工包航空股份工程技術(shù)維修管理部編制

中文標(biāo)題:第1 CheckoftheRudderServoControlsandHingeBearingsfortoo yandCondition任務(wù)號(hào)/TASKNO:工作區(qū)域編寫(xiě)/修訂Edited日期B工種額定工時(shí)MPD審核Examined日期版本實(shí)際工時(shí)Real批準(zhǔn)Approved日期AMM272400-200-001-NOV適用性 To：出廠序號(hào)：003611，機(jī)身號(hào)：003611，有效性號(hào)<---工具信息牌 數(shù) PIN- TOOLCHECK-DIGITAL,AILERONELEVATOR CHECKTOOL(OG)- LOAD,APPLICATIONTOOL-ELEVATOR,AILERON, PIN- <---材料信息

第2任務(wù)號(hào)/TASKNO:1機(jī)電工作任務(wù)27-24-00-200-001-警告:確保地面-鎖定就位在起落架上。CheckoftheRudderServoControlsandHingeBearingsfortoomuchyandConditionTASK27-24-00-200-001-WARNING:MAKESURETHATTHEGROUNDSAFETY-LOCKSAREINPOSITIONONTHELANDINGGEAR.WARNING:PUTTHESAFETYDEVICESANDTHEWARNINGNOTICESINPOSITIONBEFOREYOUSTARTATASKONORNEAR:THEFLIGHTTHEFLIGHTCONTROLTHELANDINGGEARANDTHERELATEDCOMPONENTSTHAT2機(jī)電工作準(zhǔn)備信息JobSet-up參 數(shù) 說(shuō)無(wú)規(guī) 可調(diào)工作平臺(tái)10m無(wú)規(guī) 按 警告A.Fixtures,Tools,TestandSupport No ACCESSTFORM10M(33FT)-No WARNINGB.參 名 第3任務(wù)號(hào)/TASKNO: **ONA/C001-049,051-099,101-149,151-199,201-249,251-299,301-501-509,511-540,551-557,601-657,701-PRESB27-1224forA/C001-005,051-063,101-109,151-160,201-240,251-301-315,351-355,401-405,451-455,501-509,511-540,551-557,601-651-657,701-705,751- 從黃 TSM27-20-00-810- B.Referenced EnergizetheAircraftElectricalCircuitstheExternal24-41-00-861-002-A-01EnergizetheAircraftElectricalCircuitsfromtheAPU24-41-00-861-002-A-02EnergizetheAircraftElectricalCircuitsfromEngineDe-energizetheAircraftElectricaldfromtheExternalDe-energizetheAircraftElectricaldfromtheDe-energizetheAircraftElectricaldfromtheEngine CheckoftheRudderTrailingEdge 第4任務(wù)號(hào)/TASKNO: RemovaloftheRudderServo CheckoftheRudderServoControlAttaents InstallationoftheRudderServoControl**ONA/C001-049,051-099,101-149,151-199,201-249,251-299,301-501-509,511-540,551-557,601-657,701-PRESB27-1224forA/C001-005,051-063,101-109,151-160,201-240,251-301-315,351-355,401-405,451-455,501-509,511-540,551-557,601-651-657,701-705,751- RecementoftheRudderServo-ControlBearings PressurizetheBlueHydraulicSystemwithaHydraulicGroundPower-29-10-00-863-003-A-01PressurizetheBlueHydraulicSystemwiththeElectric DepressurizetheBlueHydraulic PressurizetheGreenHydraulicSystemfromtheHydraulicSystemthroughthePTUwiththeElectricPump DepressurizetheGreenandYellowHydraulicSystemsafterOperationofthe PressurizetheYellowHydraulicSystemtheElectric DepressurizetheYellowHydraulic RemovaloftheHingeArmFittingsNo.1thruNo. InstallationoftheHingeArmFittingsNo.1thruNo.7 InspectionoftheRudderHingeLineFittings1to7for RemovalofRudderHingeBearingNo. InstallationofRudderHingeBearingNo.6TSM27-20-00-810-802 AirframeVibrationduetotheRudder3機(jī)電工作準(zhǔn)備JobSet-27-24-00-861-053-Subtask27-24-00-861-053-AA.Energizetheaircraftelectricalcircuits(參考.AMM.任務(wù)24-41-00-861-002).27-24-00-010-052-B.將可調(diào)工作平臺(tái)10M33FT)放置在325打開(kāi)檢查口蓋Subtask27-24-00-010-052- 第5任務(wù)號(hào)/TASKNO:B.GetPutanACCESSTFORM10M(33FT)-ADJUSTABLEinpositionatzoneOpentheaccessdoors325BL,325BR,325CL,325CR,325DL,325DR,325EL,27-24-00-860-050-C.飛機(jī)結(jié)增壓飛機(jī)系統(tǒng)(參考.AMM.任務(wù)29-23-00-863-001)(參考.AMM.任務(wù)29-24-00-863-001)(參考.AMM.任務(wù)29-10-00-863-003)。LEAKMEASUREMENTVALVES/B和LEAKMEASUREMENTVALVES/YOFF(3)在,在面板110VU,確保RUDTRIM指示器顯示0.Subtask27-24-00-860-050-AC.AircraftmaintenancePressurizetheaircrafthydraulicsystems(ref.AMM.任務(wù)29-23-00-863-001)(ref.AMM.任務(wù)29-24-00-863-001)(ref.AMM.任務(wù)29-10-00-863-003).OntheHYDsectionofthemaintenancepanel50VU-releasetheLEAKMEASUREMENTVALVES/BandLEAKVALVES/Ypushbuttonswitches(theOFFlegendsofthesepushbuttonswitchescomeon).Onthecenterpedestal,onthepanel110VU,makesurethattheRUDTRIMindicatorshows0.27-24-00-941-050-D.Subtask27-24-00-941-050-D.SafetyPutwarningnotice(s)onthepedals(CAPTandF/O)tolsnottooperatethem.Putwarningnotice(s)onthepanel110VUtolsnottousetheruddertrim.4機(jī)電工作步驟27-24-00-210-050-如能看到襯墊,更換相關(guān)伺服控制(參考.AMM.任務(wù)27-24-51-000-001)(參考.AMM.27-24-51-400- 第6任務(wù)號(hào)/TASKNO:或者鉸鏈臂端部接頭(157)(參考.AMM.55-36-41-000-001)(參考.AMM.任務(wù)55-36-41-400-001)任務(wù)參考.AMM55-46-11-400-001Subtask27-24-00-210-050-A.CheckoftheRudderServoControlsandHingeBearingsforGeneralMakesurethattherodsandbellcranksareinthecorrectMakesurethatthelinerisinthecorrectpositioninthehousingoftheballbearings(nomigrationoftheliner).NOTE:Thelinerisacoatofteflonbetweenthebearingcaseandtheball.Itletstheballturnwithaminimumoffriction(self-Ifyoucanseetheliner,recetherelatedservocontrol(Ref.AMM.TASK27-24-51-000-001)(Ref.AMM.TASK27-24-51-400-001)orhingearmendfitting(1to5or7)(Ref.AMM.TASK55-36-41-000-001)(Ref.AMM.TASK55-36-41-400-001)orhingebearingNo.6(Ref.AMM.TASK55-46-11-000-001)(Ref.AMM.TASK55-46-11-400-001).NOTE:Iftherod-endoftherudderservocontrolhasagreasenipple(regreasablerollerbearing):Thereisno**ONA/C001-049,051-099,101-149,151-199,201-249,251-299,301-501-509,511-540,551-557,601-657,701-PRESB27-1224forA/C001-005,051-063,101-109,151-160,201-240,251-301-315,351-355,401-405,451-455,501-509,511-540,551-557,601-651-657,701-705,751-27-24-00-220-050-B.而不是為了防止方向舵振動(dòng)的.如果在間隙小于16mm(0.6299in.)情況下，檢查方向舵后緣的間隙（參考.AMM.任務(wù)27-24-00-200-002） 間距超過(guò)16mm(0.6299in.):更換相應(yīng)方向舵伺服控制器(參考.AMM.任務(wù) (參考.AMM.任務(wù)27-24-51-400-001)或更換兩個(gè)方向舵伺服控制軸承(參考.AMM.任務(wù)27-24-51-960-001).檢查方向舵后緣的間隙（參考.AMM.任務(wù)27-24-00-200-002） 第7任務(wù)號(hào)/TASKNO:16mm(0.6299in.),檢查相應(yīng)的方向舵伺服控制器接頭(參考.AMM.任務(wù)27-24-51-200-001)。檢查方向舵后緣的間隙（參考.AMM.任務(wù)27-24-00-200-002） 仍超過(guò) (參考.AMM.任務(wù)55-46-00-200-001)。16mm(0.6299in.8mm(0.3150in.這個(gè)表面彎曲是30daN(67.4427lbf**ONA/C001-049,051-099,101-149,151-199,201-249,251-299,301-501-509,511-540,551-557,601-657,701-PRESB27-1224forA/C001-005,051-063,101-109,151-160,201-240,251-301-315,351-355,401-405,451-455,501-509,511-540,551-557,601-651-657,701-705,751-Subtask27-24-00-220-050-B.CheckoftheRudderTrailingEdgeNOTE:Formonitoringandfollowupoftheyattheruddertrailingedge,itis mendedthattheoperatorrecordinitsownationthevaluesNOTE:Theumyof16mm(0.6299in.)preventsmetal-to-metalcontactintheself-lubrificationbearingbutdoesnotalwayspreventruddervibration.Ifthereisruddervibrationwhentheyislessthan16mm(0.6299in.),refertotheprocedureforAirframeVibrationTSM27-20-00-810-802.Doacheckoftheruddertrailingedgey(Ref.AMM.TASK27-24-00-200-Foreachservocontrol(Green,YelloworBluehydraulicsystempressurized),ifthedistanceismorethan16mm(0.6299in.):(a)Recetherelatedrudderservocontrol(Ref.AMM.TASK27-24-51-000-Doacheckoftheruddertrailingedgey(Ref.AMM.TASK27-24-00-200-002).Foreachservocontrol(Green,YelloworBluehydraulicsystempressurized),ifthedistancestaysmorethan16mm(0.6299in.),doacheckoftherelatedservocontrolfitting(Ref.AMM.TASK27-24-51-200-Doacheckoftheruddertrailingedgey(Ref.AMM.TASK27-24-00-200-002).Foreachservocontrol(Green,YelloworBluehydraulicsystempressurized),ifthedistancestaysmorethan16mm(0.6299in.),doacheckoftherelatedrudderfitting(Ref.AMM.TASK55-46-00-200-NOTE:This16mm(0.6299in.)valueincludes8mm(0.3150 第8任務(wù)號(hào)/TASKNO:ofsurfacebendingastheresultofthe30daN(67.4427lbf)**ONA/C456-500,541-550,558-600,658-700,752-POSTSB27-1224forA/C001-005,051-063,101-109,151-160,201-240,251-301-315,351-355,401-405,451-455,501-509,511-540,551-557,601-651-657,701-705,751-Subtask27-24-00-220-050-B.而不是為了防止方向舵振動(dòng)的.如果在間隙小于16mm(0.6299in.)情況下，12mm(0.4724in8mm(0.3150in是30daN(67.4427lbf)力的結(jié)果.檢查方向舵后緣的間隙（參考.AMM.任務(wù)27-24-00-200-002） 對(duì)于每個(gè)伺服控制器（增壓的綠，黃或者藍(lán)系統(tǒng)），如果間距超過(guò)12(0.4724檢查相關(guān)方向舵裝置(Ref.AMMTASK55-46-00-200-001)再次檢查方向舵后緣的間隙(Ref.AMMTASK27-24-00-200-002)11mm如果間隙大于11mm0.4331(Ref.AMMTASK27-24-51-000-001(Ref.AMMTASK27-24-51-400-001)Ref.AMMTASK27-24-00-200-002)如果間隙大于11mm0.4331檢查相應(yīng)的伺服控制部件(RefAMMTASK27-24-51-200-001)**ONA/C456-500,541-550,558-600,658-700,752-POSTSB27-1224forA/C001-005,051-063,101-109,151-160,201-240,251-301-315,351-355,401-405,451-455,501-509,511-540,551-557,601-651-657,701-705,751-Subtask27-24-00-220-050-B.CheckoftheRudderTrailingEdgeNOTE:Formonitoringandfollowupoftheyattheruddertrailingedge,itis mendedthattheoperatorrecordinitsownationthevaluesmeasured.NOTE:Theumyof12mm(0.4724in.)preventsmetal-to-metalcontactintheself-lubricationbearingbutdoesnotalwayspreventrudderIfthereisruddervibrationwhentheyislessthan12mm(0.4724in.),refertotheprocedureforAirframeVibrationTSM27-20-00-810-802.NOTE:This12mm(0.4724in.)valueincludes8mm(0.3150in.)ofsurfacebendingastheresultofthe30daN(67.4427lbf).(1)Doacheckoftheruddertrailingedgey(Ref.AMMTASK27-24-00-200-002) 第9任務(wù)號(hào)/TASKNO:Foreachservocontrol(Green,YelloworBluehydraulicsystempressurized),ifthedistanceismorethan12mm(0.4724in.):Doacheckoftherelatedrudderhingefitting(Ref.AMMTASK55-46-00-200-001).Doagainacheckoftheruddertrailingedgey(Ref.AMMTASK27-24-00-200-002).NOTE:Theymustbedecreasedto11mmorless.Ifnot,itstaysaresidualclearancethatmustbedecreasedinthestepsthatfollow.Ifthedistancestaysmorethan11mm(0.4331recetherelatedrudderservo(Ref.AMMTASK27-24-51-000-001)and(Ref.AMMTASK27-24-51-400-001)Doagainacheckoftheruddertrailingedgey(Ref.AMMTASK27-24-00-200-002).Ifthedistancestaysmorethan11mm(0.4331Doacheckoftherelatedservocontrolfitting(Ref.AMMTASK27-24-51-200-001).5機(jī)電結(jié)束 Close27-24-00-942-052-A.(1)在面板50VU的HYD段LEAKMEASUREMENTVALVES/B和LEAKMEASUREMENT(參考.AMM.29-24-00-864-001).AMM29-10-00-864-003)Subtask27-24-00-942-052-A.Puttheaircraftbacktoitsini