONTROLSURFACESARECLEARBEFOREYOUPRESSURIZE/DEPRESSURIZEAHYDRAULICSYSTEM.Extendtheflapstoposition1(Ref.AMMTASK27-50-00-866-008)MakesurethattheLOCKINGTOOL-FLAPSLATLEVER,INT.(98D27803000000)isinstalledontheflap/slatcontrollever(Ref.AMMTASK27-00-00-480-002).Removetheapplicableupperandlowerkink-seals(1)and(2)from 第6任务号/TASKNO:inboardandtheoutboardflaps(Ref.AMMTASK27-54-61-000-002)RemovetheLOCKINGTOOL-FLAPSLATLEVER,INT.POSITIONfromtheflap/slatcontrollever(Ref.AMMTASK27-00-00-080-002)Fullyextendtheflaps(Ref.AMMTASK27-50-00-866-008)MakesurethattheLOCKINGTOOL-FLAPSLATLEVER,INT.(98D27803000000)isinstalledontheflap/slatcontrollever(Ref.AMMTASK27-00-00-480-002).27-51-44-865-068-Subtask27-51-44-865-068-C.Open,safetyandtagthis(these)circuit面板名 识 位PANEL IDENT.49VUFLIGHTCONTROLS/FLP/CTLAND 121VUFLIGHTCONTROLS/FLP/CTL 27-51-44-020-054-D.(Ref.Fig.FlapInterconnectingStrut-Inspection/CheckSHEETSubtask27-51-44-020-054-D.Preparationfor(Ref.Fig.FlapInterconnectingStrut-Inspection/CheckSHEETWARNING:OBEYTHEMANUFACTURER′SINSTRUCTIONSWHENYOUTHIS/THESEUSEPROTECTIVECLOTHING,RUBBERGLOVES,GOGGLESANDAUseaMaterialNo.19-003*(LINT-COTTONCLOTH)mademoistwithMaterialNo.11-026*(CLEANINGAGENTS)tocleantheflapinterconnectingstrutandtheflapattaentbrackets(5)and(8).Removeanddiscardthecotterpin 第7任务号/TASKNO:Removethenut(15),thewasher(13)andtheboltDisconnecttheflapinterconnectingstrutfromtheattaentbracketPulltheactuatingrodoutoftheflapinterconnectingstrutuntilittouchestheinternallimit.CAUTION:BECAREFULWHENYOUDOMAINTENANCETASKSONTHEWINGTRAILINGDONOTCAUSEDAMAGETOTHEELECTRICALCABLEDONOTCAUSEDAMAGETOTHEELECTRICALCABLEMAKESURETHATTHEELECTRICALCABLESAREINSTALLEDCORRECTLY.INCORRECTINSTALLATIONCANCAUSEDAMAGE.4机电工作步骤(Ref.Fig.FlapInterconnectingStrut-Inspection/CheckSHEET**27-51-44-210-053-A.(参见.图.FlapInterconnectingStrut-RadialySHEET1 连接杆端头或磨损或损伤锁定装置(参见.AMM.任务27-51-44-960-001). 第8任务号/TASKNO: (参见.AMM.27-51-00-710-(Ref.Fig.FlapInterconnectingStrut-Inspection/CheckSHEET**ONA/CSubtask27-51-44-210-053-A.InspectionoftheInterconnectingStrutandAtta (Ref.Fig.FlapInterconnectingStrut-RadialDoaninspectionoftheactuatingrodfordamageandDoaninspectionoftheflapinterconnecting-strutinternalstructure,throughtheinspectionholes(7),fordamageandcorrosion.Doaninspectionoftheflapinterconnectingstrutdamagedpaintandcorrectconditionoftheelectricalplugscorrectconditionoftheelectricalcablescorrectconditionofallthefastenersoftheattaentbrackets(5)and(8)correctconditionofallthesafety-correctconditionofthebearingsoftheflapinterconnectingstrut,asfarasispossiblecorrectconditionofthebolts(6)and(16)asfarasisMakesurethattherod-end(9)orlockingdevice(11)isnotwornordamaged.Receawornordamagedrod-end,orawornordamagedlockingdevice(Ref.AMMTASK27-51-44-960-001).Makesurethattheword′TOP′ontheflapinterconnectingstrutisatthetop.Doacheckoftheradialyoftheactuatingrodoftheinterconnectinstrutasfollows:MakesurethattheactuatingrodisfullyMakesurethattheactuatingrodismoveduntilspaceYisclosedontheothersideoftheforwardbush.UseaGAGE-SET,FEELERandmeasurethedimensionX(betweentheactuatingrodandtheforwardbush)intwodifferentpointsofthecircumference,inthehorizontalandverticalnes.MakesurethatthedimensionXisnotmorethan0.4mm(0.0157in.).IfthedimensionXismorethan0.4mm(0.0157in.)theinterconnectingstrutmustbere 第9任务号/TASKNO:(7)Doanoperationaltestoftheflapinterconnectingstrutandtheflap-attaentfailure-detectionsensors(Ref.AMMTASK27-51-00-710-002)5机电结束 Close(参见.图.FlapInterconnectingStrut-RadialySHEET(Ref.Fig.FlapInterconnectingStrut-Inspection/CheckSHEET**27-51-44-420-056-注意：通过检查/设置孔和作动杆上的凹槽安装GO/NOGOGAGE检查/设置孔和作动杆上的凹槽能完全对齐。当襟翼操作后，由于襟翼间隙，GO/NOGOGAGE状态良好，如果GO/NOGOGAGE能被安装，则内联接支柱正确到位。如不能，在检查/设置孔安装GAGEGO/NOGO(98D27504008000)。如果1GAGEGO/NOGO(98D275040080002(15)，垫片(13),螺栓(16通过已给的Para5.B对内联接支柱进行调节。1GAGEGO/NO215),力矩在1.1至1.7m.daN(97.35至150.443IPC-CSN(27-51-05-01-100)新的开口销(14Subtask27-51-44-420-056-A.ConnectionoftheInterconnectingStruttotheFlapAttaent(1)Pushtheactuatingrodintotheflapinterconnectingstrutuntilittouchestheinternallimit. 第10任务号/TASKNO:PuttheinterconnectingstrutinpositionintheattaentbracketInstallthebolt(16),thewasher(13)andthenutMakesurethattheinterconnectingstrutiscorrectlysetasRetracttheflapstoposition1(Ref.TASK27-50-00-866-NOTE:TheGO/NOGOGAGEisinstalledthroughtheinspection/settingholeandagrooveintheactuatingrod.Whenthestrutissetduringitsinitialinstallationtheinspection/settingholeandthegroovealignfully.Afterflapoperation,becauseoftheflaptolerances,theinspection/settingholeandtheactuatingrodgroovewillnotfullyalign.ThisispermittedifthecheckwiththeGO/NOGAGEissatisfactory.IftheGO/NOGOGAGEcanbeinstalled,theinterconnectingstrutiscorrectlyset.Ifnot,thestrutisincorrectlysetandmustbeadjusted.NOTE:Theinterconnectingstrutcanhaveoneortwoinspection/settingholes.Iftherearetwo,usetheholethatisnotblockedbytheaircraftstructure.InstalltheGAGE-GO/NOGO(98D27504008000)intheinspection/settinghole.Thestrutiscorrectlysetifthegagegoesfullyintotheinspection/settinghole.Ifthegagedoesnotgofullyintotheinspection/settingRemovetheGAGE-GO/NORemovethenut(15),thewasher(13),andtheboltDisconnectthetheinterconnectingstrutfromtheattaentbracketDotheadjustmentoftheinterconnectingstrutgiveninPara_IfnoadjustmentoftheinterconnectingstrutisRemovetheGAGE-GO/NOTORQUEthenut(15)tobetween1.1and1.7m.daN(97.35and150.44InstallanewIPC-CSN(27-51-05-01-100)cotterpin(5)Makesurethattheworkareaiscleanandclearoftool(s)andother**ONA/C001-049,051-099,101-149,151-199,201-249,251-299,351-511-550,651-27-51-44-820-054-B.（如需要 第11任务号/TASKNO:(如上锁螺帽(10)松动，拧紧它，力矩在5.1至5.9m.daN(37.61至43.51lbf.ft)。-螺帽-垫片-开口销**ONA/C001-049,051-099,101-149,151-199,201-249,251-299,351-511-550,651-Subtask27-51-44-820-054-B.AdjustmentoftheInterconnectingStrut(ifInstallthePIN-SETTING(98D27504031000)intheinspection/settingholeintheinterconnectingstrut.NOTE:Theinterconnectingstrutcanhaveoneortwoinspection/settingholes.Iftherearetwo,usetheholethatisnotblockedbytheaircraftIfnecessary,adjusttheactuatingrodoftheinterconnectingstrutsothatyoucaninstallthePIN-SETTING(98D27504031000)asfollows:Aligntherod-end(9)withtheflapuntilyoucaninstallthebolt(16).WARNING:USEPROTECTIVEGOGGLESANDGLOVESWHENYOUREMOVEORINSTALLLOCKWIRE.EACHTIMEYOUCUTLOCKWIREDURINGTHETASK,REMOVEANDDISCARDIT.LOOSELOCKWIRECANCUTYOUORMAKEYOUBLIND.Ifnecessary,removeanddiscardthelockwirefromtheLoosenthelocknutAdjustthenut(12)untilyoucaninstallthePIN- 第12任务号/TASKNO:(98D27504031000)Makesurethatyoucanseethethreadsoftherod-end(9)throughthecheckhole.Ifyoucannotseethethreadsoftherod-end(9)throughthecheckhole,checktheflaprigging(Ref.TASK27-51-00-820-003).TightenthelocknutInstallthewasher(13)andthenutTorquethenut(15)tobetween1.1and1.7m.daN(97.35and150.44NOTE:Itispossibletohaveaclearancebetweenthebushandthestrutattaentbracket.InstallanewIPC-CSN(27-51-05-01-100)cotterpin(14)Ifyouloosenedthelocknut(10),TORQUEittobetween5.1and5.9m.daN(37.61and43.51lbf.ft).WARNING:WEARGOGGLESWHENYOUREMOVEORINSTALLTHELOCKWIRE.CUT,REMOVEANDDISCARDTHELOCKWIREASYOUDOTHETASK.LOOSELOCKWIRECANCUTORBLINDYOU.Safetythelocknut(10)withMaterialNo.19-010*(LOCKWIRESTAINLSSSTLANNEALED0.8MMDIA).RemovethePIN-SETTING(98D27504031000)fromtheinspection/settingholeintheinterconnectingstrut.WARNING:OBEYTHEMANUFACTURER′SINSTRUCTIONSWHENYOUTHIS/THESEMATERIAL/S.USEPROTECTIVECLOTHINGANDRUBBERApplyalayerofMaterialNo.15-007*(STORAGEPRESERVATION)theheadoftheboltthenutthewasherthecotterpin**301-350,551-27-51-44-820-054-B.（如需要拧紧螺帽(15),力矩在1.1至1.7m.daN(97.35至150.44 第13任务号/TASKNO:如果松动过上锁螺帽(10)，拧紧它，力矩在5.1至5.9m.daN(37.61至43.51lbf.ft)。-螺帽-垫片-开口销**ONA/C301-350,551-650B.AdjustmentoftheInterconnectingStrut(ifInstallthePIN-SETTING(98D27504031000)intheinspection/settingholeintheinterconnectingstrut.NOTE:Theinterconnectingstrutcanhaveoneortwoinspection/settingholes.Iftherearetwo,usetheholethatisnotblockedbytheaircraftstructure.Ifnecessary,adjusttheactuatingrodoftheinterconnectingstrutsothatyoucaninstallthePIN-SETTING(98D27504031000)asfollows:Aligntherod-end(9)withtheflapuntilyoucaninstallthebolt(16).WARNING:USEPROTECTIVEGOGGLESANDGLOVESWHENYOUREMOVEORINSTALLLOCKWIRE.EACHTIMEYOUCUTLOCKWIREDURINGTHETASK,REMOVEANDDISCARDIT.LOOSELOCKWIRECANCUTYOUORMAKEYOUIfnecessary,removeanddiscardthelockwirefromthelocknutLoosenthelocknutAdjustthenut(12)untilyoucaninstallthePIN-SETTING(98D27504031000).Makesurethatyoucanseethethreadsoftherod-end(9)throughthecheckhole.Ifyoucannotseethethreadsoftherod-end(9)throughthecheckhole,checktheflaprigging(Ref.AMMTASK27-51-00-820-003).TightenthelocknutInstallthewasher(13)andthenutTORQUEthenut(15)tobetween1.1and1.7m.daN(97.35and150.44NOTE:Itispossibletohaveaclearancebetweenthebushandthestrutattaentbracket.InstallanewIPC-CSN(27-51-05-05-100)cotterpin(14) 第14任务号/TASKNO:Ifyouloosenedthelocknut(10),TORQUEittobetween5.1and5.9m.daN(37.61and43.51lbf.ft).WARNING:WEARGOGGLESWHENYOUREMOVEORINSTALLTHELOCKWIRE.CUT,REMOVEANDDISCARDTHELOCKWIREASYOUDOTHETASK.LOOSELOCKWIRECANCUTORBLINDYOU.Safetythelocknut(10)withMaterialNo.19-010*(LOCKWIRESTAINLSSSTLANNEALED0.8MMDIA).RemovethePIN-SETTING(98D27504031000)fromtheinspection/settingholeintheinterconnectingstrut.WARNING:OBEYTHEMANUFACTURER′SINSTRUCTIONSWHENYOUUSETHIS/THESEMATERIAL/S.USEPROTECTIVECLOTHINGANDRUBBERGLOVES.ApplyalayerofMaterialNo.15-007*(STORAGEPRESERVATION)theheadoftheboltthenutthewasherthecotterpin**27-51-44-865-069-Subtask27-51-44-865-069-C.Removethesafetyclip(s)andthetag(s)andclosethis(these)circuit面板名 识别位PANEL IDENT.49VUFLIGHTCONTROLS/FLP/CTLAND 6CV121VUFLIGHTCONTROLS/FLP/CTL 8CV**ONA/CSubtask27-51-44-865-069-C.Removethesafetyclip(s)andthetag(s)andclosethis(these)circuit27-51-44-710-058-.任务动 结 压入行键<SFCC -MCDU上显示SFCC1页压入行键 -MCDU显示SFCC1SYSSTATUS 第15任务号/TASKNO:STATUSFLP -FLP1NOSFCC2DATACHECKWIRING&SFCC-FLP1FAULTYFLP2DATACHECKSFCC1OR-NOLGCIU1DATACHECKWIRINGTOFLP-FLPLHPROXSNSR1ANDFLPLHPROXSNSR2ORWIRINGTOLGCIU-FLPLHPROXSNSR1ORWIRINGTOLGCIU-FLPLHPROXSNSR2ORWIRINGTOLGCIU-FLPRHPROXSNSR1ANDFLPRHPROXSNSR2ORWIRINGTOLGCIU-FLPRHPROXSNSR1ORWIRINGTOLGCIU-FLPRHPROXSNSR2ORWIRINGTOLGCIU -MCDU显示SFCC1页面 -MCDU显示SYSTEMREPORT/TEST页面压入行键<SFCC -MCDU上显示SFCC2页压入行键 -MCDU显示SFCC2SYSSTATUSSTATUSFLP -FLP2NOSFCC1DATACHECKWIRING&SFCC-FLP2FAULTYFLP1DATACHECKSFCC1OR-NOLGCIU2DATACHECKWIRINGTOFLP-FLPLHPROXSNSR2ANDFLPLHPROXSNSR1ORWIRINGTOLGCIU-FLPLHPROXSNSR1ORWIRINGTOLGCIU-FLPLHPROXSNSR2ORWIRINGTOLGCIU-FLPRHPROXSNSR2ANDFLPRHPROXSNSR1ORWIRINGTOLGCIU-FLPRHPROXSNSR1ORWIRINGTOLGCIU-FLPRHPROXSNSR2ORWIRINGTOLGCIU2Subtask27-51-44-710-058-AD.Getaccesstotheflightcontrols(F/CTL)pageoftheMCDU(Ref.TASKDothistestoftheflapinterconnectingstrutandtheflap-attaentfailure-detectionsensors: Onthe OnthePush(in)thelinekey<;SFCC1.-theMCDUshowstheSFCC1Push(in)thelinekeySYSTEM -theMCDUshowstheSFCC1SYSTEMSTATUSFLP>. STATUSFLAPpage.ThesesubsequentmessagesmustnotFLP1NOSFCC2DATACHECKWIRING&SFCCFLP1FAULTYFLP2DATACHECKSFCC1OR 第16任务号/TASKNO:NOLGCIU1DATACHECKWIRINGTOFLPFLPLHPROXSNSR1andFLPLHPROXSNSR2ORWIRINGTOLGCIUFLPLHPROXSNSR1ORWIRINGTOLGCIUFLPLHPROXSNSR2ORWIRINGTOLGCIUFLPRHPROXSNSR1andFLPRHPROXSNSR2ORWIRINGTOLGCIUFLPRHPROXSNSR1ORWIRINGTOLGCIUFLPRHPROXSNSR2ORWIRINGTOLGCIUPush(in)thelinekey<RETURN.-theMCDUshowstheSFCC1Push(in)thelinekey<RETURN.-theMCDUshowstheSYSTEMREPORT/TESTPush(in)thelinekey<SFCC2.-theMCDUshowstheSFCC2Push(in)thelinekeySYSTEM -theMCDUshowstheSFCC2SYSTEMSTATUSFLP>. STATUSFLAPpage.ThesesubsequentmessagesmustnotFLP2NOSFCC1DATACHECKWIRING&SFCCFLP2FAULTYFLP1DAT