內(nèi)容az h71 22 00 000wono工作指令號(hào)

HongKongAirlinesHongKongAirlines HongKongAirlinesRepetiveInspcetionOfCFM56-5BAfterEngineMountInnerSBRA32071-160R00,SBA320-71-1060R02,ADCAD2013-A320-動(dòng)力MPItem/MPMPREV/MPMPD712215-01-1,EASA Issue2Revision365CA11(必需2TOOL-ZEROLOCKING,1(必需3放大鏡-10倍(按名稱核實(shí)1(必需1FIBERSCOPESET(孔探設(shè)備-纖孔探儀1213141(視情/As注釋：請(qǐng)工作者嚴(yán)格按照工作指令號(hào)領(lǐng)取預(yù)定的航材裝機(jī)13(視情/As23(視情/As33(視情/AsNOTE:ThecomponentinPN,SNformisneedtodoperiodicmaintenance.Forthereturnrepairorretrofit，theformisPN,SNoftheremovedcomponent.AndthePN-IN,SN-INwouldbewrittenaccordingtonewpartsafterfinish.Forthenon-returns(suchasweight,test)，theformisPN,SNoftheon-wingmaintenancecomponent.AndfillthePN-IN,SN-INwithbiasafterfinish.LEFTIntheeventofanydiscrepanciesbetweentheChineseinstructionandtheEnglishinstruction,theEnglishprocedureshouldCertificateofReleaseto (*Tickas #DifferentcrewsshouldperformtheworkoneachoftheCertifiesthattheworkspecified,exceptasotherwisespecified,wascarriedoutinaccordancewithHKAR-145andinrespecttothatwork,Theaircraft/aircraftcomponentsareconsideredreadyforReleasetoService.□HKAApprovalNo:AI/135/706 □CASLApprovalNo:AI/101/798 □TAECOApprovalNo.:DAI/89/1295□HAECOApprovalNo:DAI/1/853 □SMECOApprovalNo:JMM081,D.400009*□AMECOApprovalNo.: □ RepetiveInspcetionOfCFM56-5BAfterEngineMountInnerNOTE:Pleasefeedbackthepartsofphotoestots@ifthereisafindingwhenyouperformthisTASK.OpenthefancowldoorsrefertoAMMTASK71-13-00-010-040-OpenthethrustreverserdoorrefertoAMMTASK78-36-00-010-040-InspectionoftheInnerRetainers(3locations,P/N238-0252-505)perthefollowingNOTE：PaycloseattentiontotheinnerbendoftheNOTE：Thecenterretainermaybedifficulttoinspectvisually,thenanarticulatedfiberscopecanbeusedasahelp.Incaseofdoubt,removetheretainerasperprocedureA.4forinspection.參考步驟A.4拆下保持片做檢查。Cleananydirtorunwantedmaterialfromtheaftenginemountwithalint-freecotton Withouttheremovalofanyhardware,doavisualinspectionoftheinnerretaineritem(8)inFigure2forcracksusing10xmagnification,mirrorandlight.RefertoFigure1&Figure4.Forretainerswhicharedullsurfacefinishesorcrackedorfailed,proceedtostepA.4throughForretainers(brightsurfacefinish)withoutcracksandnotfailed,nofurtheractionisrequired.proceeddirectlytoprocedureA.8throughA.11.RemovalofOuterRetainers(3locations)perthefollowingNOTE1：Thistaskcanbeaccomplisedonwing,eventhroughclearanceistight,usingMMMTTTRepetiveInspcetionOfCFM56-5BAfterEngineMountInnerNOTE2：DonotremovethepinsItem(1)and(2)andtheanti-rotationbracketItem(3)fromlinkassemblyItem(5)inFIG3whenyouremovethenutsitem(10)and(11)inFigure(1).Withouttheuseoftheenginebootstrapsystem,removethefollowingparts:theboltsitem(6),thewashersitem(7),thewashersitem(13),andthenutsitem(14)thatattachtheouterretainerstotheinnerretainers.RefertoFigureT(2).Removetheouterretainersitem(9)anditem(12).RefertoFigureT(3).Inspectforagapbetweenthepinheadandanti-rotationbracket.RefertoFigure2andT(4).Ifthereisagapofmorethan0.001inch(0.025mm),refertoprocedureA.5toinstallthebootstrapsystem.T(5).Ifthegapislessthan0.001inch(0.025mm),refertoprocedureA.6toreplacetheInnerretainers(3locations).T5.InstallthebootstrapsystemtotaketheengineweightoffoftheaftenginemountperthefollowingT(1).MakesurethattheslatsareretractedandinstallTOOL-ZEROLOCKING,FLAPSLATCTLLEVER(98D27803500001)ontheflapandslatcontrollever.(2).Openthethrustreverserdoorstothe45degreesposition(Ref.AMMTASK78-36-00-010-RepetiveInspcetionOfCFM56-5BAfterEngineMountInner6.ReplacementoftheInnerRetainers(3locations)perthefollowingprocedure.RefertoFigure(1).Inspectthenutsitem(10)anditem(11)foranyloosenessorwear.Iflooseorworn,replace.RecordtheconditionofnutsinSheet1.T(2).Applytorqueonlargenutitem(10)inthetighteningdirectionwithanopenendtypeadapteroratorquewrenchat80lbf.ft.RecordifthereisanymovementofthenutinSheet1.T(3).Applytorqueonsmallnutitem(11)inthetighteningdirectionwithatorquewrenchsetat35lbf.ft.RecordifthereisanymovementofthenutinSheet1.T(4).RemovethefollowingpartsinaccordancewithAMM71-22-11-000-043section4.A.(3):thenutsitem(10)anditem(11).T(5).Removetheinnerretaineritem(8).Refertosection4.A.(3)ofAMM71-22-11-000-T(6).Repalcetheinnerretaineritem(8).Refertosection4.G.(11)ofAMM71-22-11-400-T7.ReplacementoftheouterRetainers(3locations)perthefollowing(1).InstalltheouterRetainers(3locations)inaccordancewithAMM71-22-11-400-043sectionM(2).IfInstalled,removetheBootstrapsystemrefertoAMM71-22-11-400-043-AsectionM8.Ifneeded,closethethrustreverserdoorsrefertoAMMTASK78-36-00-410-040-MMRepetiveInspcetionOfCFM56-5BAfterEngineMountInnerIfneeded,removeTOOL-ZEROLOCKING,FLAPSLATCTLLEVER(98D27803500001)onflapandslatcontrolFilltheSheet1,andfeedbacktoInspectionoftheInnerRetainers(3locations,P/N238-0252-505)perthefollowingprocedure.Ifthereisnoaftenginemountonspareengine,gotoprocedureB.5directlyifnorearmountinstalled.接執(zhí)行步驟B.5。NOTE：PaycloseattentiontotheinnerbendoftheNOTE：Thecenterretainermaybedifficulttoinspect.Incaseofdoubt,removetheretainerasperprocedureB.2forinspection.Cleananydirtorunwantedmaterialfromtheaftenginemountwithalint-freecotton Withouttheremovalofanyhardware,doavisualinspectionoftheinnerretaineritem(8)inFigure2forcracksusing10xmagnification,mirrorandlight.RefertoFigure1&Figure4.Forretainerswhicharedullsurfacefinishesorcrackedorfailed,proceedtostepB.2throughForretainers(brightsurfacefinish)withoutcracksandnotfailed,nofurtheractionisrequired.proceeddirectlytoprocedureB.5.RemovalofOuterRetainers(3locations)perthefollowingNOTE1：Thistaskcanbeaccomplisedonwing,eventhroughclearanceistight,usingthefollowingproceduresB.2(1)throughB.2(2).MMTTTTRepetiveInspcetionOfCFM56-5BAfterEngineMountInnerNOTE2：DonotremovethepinsItem(1)and(2)andtheanti-rotationbracketItem(3)fromthelinkassemblyItem(5)inFIG3whenyouremovethenutsitem(10)and(11)inFigure2.銷子（2）和防轉(zhuǎn)支架（3。(1).Withouttheuseoftheenginebootstrapsystem,removethefollowingparts:theboltsitem(6),thewashersitem(7),thewashersitem(13),andthenutsitem(14)thatattachtheouterretainerstotheinnerretainers.RefertoFigure2.T(2).Removetheouterretainersitem(9)anditem(12).RefertoFigureT3.ReplacementoftheInnerRetainers(3locations)perthefollowingprocedure.RefertoFigure(1).Inspectthenutsitem(10)anditem(11)foranyloosenessorwear.Iflooseorworn,replace.RecordtheconditionofnutsinSheet1.T(2).Applytorqueonlargenutitem(10)inthetighteningdirectionwithanopenendtypeadapteroratorquewrenchat80lbf.ft.RecordifthereisanymovementofthenutinSheet1.T(3).Applytorqueonsmallnutitem(11)inthetighteningdirectionwithatorquewrenchsetat35lbf.ft.RecordifthereisanymovementofthenutinSheet1.T(4).RemovethefollowingpartsinaccordancewithAMM71-22-11-000-043section4.A.(3):thenutsitem(10)anditem(11).T(5).Removetheinnerretaineritem(8).Refertosection4.A.(3)ofAMM71-22-11-000-T(6).Repalcetheinnerretaineritem(8).Refertosection4.G.(11)ofAMM71-22-11-400-TRepetiveInspcetionOfCFM56-5BAfterEngineMountInner4.ReplacementoftheouterRetainers(3locations)perthefollowing(1).InstalltheouterRetainers(3locations)inaccordancewithAMM71-22-11-400-043section5.FilltheSheet1,andfeedbacktoTMRepetiveInspcetionOfCFM56-5BAfterEngineMountI