个项目工卡ces smjc a320fam特别详细检查US中央翼盒十字形配件FR42处左右侧后梁

第2页共14页机号中文标题 特别详细检查(US)翼盒十字形配件，FR42处左右侧后CES-SMJC-A320FAM-571170-01-8- SpecialDetailedInspection(US)ofCenterWingBox,CruciformFitting,RearSparattheLevelofFrame42,LH/RH任务号Task571170-01-参参说无指No5M16FT)可调节工作平 TFORM5M(16FT)-参说无水清NonAqueousCleaner-General-不Textile-Cotton区域/接区域说ZONE空调舱和整流AIRCONDITONINGCOMPTAND空调舱和整流 第3页共14页机号CES-SMJC-A320FAM-571170-01-8-任务号Task571170-01-任务TASK57-10-00-220-006-**ONA/C:警告 使用消耗材料时须。遵守厂家说明与当地BECAREFULWHENYOUUSECONSUMABLEMATERIALS.OBEYTHEMATERIALMANUFACTURER'SINSTRUCTIONSANDYOURLOCALREGULATIONS.工作任务Reasonforthe(Ref:参考MPDTASK:571170-01(Ref:RefertotheMPDTASK:571170-01特别详细检查(US)翼盒十字形配件，FR42处左右侧后SPECIALDETAILEDINSPECTION(US)OFCENTERWINGBOX,CRUCIFORMFITTING,REARSPARATTHELEVELOFFR42,注意NOTE 本任务适用所有飞机。为了解该任务是否适用于本架飞机，可参见MPD中的适用性描述和SRM介绍部分中的重量变量数据。Theeffectivityofthistaskis"ALL".Toknowifthistaskisapplicableforyouraircraft,refertotheMPDtaskapplicabilityandtheweightvariantdatagivenintheSRMintroduction.工作准备信息JobSet-upFixtures,Tools,TestandSupportConsumableWorkZonesandAccess

机号

第4页共14页

CES-SMJC-A320FAM-571170-01-8-任务号Task571170-01-区域/接

区域说ZONEAIRCONDITONINGCOMPTAND

燃油燃油191DT191ET192DT191DT,191ET,192DT, Referenced参说(参考:53-35-11-000-001-(Ref:53-35-11-000-001-A拆卸机翼到机身整流RemovaloftheWing-to-Fuselage(参考:53-35-11-400-001-(Ref:53-35-11-400-001-A安装机翼到机身InstallationoftheWing-to-Fuselage(Ref:NTM571147(Ref:SRM511100)(Ref:SRM511100(纠正措施(forcorrective(Ref:SRM512200)(Ref:SRM512200(纠正措施(forcorrective(参考:翼盒-FR42处十字形配件后梁(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42(参考:翼盒-FR42处十字形配件后梁(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42(参考:翼盒-FR42处十字形配件后梁(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42(参考:翼盒-FR42处十字形配件后梁(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42 工作准备JobSet-工工作者/日检验员/日 第5页共14页机号CES-SMJC-A320FAM-571170-01-8-任务号Task571170-01-子任务Subtask57-10-00-010-084-**ONA/C:接Get将5M(16FT191和192PutanACCESSTFORM5M(16FT)-ADJUSTABLEinpositioninzones191and191DT191ET192DT192ET:53-35-11-000-001Removethewing-to-fuselagefairings191DT191ET192DTand192ET(Ref:53-35-11-000-001)子任务Subtask57-10-00-110-073-**ONA/C:PreparationoftheInspection**ONA/C:(参考:翼盒-FR42处十字形配件后梁**ONA/C:(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42**ONA/C:(参考:翼盒-FR42处十字形配件后梁**ONA/C:(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42**ONA/C:(参考:翼盒-FR42处十字形配件后梁**ONA/C:(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42**ONA/C:(参考:翼盒-FR42处十字形配件后梁**ONA/C:(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42 Cleantheinspectionareawith08BAA9NonAqueousCleaner-General--andalint-cottoncloth14SBA1Textile-LintCotton-,ifnecessary.MakesurethatthesurfaceoftheinspectionareaiscleanandDoavisualcheckoftheinspectionareafordamageorMakesurethatthereisCorrosion如果有腐蚀损伤,参考结构修理手册(Ref:SRM512200)进行分类,检查,去除和防腐蚀处理工工作者/日检验员/日 第6页共14页机号CES-SMJC-A320FAM-571170-01-8-任务号Task571170-01-Ifyoufindcorrosiondamage,refertotheStructuralRepairManual(Ref:SRM512200)fortypes,inspection,removalandcorrosionprotection.其它损伤(刮伤,裂纹,沟槽,凹痕,折痕等Otherdamage(scratches,cracks,gouges,dents,如果发现这种类型的损伤,根据结构修理手册(Ref:SRM511100)Ifyoufindthistypeofdamage,refertotheStructuralRepairManual(Ref:SRM511100)fordamageclassificationandcorrectiveaction.记录检查结果: 工作步骤子任务Subtask57-10-00-270-055-**ONA/C:检**ONA/C:(参考:翼盒-FR42处十字形配件后梁**ONA/C:(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42**ONA/C:(参考:翼盒-FR42处十字形配件后梁**ONA/C:(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42**ONA/C:(参考:翼盒-FR42处十字形配件后梁**ONA/C:(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42**ONA/C:(参考:翼盒-FR42处十字形配件后梁**ONA/C:(Ref:CenterWingBox-RearSparoftheCruciformFittingatFR42对翼盒十字形配件的后梁作特殊详细检查。本检查适用于FR42左右侧。参考无损探伤手册(Ref:NTM571147)。DoaspecialdetailedinspectionoftherearsparofthecruciformfittingoftheCenterWingBoxThisinspectionisapplicableatFR42,leftandrightsides.RefertotheNon-destructiveTestingManual(Ref:NTM571147).MakeareportofthedamageaftertheNDTCorrosion如果发现腐蚀损伤,参照结构修理手册(Ref:SRM512200)进行腐蚀定级,检查,去除和进行防腐保护Ifyoufinddamage,refertotheStructuralRepairManual(Ref:SRM512200)fortypesofcorrosion,inspection,removalandcorrosionprotection.其它损伤(刮伤,裂纹,沟槽,凹痕,折痕等Otherdamage(scratches,cracks,gouges,dents,工作者工作者/日检验员/日工作者/日检验员/日 第7页共14页机号CES-SMJC-A320FAM-571170-01-8-任务号Task571170-01-如果发现这种类型的损伤,根据结构修理手册(Ref:SRM511100)Ifyoufindthistypeofdamage,refertotheStructuralRepairManual(Ref:SRM511100)fordamageclassificationandcorrectiveaction.注意 如果在作NTM571147P.Block401检查时发现裂纹,在下次飞行前向空客报告IfyoufindcrackswhenyoudotheNTM571147P.Block401procedure,refertoAIRBUSbeforethesubsequentflight.记录检查结果: 子任务Subtask57-10-00-410-084-**ONA/C:Close确认工作区域清洁，所有工具和其他杂物已清除Makesurethattheworkareaiscleanandclearoftoolsandother191DT191ET192DTand192ET:53-35-11-400-001Installthewing-to-fuselagefairings191DT191ET192DTand192ET(Ref:53-35-11-400-001)Removetheaccess子任非例行工作单:Non-routinecard注意NOTE对实施工作中生成的非例行工作单，工作者应记录处理单号及相应的工序。完成的非例行工作单与本工作单卡一并保orNon-routinecardsfoundduringtheworkprocess,themechanicshouldnotedownthereport;Non-routinecardnumberandthecorrespondingworkprocedure.TheNon-routinecardshouldbekepttogetherwiththisgeneratingtaskcard."None"shouldbewrittenifnosuchreportsheetisgenerated.最终工作结论:Final 完成日期: 工工作者/日检验员/日 第8页共14页机号CES-SMJC-A320FAM-571170-01-8-任务号Task571170-01-CenterWingBox-RearSparoftheCruciformFittingat 第9页共14页机号CES-SMJC-A320FAM-571170-01-8-任务号Task571170-01-**ONA/C:CenterWingBox-RearSparoftheCruciformFittingat**ONA/C: 第10页共