工包航空股份工程技术维修管理部编制

1 DetailedInspectionof -FallExtensionMechanismIncluding编写/修订EditedC工种额定工时MPD审核Examined版本实际工时Real批准ApprovedAMT323300-200-002-NOV<---工信息牌 数 RIGGING RIGGING RIGGING RIGGING RIGGINGPIN,RIGGING-RUDDERSAFETYPIN-NLGDOORSLEEVE-GROUNDLOCK <---材料信息

21工作任务**ONA/C32-33-00-200-002--飞行装-飞行.**ONA/CTASK32-33-00-200-002-DetailedInspectionof-FallMechanismIncludingWARNING:PUTTHESAFETYDEVICESANDTHEWARNINGNOTICESINPOSITIONSTARTATASKONOR-THEFLIGHT-THEFLIGHTCONTROL-THELANDINGGEARANDTHERELATED-COMPONENTSTHATWARNING:MAKESURETHATTHEGROUNDSAFETY-LOCKSAREINPOSITIONONTHE2工作准备信息JobSet-up参 数无规 按无规 按无规 3.Fixtures,Tools,TestandSupport No SAFETYNo WARNINGNo WEDGE-NON RIGGING RIGGING PIN,RIGGING-RUDDER RIGGING RIGGING RIGGING SAFETYPIN-NLG SLEEVE-GROUND.参 名 FR34 从FR1FR12 从FR1FR12 FR12FR24 FR12FR24 客舱地板图1驾驶 基座后盖板-位置图前货舱 盖板图 411.B.Referenced CheckoftheControl RemovaloftheForward partmentPartitionFR34 Installationofthe partment OpentheMainGearDoorsforAccess ClosetheMainGearDoorsafterAccess NoseGearDoors-GroundDoorsOpening NoseGearDoors-GroundDoors OpentheFWDor partmentDoorwithYellowElectric ClosetheFWDor partmentDoorwithYellowElectric OpentheAvionicsCompartmentDoorsforAccess ClosetheAvionicsCompartmentDoorsafterAccess RemovaloftheCockpitFloorPanelsfromFR1ThruFR12 InstallationoftheCockpitFloorPanelsfromFR1 RemovaloftheCabinFloorPanelsfromFR12thruFR24 InstallationoftheCabinFloorPanelsfromFR12 RemovaloftheCabinFloor InstallationoftheCabinFloorPanels RemovaloftheCabinFloorPanels InstallationoftheCabinFloorPanelsNOTE:Referenceapplicablenedrawings.CabinFloorPanelsSHEETCockpitCenter-PedestalRearCover-LocationSHEET1 partmentAccessPanelsSHEET1CockpitandCabinFloorPanelsSHEET1 partmentAccessPanelsSHEET-FallExtensionSystem-RiggingPinsandDetailsSHEET1--FallExtensionSystem-InspectionAreasandDetailsSHEET1-3工作准备JobSet- 5(参考图.驾驶舱 基座后盖板-位置图1)(参考图.前货舱-(参考图.驾驶舱和客舱地板图1)(参考图.前货舱-盖板图**ONA/C32-33-00-941-064-A.在面板400VU6GADOWN在面板110VU,确保GRAVITYGEAREXTN手柄折叠进入主控台在每侧GRAVITYGEAREXTN.NOTE:Referenceapplicablenedrawings.(Ref.Fig.CabinFloorPanelsSHEET1)(Ref.Fig.CockpitCenter-PedestalRearCover-LocationSHEET1)(Ref.Fig.Forward partmentAccessPanelsSHEET1)(Ref.Fig.CockpitandCabinFloorPanelsSHEET1)(Ref.Fig. partmentAccessPanelsSHEET**ONA/CSubtask32-33-00-941-064-SafetyPuttheSAFETYBARRIER(S)inMakesurethatthegroundsafetylocksareonthelandingOnthepanelmakesurethatthelanding-gearcontrol-lever6GAisintheDOWNputaWARNINGNOTICE(S)inpositiontolsnottooperatethelandinggear.Onthepanel110VU,makesurethattheGRAVITYGEAREXTNhandleisfoldedintothecenterconsole.InstallaWEDGE-NONMETALLIConeachsideoftheGRAVITYGEAREXTNhandletolockthehandleinposition.**ONA/C001-001,003-003,051-PRESB53-1143forA/C001-001,003-32-33-00-010-051-AMM32-22-00-010-001(98D32203502000) 6AMM32-12-00-010-001 打开电子设备舱右侧舱门822(AMM52-41-00-010-002825(AMM52-30-00-860-001131AC,131BC,131CC拆卸前货舱的后隔板132PWAMM25-54-12-000-001)拆卸驾驶舱地板211FF、211JF、212GF(AMM53-12-11-000-001)221AF,221DF,231AF,231BF(AMM53-12-12-000-001)232LF(AMM53-22-12-000-001)(参见AMM任务53-32-12-000-002)。(参见AMM任务53-32-12-000-002)。拆下后部护罩(在GEARGRAVITYEXTN手柄下面)(参考图.驾驶舱基座后盖板-位置图.**ONA/C001-001,003-003,051-PRESB53-1143forA/C001-001,003-003Subtask32-33-00-010-051-AB.GetOpentheNLGdoors(Ref.AMMTASK32-22-00-010-MakesurethataSAFETYPIN-NLGDOOR(98D32203502000)isinstalledineachNLGdoor.OpentheMLGdoors(Ref.AMMTASK32-12-00-010-MakesurethattheSLEEVE-GROUNDLOCK( )isontheapplicableMLGdooractuator.Openthe partmentlal-rightdoor822(Ref.AMMTASK52-41-00-010-002).Opentheforward partmentdoor825(Ref.AMMTASK52-30-00-860-001).Removethe partmentceilingpanels131AC,131BC,Removetherearpartition132PWoftheforward (Ref.AMMTASK25-54-12-000-001).Removethecockpitfloorpanels211FF,211JF,212GF(Ref.AMMTASK53-12-11-000-001).WARNING:MAKESURETHATTHESAFETYDEVICESANDTHEWARNINGNOTICESAREINPOSITIONWHENTHETRAPDOOR(231AF)ISOPEN.INJURYCANOCCURIFSFALLTHROUGHTHERemovethecabinfloorpanels221AF,221DF,231AF,231BF(Ref.AMMTASK53-12-12-000-001).Removethecabinfloorpanel232LF(Ref.AMMTASK53-22-12-000-Removethecabinfloorpanels242BF,241EF,241FF,242FF, 7(Ref.AMMTASK53-32-12-000-Removethecabinfloorpanels242MF,242LF,242KF,241JF,241KF,241LF,241MF(Ref.AMMTASK53-32-12-000-002).Removethecockpitcenter-pedestalrearcover(belowtheGEARGRAVITYEXTNhandle).(Ref.Fig.CockpitCenter-PedestalRearCover-LocationSHEET**ONA/C002-002,004-049,054-099,101-149,201-249,251-299,301-350,451-POSTSB53-1143forA/C001-001,003-32-33-00-010-051-B.AMM32-22-00-010-001(98D32203502000)AMM32-12-00-010-001 打开电子设备舱右侧舱门822(AMM52-41-00-010-002825(AMM52-30-00-860-001131AC,131BC,131CC拆卸前货舱的后隔板132PWAMM25-54-12-000-001)拆卸驾驶舱地板211FF、211JF、212GF(AMM53-12-11-000-001)拆卸客舱地板221LF,221DF231AF,231BF(AMM53-12-12-000-001)232LF(AMM53-22-12-000-001)(参见AMM任务53-32-12-000-002)。(参见AMM任务53-32-12-000-002)。拆下后部护罩(在GEARGRAVITYEXTN手柄下面).**ONA/C002-002,004-049,054-099,101-149,201-249,251-299,301-350,451-POSTSB53-1143forA/C001-001,003-003Subtask32-33-00-010-051-DB.GetOpentheNLGdoors(Ref.AMMTASK32-22-00-010-MakesurethataSAFETYPIN-NLGDOOR(98D32203502000)isinstalledineachNLGdoor.OpentheMLGdoors(Ref.AMMTASK32-12-00-010-MakesurethattheSLEEVE-GROUNDLOCK( )isontheapplicableMLGdooractuator.Open partmentlal-rightdoor 8(Ref.AMMTASK52-41-00-010-Opentheforward partmentdoor825(Ref.AMMTASK52-30-00-860-001).Removethe partmentceilingpanels131AC,131BC,Removetherearpartition132PWoftheforward (Ref.AMMTASK25-54-12-000-001).Removethecockpitfloorpanels211FF,211JF,212GF(Ref.AMMTASK53-12-11-000-001).WARNING:MAKESURETHATTHESAFETYDEVICESANDTHEWARNINGNOTICESAREINPOSITIONWHENTHETRAPDOOR(231AF)ISOPEN.INJURYCANOCCURIFSFALLTHROUGHTHERemovethecabinfloorpanels221LF,221DF,231AF,231BF(Ref.AMMTASK53-12-12-000-001).Removethecabinfloorpanel232LF(Ref.AMMTASK53-22-12-000-Removethecabinfloorpanels242BF,241EF,241FF,242FF,242GF(Ref.AMMTASK53-32-12-000-002).Removethecabinfloorpanels242MF,242LF,242KF,241JF,241KF,241LF,241MF(Ref.AMMTASK53-32-12-000-002).Removethecockpitcenter-pedestalrearcover(belowtheGEARGRAVITYEXTNhandle).(Ref.Fig.CockpitCenter-PedestalRearCover-LocationSHEET**ONA/C151-199,351-450,701-32-33-00-010-051-B.AMM32-22-00-010-001(98D32203502000)AMM32-12-00-010-001 打开电子设备舱右侧舱门822(AMM52-41-00-010-002825(AMM52-30-00-860-001131MC,131NC拆卸前货舱的后隔板132PWAMM25-54-12-000-001)拆卸驾驶舱地板211FF、211JF、212GF(AMM53-12-11-000-001)拆卸客舱地板221LF,221DF231AF,231BF(AMM53-12-12-000-001)232LF(AMM53-22-12-000-001)242BF,241EF,241FF,242FF,242GF(参见AMM任务53-32-12-000-002)。242MF,242LF,242KF,241JF,241KF,241LF,241MF(参见AMM任务53-32-12-000-002)。拆下后部护罩(在GEARGRAVITYEXTN手柄下面)(参考图.驾驶舱基座后盖板-位置图 9.**ONA/C151-199,351-450,701-850Subtask32-33-00-010-051-EB.GetOpentheNLGdoors(Ref.AMMTASK32-22-00-010-MakesurethataSAFETYPIN-NLGDOOR(98D32203502000)isinstalledineachNLGdoor.OpentheMLGdoors(Ref.AMMTASK32-12-00-010-MakesurethattheSLEEVE-GROUNDLOCK( )isontheapplicableMLGdooractuator.Openthe partmentlal-rightdoor822(Ref.AMMTASK52-41-00-010-002).Opentheforward partmentdoor825(Ref.AMMTASK52-30-00-860-001).Removethe partmentceilingpanels131MC,Removetherearpartition132PWoftheforward (Ref.AMMTASK25-54-12-000-001).Removethecockpitfloorpanels211FF,211JF,212GF(Ref.AMMTASK53-12-11-000-001).WARNING:MAKESURETHATTHESAFETYDEVICESANDTHEWARNINGNOTICESAREINPOSITIONWHENTHETRAPDOOR(231AF)ISOPEN.INJURYCANOCCURIFSFALLTHROUGHTHERemovethecabinfloorpanels221LF,221DF,231AF,231BF(Ref.AMMTASK53-12-12-000-001).Removethecabinfloorpanel232LF(Ref.AMMTASK53-22-12-000-Removethecabinfloorpanels242BF,241EF,241FF,242FF,242GF(Ref.AMMTASK53-32-12-000-002).Removethecabinfloorpanels242MF,242LF,242KF,241JF,241KF,241LF,241MF(Ref.AMMTASK53-32-12-000-002).Removethecockpitcenter-pedestalrearcover(belowtheGEARGRAVITYEXTNhandle).(Ref.Fig.CockpitCenter-PedestalRearCover-LocationSHEET4工作 11**ONA/C001-049,051-099,101-149,151-199,201-249,251-299,351-509,511-32-33-00-210-059- 10FR7FR12AMM20-24-12-200-001在FR9和FR10上的两根钢索接头是的和松紧螺套是紧的FR12FR16AMM20-24-12-200-001FR14FR24A(AMM20-24-12-200-001FR24AFR36AMM20-24-12-200-001FR23,FR28FR33FR23和FR28之间的钢索接头是的和松紧螺套是拧紧的FR34FR46AMM20-24-12-200-001钢索的压力密封件(FR42FR43)钢索接头(FR42FR43.NOTE:Referenceapplicablene(Ref.Fig. -FallExtensionSystem-RiggingPinsandDetailsSHEET1-4)(Ref.Fig. -FallExtensionSystem-InspectionAreasandDetailsSHEET1-2)**ONA/C001-049,051-099,101-149,151-199,201-249,251-299,351-509,511-Subtask32-33-00-210-059-A.DetailedInspectionofthe-FallMechanismDoacheckofthecablesfromFR7thru(Ref.AMMTASK20-24-12-200-001)tomakesuretheyareattachedandconnectedcorrectlywiththeendfittingsnotpulledouttheydonothavekinks,brokenwiresortoomuchthetwocableconnectorsatFR9andFR10aresafetiedandtheturnbucklesaretight.DoacheckofthecablesfromFR12thru(Ref.AMMTASK20-24-12-200-001)tomakesuretheydonothavekinks,brokenwiresortoomuchthecableguidesatFR14arenotdamagedanddonothavetoomuchDoacheckofthecablesfromFR14thruFR24A(PassengerCompartment)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:theydonothavekinks,brokenwiresortoomuchDoacheckofthecablesfromFR24AthruFR36(ForwardCompartment)(Ref.AMMTASK20-24-12-200-001)tomakesurethat: 11theydonothavekinks,brokenwiresortoomuchthecableguidesatFR23,FR28andFR33arenotdamagedanddonothavetoomuchwearthecableconnectorsbetweenFR23andFR28aresafetiedandtheturnbucklesaretight.DoacheckofthecablesfromFR34thruFR46(MLGBay)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:thecablepressureseals(FR42toFR43)areattachedcorrectlyandarenotwornthecableguides(FR42)arenotdamagedanddonothavetoomuchthecableconnectors(FR42toFR43)aresafetiedandtheturnbucklesaretheyhavenokinks,brokenwiresorsignsof**ONA/C301-350,551-32-33-00-210-059-FR7FR12AMM20-24-12-200-001在FR9和FR10上的两根钢索接头是的和松紧螺套是紧的FR12FR16AMM20-24-12-200-001FR14FR24A(AMM20-24-12-200-001FR24AFR36AMM20-24-12-200-001FR23,FR28FR33FR34FR46AMM20-24-12-200-001钢索的压力密封件(FR42FR43)钢索接头(FR42FR43.**ONA/C301-350,551-650A.DetailedInspectionofthe-FallMechanism(1)DoacheckofthecablesfromFR7thru(Ref.AMMTASK20-24-12-200-001)tomakesure-theyareattachedandconnectedcorrectlywiththeendfittings 12pulledtheydonothavekinks,brokenwiresortoomuchthetwocableconnectorsatFR9andFR10aresafetiedandtheturnbucklesaretight.DoacheckofthecablesfromFR12thru(Ref.AMMTASK20-24-12-200-001)tomakesuretheydonothavekinks,brokenwiresortoomuchthecableguidesatFR14arenotdamagedanddonothavetoomuchDoacheckofthecablesfromFR14thruFR24A(PassengerCompartment)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:theydonothavekinks,brokenwiresortoomuchDoacheckofthecablesfromFR24AthruFR36(ForwardCompartment)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:theydonothavekinks,brokenwiresortoomuchthecableguidesatFR23,FR28andFR33arenotdamagedanddonothavetoomuchwearthecableconnectorsatFR36aresafetiedandtheturnbucklesareDoacheckofthecablesfromFR34thruFR46(MLGBay)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:thecablepressureseals(FR42toFR43)areattachedcorrectlyandarenotwornthecableguides(FR42)arenotdamagedanddonothavetoomuchthecableconnectors(FR42toFR43)aresafetiedandtheturnbucklesaretheyhavenokinks,brokenwiresorsignsof**ONA/C32-33-00-860-077-B.飞机结110VU,从GRAVITYGEAREXTNGRAVITYGEAREXTN手柄。顺时针全面转动GRAVITYGEAREXTN将GRAVITYGEAREXTN在GRAVITYGEAREXTN1.**ONA/CSubtask32-33-00-860-077-B.AircraftMaintenanceWARNING:MAKESURETHATTHEWARNINGNOTICESAREINPOSITIONWHENYOUTHE-FALLMECHANISMCABLES.INJURYCANOCCURIFNEL 13LOOSE ECAUGHTINTHEWARNING:MAKESURETHEREARENONELNEARTHE-FALLMECHANISMCABLESBEFOREYOUTURNTHEGRAVITYGEAREXTNHANDLE.INJURYCANOCCURIFNELORLOOSECLOTHING ECAUGHTINTHE-FALLOnthepanel110VU,removetheWEDGE-NONMETALLICfromtheGRAVITYGEAREXTNhandle.MovetheGRAVITYGEAREXTNhandlefromthefoldedposition.TurntheGRAVITYGEAREXTNhandleclockwisethreefullFoldtheGRAVITYGEAREXTNhandleintothecenterInstallaWEDGE-NONMETALLIConeachsideoftheGRAVITYGEAREXTNhandletolockthehandleintoposition.32-33-00-210-060-FR7FR12)之前检查钢索不能看见的部份(参见AMM任务20-24-12-200-001)以确保:FR12FR16)之前检查钢索不能看见的部份(参见AMM任务20-24-12-200-001)以确保:FR14FR24A-客舱)之前检查钢索不能看见的部份(参见AMM任务20-24-12-200-001)以确保:FR24AFR36-前舱)之前检查钢索不能看见的部份(参见AMM任务20-24-12-200-001)以确保:FR34FR46-主起落架舱)之前检查钢索不能看见的部份(参见AMM任务20-24-12-200-001)以确保:.Subtask32-33-00-210-060-C.DetailedInspectionofthe-FallMechanismCablesafterthe-fallMechanismhasbeenMovedCheckthepartofthecablesthatcouldnotbeseenbefore(fromFR7thruFR12)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:theydonothavekinks,brokenwiresortoomuchCheckthepartofthecablesthatcouldnotbeseenbefore(fromFR12thruFR16)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:theydonothavekinks,brokenwiresortoomuchCheckthepartofthecablesthatcouldnotbeseenbefore(fromFR14thruFR24A-PassengerCompartment)(Ref.AMMTASK20-24-12-200-001)tomakesure 14-theydonothavekinks,brokenwiresortoomuchCheckthepartofthecablesthatcouldnotbeseenbefore(fromFR24AthruFR36-ForwardCompartment)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:theydonothavekinks,brokenwiresortoomuchCheckthepartofthecablesthatcouldnotbeseenbefore(fromFR34thruFR46-MLGBay)(Ref.AMMTASK20-24-12-200-001)tomakesurethat:theyhavenokinks,brokenwiresorsignsof32-33-00-860-078-D.飞机结110VU,从GRAVITYGEAREXTNGRAVITYGEAREXTN手柄。逆时针全面转动GRAVITYGEAREXTN将GRAVITYGEAREXTN在GRAVITYGEAREXTN1.Subtask32-33-00-860-078-D.AircraftMaintenanceWARNING:MAKESURETHATTHEWARNINGNOTICESAREINPOSITIONWHENYOUMOVETHE-FALLMECHANISMCABLES.INJURYCANOCCURIFNELORLOOSECLOTHINGECAUGHTINTHEMECHANISM.WARNING:MAKESURETHEREARENONELNEARTHE-FALLMECHANISMCABLESBEFOREYOUTURNTHEGRAVITYGEAREXTNHANDLE.INJURYCANOCCURIFNELORLOOSECLOTHING ECAUGHTINTHE-FALLOnthepanel110VU,removetheWEDGE-NONMETALLICfromtheGRAVITYGEAREXTNhandle.MovetheGRAVITYGEAREXTNhandlefromthefoldedposition.TurntheGRAVITYGEAREXTNhandlecounterclockwisethreefullFoldtheGRAVITYGEAREXTNhandleintothecenterInstallaWEDGE-NONMETALLIConeachsideoftheGRAVITYGEAREXTNhandletolockthehandleintoposition.32-33-00-480-052-E..Subtask32-33-00-480-052- 15E.InstallationoftheRiggingNOTE:Itisimportanttoinstalltheriggingpinsexactlyasgivenintheprocedure.Thiswillmakesurethatallthedatumpositionsarecorrect.(1)InstalltheRIGGINGPIN(98A27801001000)atpositionPin1.Makesurethattheriggingpingoesthroughthepulleyframeandthepulley.Keeptheriggingpinin32-33-00-210-056-F.FR7FR12检查GEARGRAVITYEXTN确保FR8FR12.Subtask32-33-00-210-056-F.DetailedInspectionfromFR7thruExaminetheGEARGRAVITYEXTNhandleforAtthereductiongearboxmakesureitisattachedcorrectlyandthepartsthatattachthegearboxarethedriveshaftisfromdamage,cracksandthedriveshaftisattachedthepulleystopscrewsaresafetiedandthepulleyshearpinsarenotdamagedorthepulleyisnotloose,damagedorMakesurethatthetransmissionrodbetweenthereductiongearboxandthepulleyatFR8isnotloose,damagedorcracked.MakesurethatthetwopulleysatFR8andFR12arenotloose,damagedorMakesurethatthecableretainingpinsonthepulleyatFR12arenotdamagedorcrackedandareattachedcorrectly.32-33-00-210-057-G.FR12FR16 16.Subtask32-33-00-210-057-G.DetailedInspectionfromFR12thruAtthepulley(FR16)makesureitisnotloose,damagedorthesupportbracketisattachedtheverticalshaftisnotloose,damagedor32-33-00-480-053-H.FR13FR19(NLG.Subtask32-33-00-480-053-H.InstallationoftheRiggingPinsfromFR13thruFR19(NLG-RIGGINGPIN(98A32301000000)atpositionPin13.Makesurethattheriggingpingoesthroughtheleverintotheuplock.Keeptheriggingpininposition.RIGGINGPIN(98A32301000000)atpositionPin14.Makesurethattheriggingpingoesthroughtheleverintheframe.KeeptheriggingpininPIN,RIGGING-RUDDERCONTROL(98A27901002000)atpositionPinMakesurethattheriggingpingoesthroughtheleverandthesupport.Keeptheriggingpininposition.RIGGINGPIN(98A32301000000)atpositionPin16.Makesurethattheriggingpingoesthroughtheleverintotheuplock.Keeptheriggingpininposition.32-33-00-210-058-J.FR13FR19. 17Subtask32-33-00-210-058-J.DetailedInspectionfromFR13thruFR19(NLGAttherodsmakesuretheyarenotloose,damagedortherodendfittingsaretightand32-33-00-480-054-K.FR34FR46 )在定位销2和销11处，确保校装销通过框和滑轮， )在定位销3和销7处，确保校装销通过手柄和支架， )在定位销4,销6,销8和销9处，确保校装销通过 .Subtask32-33-00-480-054-K.InstallationoftheRiggingPinsfromFR34thruFR46(MLGRIGGINGPIN(98DNSA )atpositionsPin2andPin11.Makesurethattheriggingpingoesthroughtheframeandthepulley.Keeptheriggingpinsinposition.RIGGINGPIN(98DNSA)atpositionsPin3andPin7.Makesurethattheriggingpingoesthroughtheleverandthesupport.Keeptheriggingpinsinposition.RIGGINGPIN(98DNSA )atpositionsPin4,Pin6,Pin8andPin9.Makesurethattheriggingpingoesthroughtheleverintotheuplock.Keeptheriggingpinsinposition.RIGGINGPIN(98DNSA)atpositionPin5.Makesurethattheriggingpingoesthroughtheleverintothecut-outvalve.KeeptheriggingpininRIGGINGPIN(98DNSA )atpositionPin10.Makesurethattheriggingpingoesthroughtheleverintothevalve.KeeptheriggingpininRIGGINGPIN(98A27003001000)atpositionPin12.Makesurethattheriggingpingoesthroughtheframeandthepulley.Keeptheriggingpinin 1832-33-00-210-062-L.FR34FR463.4mm(0.134in..Subtask32-33-00-210-062-L.DetailedInspectionbetweenFR34andFR46(MLGAtthepulleysmakesuretheyarenotloose,damagedorthepulleysupportbracketsareattachedcorrectlyandarenotcrackedordamagedthepulleyshearpins(FR41)arenotdamagedorthecableretainingpinsarenotdamagedandareattachedAttherodsmakesuretheyarenotloose,damagedortherodendfittingsaretightandAtthetorqueshafts(FR43)makesuretheyarenotdamagedorthesupportbracketsarenotdamagedandareattachedtheaxialmovementislessthan3.4mm(0.134NOTE:Permittedaxialmovementcanincludemovementbetweenthefloatingbearingsandthesupportbracket.32-33-00-080-051-M.12(98A27003001000拆卸在定位销10处的校装销 2345,6,78,911 15(98A27901002000)13,1416(98A32301000000 19(6)1(98A27801001000).Subtask32-33-00-080-051-M.RemovaloftheRiggingRemovetheRIGGINGPIN(98A27003001000)atpositionPinRemovetheRIGGINGPIN )atpositionPinRemovetheRIGGINGPIN(98DNSA )atpositionsPin2,Pin3,Pin4,Pin5,Pin6,Pin7,Pin8,Pin9andPin11.RemovethePIN,RIGGING-RUDDERCONTROL(98A27901002000)atpositionPinRemovetheRIGGINGPIN(98A32301000000)atpositionsPin13,14andRemovetheRIGGINGPIN(98A27801001000)atpositionPin5结束 Close**ONA/C001-001,003-003,051-PRESB53-1143forA/C001-001,003-32-33-00-410-051-A. (参考图.驾驶 基座后盖板-位置图安装驾驶舱地板面板211FF、211JF、212GF(AMM53-12-11-400-001)221AF,221DF,231AF,231BF(AMM53-12-12-400-001)安装客舱地板232LF(AMM53-22-12-400-001)(参见AMM任务53-32-12-400-002)。(参见AMM任务53-32-12-400-002)。132PW(AMM25-54-12-400-001)825(AMM52-30-00-860-002822(AMM52-41-00-410-002AMM32-12-00-410-001AMM32-22-00-410-001110VU,从GRAVITYGEAREXTN.**ONA/C001-001,003-003,051-PRESB53-1143forA/C001-001,003-003Subtask32-33-00-410-051-ACloseMakesurethattheworkareaiscleanandclearoftool(s)andotherInstallthecockpitcenter-pedestalrear 20(Ref.Fig.CockpitCenter-PedestalRearCover-LocationSHEETInstallthecockpitfloorpanels211FF,211JF,212GF(Ref.AMMTASK53-12-11-400-001).Installthecabinfloorpanels221AF,221DF,231AF,231BF(Ref.AMMTASK53-12-12-400-001).Installthecabinfloorpanel232LF(Ref.AMMTASK53-22-12-400-Installthecabinfloorpanels242BF,242GF,242FF,241EF,241FF(Ref.AMMTASK53-32-12-400-002).Installthecabinfloorpanels242MF,242LF,242KF,241JF,241KF,241LF,241MF(Ref.AMMTASK53-32-12-400-002).Installtherearpartition132PWoftheforward (Ref.AMMTASK25-54-12-400-001).Installthe partmentceilingpanels131AC,131BC,Closetheforward partmentdoor825(Ref.AMMTASK52-30-00-860-002).Closethe partmentlal-rightdoor822(Ref.AMMTASK52-41-00-410-002).ClosetheMLGdoors(Ref.AMMTASK32-12-00-410-ClosetheNLGdoors(Ref.AMMTASK32-22-00-410-Onthepanel110VU,removetheWEDGE-NONMETALLICfromtheGRAVITYGEAREXTNhandle.**ONA/C002-002,004-049,054-099,101-149,201-249,251-299,301-350,451-POSTSB53-1143forA/C001-001,003-32-33-00-410-051-A. (参考图.驾驶 基座后盖板-位置图安装驾驶舱地板面板211FF、211JF、212GF(AMM53-12-11-400-001221LF,221DF,231AF,231BFAMM53-12-12-400-001)安装客舱地板232LF(53-22-12-400-001)(参见AMM任务53-32-12-400-002)。(参见AMM任务53-32-12-400-002)。132PW(AMM25-54-12-400-001)131AC,131BC,131CC825(AMM52-30-00-860-002822(AMM52-41-00-410-002AMM32-12-00-410-001AMM32-22-00-410-001110VU,从GRAVITYGEAREXTN 21.**ONA/C002-002,004-049,054-099,101-149,201-249,251-299,301-350,451-POSTSB53-1143forA/C001-001,003-003Subtask32-33-00-410-051-DA.CloseMakesurethattheworkareaiscleanandclearoftool(s)andotherInstallthecockpitcenter-pedestalrear(Ref.Fig.CockpitCenter-PedestalRearCover-LocationSHEETInstallthecockpitfloorpanels211FF,211JF,212GF(Ref.AMMTASK53-12-11-400-001).Installthecabinfloorpanels221LF,221DF,231AF,231BF(Ref.AMMTASK53-12-12-400-001).Installthecabinfloorpanel232LF(Ref.AMMTASK53-22-12-400-Installthecabinfloorpanels242BF,242GF,242FF,241EF,241FF(Ref.AMMTASK53-32-12-400-002).Installthecabinfloorpanels242MF,242LF,242KF,241JF,241KF,241LF,241MF(Ref.AMMTASK53-32-12-400-002).Installtherearpartition132PWoftheforward (Ref.AMMTASK25-54-12-400-001).Ins