WOHA33_2632230_801_EOA33-53-0047

Hong Kong Airlines Limited香港航空有限公司03110-01Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA332632_801_230适航指令(AD) 2632230TitleFuselage - Main Structure - Inspection of Cabin Compartment Parts Following Heat Treatment Non ConformityMcd&Rev/厂家工卡&修订日期标题机身-主结构-客舱件热处理状态不符检查A/C/飞机号/组别EO JC No./EO工卡EO JC Rev/工卡版本Workarea/工作区域Skill/工种Man Hour/工时BLNV/2EOA33-53-0047R02机身/AirframeAIRP/NDT01:00/06:00Baseline/依据Operator EO/营运人EOEO Rev/EO版本Work Type/工作类别Threshold/首检Interval/重复检ASB A330-53-3228R00,AD 2015-0212,CAD 2015-A330-01EOA33-HKG53-0035R02Written/编写Reviewed/审核Approved/批准2016-04-152016-04-152016-04-15Accomplished完工签署Complete Date完工日期Station维修站PVGREASON & DESCRIPTION/原因及描述空客质量控制认定一些没有经过热处理的材料可能已经进入了供应链。已执行关于受影响的疑似和/或实际不符合设计定义的飞机结构的详细安全评估。完成本EO将检测出受影响的部件Airbus quality control identified that items manufactured without heat treated material may have entered the supply chain. Detailed safety assessment of the impact on aircraft structure regarding suspected and/or actual non-conformance to design definition has been performed.Accomplishment of this EO will allow detection of the affected parts. R01改版原因/Reason for R01:1.根据AD要求修 改计划信息和工作步骤。Revise the plan information and work instructions as per AD requirement.2.升级本EO为AD控制。Upgrade this EO as AD control. R02改版原因/Reason for R02：飞机转租，增加BLNN飞机的适用性。Add the applicability of A/C BLNN due to aircraft sublease.TOOLS/工具TOOLS NECESSARY/必须工具ITEM项目P/N件号DESCRIPTION名称EQTP类型QTY数量APP适用性Conditions note互换信息及备注TOOLS IF NECESSARY/视情工具ITEM项目P/N件号DESCRIPTION名称EQTP类型QTY数量APP适用性Conditions note互换信息及备注PARTS AND MATERIAL/航材NOTE:OPERATOR MUST GET AND INSTALL THE PARTS THAT CORRESPOND TO THE RELATIVE WORKORDER NO.注释：请工作者严格按照工作指令号领取预定的航材装机PARTS AND MATERIAL NECESSARY/必须航材ITEM项目P/N件号DESCRIPTION名称EQTP类型QTY数量APP适用性Conditions note互换信息及备注1F5397460901451BRACKETAS1BLNV视情/On conditionPARTS AND MATERIALIF NECESSARY/视情航材ITEM项目P/N件号DESCRIPTION名称EQTP类型QTY数量APP适用性Conditions note互换信息及备注1F5397463600000BRACKETAS1BLNV视情/On condition2F5397463601000BRACKETAS1BLNV视情/On condition3F5397463622651BRACKETAS1BLNV视情/On condition4F5397605720000SECTIONAS1BLNV视情/On condition5F5397605720200SECTIONAS1BLNV视情/On condition6F5397605720400SECTIONAS1BLNV视情/On condition7F5397605720600SECTIONAS1BLNV视情/On condition8F5398903100051SUPPORTAS1BLNV视情/On condition9A2527036700051BRACKETAS1BLNV视情/On condition10A2527036700151BRACKETAS1BLNV视情/On condition11F5397460902051BRACKETAS1BLNV视情/On condition12F5398903300251SUPPORTAS1BLNV视情/On condition13F5398905700051SUPPORTAS1BLNV视情/On condition14G5397087601400BRACKETAS1BLNV视情/On condition15F5377055220451BRACKETAS1BLNV视情/On condition16F5397471500851BRACKETAS1BLNV视情/On condition17F5397471500951BRACKETAS1BLNV视情/On conditionIMPORTANT NOTE:In the event of any discrepancies between the Chinese instruction and the English instruction, the English procedure should prevail.Record Additional Work/Findings(If Applicable) Reference No. Certificate of Release to Service (* Tick as appropriate # Different crews should perform the work on each of the systems)Certifies that the work specified, except as otherwise specified, was carried out in accordance with HKAR-145and in respect to that work, The aircraft / aircraft components are considered ready for Release to Service. HKA Approval No: AI / 135 / 706 * HKE Approval No: AI /218/1215, JMM 133 * HNAT Approval No.: D.101115, JMM 047* CASL Approval No: AI / 101 / 798 * AMECO Approval No.: D.101131, JMM 001* HNAT- North West Approval No.: D.500023, JMM 049 * HAECO Approval No: DAI / 1 / 853 * SMECO Approval No.: D.400009, JMM 081* HNAT- YN Approval No.: D.4108, JMM 134 * TAECO Approval No.: DAI / 89 / 1295 * CEA Approval No.: D.200002, JMM 112 * HNAT Approval No.: D.3039, JMM 076 * THAECO Approval No.: D.101661, JMM 124 * CEA-Jiangsu Approval No.: D.200047, JMM 117 * SPRING Approval No.: D.200081, JMM 121 * SIAEC Approval No: AWI / 01 * STARCO Approval No.: D.200078,JMM 039* GAMECO Approval No.: D.300001, JMM 006* THAI Approval No.: AI / 147 / 0910 * Other: * Signature:_ Authorization No.:_ Date:_工卡Job card:EOA33-53-0047TITLEFuselage - Main Structure - Inspection of Cabin Compartment Parts Following Heat Treatment Non ConformityPerfInsp标题机身-主结构-客舱件热处理状态不符检查工作者检查者A. 通用信息/GENERAL警 告： 确认遵守所参考手册的所有警告和注意事项WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES.注 意： 遵守使线束和设备处于良好状态的警示信息。当执行设备维护、修理及改装时，尽可能地保持线束、电气设备及工组区域的洁净，执行下述要求：使用如塑料布、布匹等铺盖在上述设备上；经常性的去除线束、电气设备上的杂物及其他污染物。可减少安装电线时的污染和损伤。若污染,参照ESPM20-55-00处理。CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRINGIN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRSOR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTSAND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS:- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARYON WIRING AND COMPONENTS.- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL ANDOTHER CONTAMINATION.THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION ANDDAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.注 ： 当步骤中出现“refer to”字样时，工作者可参考地方当局批准的替代程序进行施工；当步骤中出现“in accordance with”字样时，必须按照工作步骤中所引用的文件要求施工。NOTE: When the words refer to are used and the operator has a procedure accepted by thelocalauthority he belongs to, the accepted alternative procedure can be used. Whenthe words in accordance with are used then the given procedure must be followed.注 ：手册名以缩写表示。NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.B. 标准施工/STANDARD PRACTICES1. 飞机区域的识别，参考AMM 06-20-00, Page Block 001。For the identification of zones, refer to AMM 06-20-00, Page Block 001.2. 飞机隔框的识别，参考AMM 06-31-53, Page Block 001。For Frame(FR) identification, refer to AMM 06-31-53, Page Block 001.C. 施工准备/PREPARATION1. 工作准备/Job Set-up注 ：在开始维护检查前，如下的项目必须作为基本飞机构型加以考虑：- 飞机地面停放在起落架上（起落架安全销和轮挡必须在起落架上安装到位）- 发动机关车，反推关闭并锁定- 飞机处于空机状态- 设置停留刹车- 飞机电路关断- 液压系统卸压- 到驾驶舱和客舱的接近门可用- 所有跳开关在闭合位置- 所有控制器在NORM, AUTO或OFF位置NOTE: The items given in this note shall be considered as the basic Aircraft configurationbefore you start a maintenance task:- Aircraft on the ground resting on landing gear (the ground safety locks and the wheelchocks are in position on the landing gear)- Engine shut down, thrust reversers closed and locked- Aircraft in clean configuration- Parking brake applied- Aircraft electrical network de-energized- Hydraulic systems depressurized- Access to the cockpit and cabin is available- All circuit breakers are in closed position- All controls in NORM, AUTO or OFF position.a. 在工作区域下部放置接近平台。Put an access platform in position below the work areas.b. 参考AMM Task 12-34-24-860-802 保证飞机接地。Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802.c. 如果需要，可额外拆下接近所需的部件。如果不需拆下某些部件也可实现接近，可不用拆下这些部件。必须遵守顶升的限制。If it is necessary to remove more parts for access, you can remove those parts. If you can get access without removing identified parts, it is not necessary to remove all of the identified parts. Jacking and shoring limitations must be observed. D. 施工步骤/PROCEDURE1. 对客舱行李架前部执行涡流电导率测试。Do an Eddy Current Conductivity Measurement of the Forward Cabin Overhead Compartmenta. 参考Fig. A-GBAAB Sheet 01, Fig. A-GBAAB Sheet 02, Fig. A-GBBAB Sheet 01, Fig. A-GBBAB Sheet 02, Fig. A-GBBAB Sheet 03, Fig. A-GBCAA Sheet 01, Fig. A-GBDAA Sheet 01,附录1-铝合金热处理后涡流电导率测试和附录2-更换件，对涉及的区域所安装的结构件执行涡流电导率测量。Do the Eddy Current Conductivity Test of the installed structural parts in the involved areas, refer to Fig. A-GBAAB Sheet 01, Fig. A-GBAAB Sheet 02, Fig. A-GBBAB Sheet 01, Fig. A-GBBAB Sheet 02, Fig. A-GBBAB Sheet 03, Fig. A-GBCAA Sheet 01, Fig. A-GBDAA Sheet 01, Appendix 01 - Assessment for Heat Treatment Using Eddy Current Conductivity Measurement (COT) on Aluminum Alloys and Appendix 02 - Replacement Parts .注 ：使用探头直接接近扁平区域进行检查。NOTE: The inspection requires direct access to a flat area of the part with a probe.1) 若测量值小于22 MS/m或者小于37.9% IACS，执行步骤E：If measured value 22 MS/m or 37.9% IACS,perform procedure E.2) 若测量值大于26 MS/m或者大于44.8% IACS，更换部件。If measured value 26 MS/m or 44.8% IACS, replace parts.3) 若发现其他测量值，请检查NDT 工具并重新测量，若仍保持此测量值，联系结构工程师。If other measured value found, please check ndt tool and perform new measurement. if measured value is confirmed, please contact structure engineer.2. 对后客舱顶部执行涡流电导率测试。Do an Eddy Current Conductivity Measurement of the Aft Cabin Overhead Compartmenta. 参考Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02，附录1-铝合金热处理后涡流电导率测试和附录2-更换件，对涉及的区域所安装的结构件执行涡流电导率测量。Do the Eddy Current Conductivity Test of the installed structural parts in the involved areas, refer to Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02, Appendix 01 - Assessment for Heat Treatment Using Eddy Current Conductivity Measurement (COT) on Aluminum Alloys and Appendix 02 - Replacement Parts .注 ：使用探头直接接近扁平区域进行检查。NOTE: The inspection requires direct access to a flat area of the part with a probe.1) 若测量值小于22 MS/m或者小于37.9% IACS，执行步骤E：If measured value 22 MS/m or 37.9% IACS,perform procedure E.2) 若测量值大于26 MS/m或者大于44.8% IACS，更换部件。If measured value 26 MS/m or 44.8% IACS, replace parts.3) 若发现其他测量值，请检查NDT 工具并重新测量，若仍保持此测量值，联系结构工程师。If other measured value found, please check ndt tool and perform new measurement. if measured value is confirmed, please contact structure engineer.3. 对后客舱功能区执行涡流电导率测试。Do an Eddy Current Conductivity Measurement of the Aft Cabin Utility Areaa. 参考Fig. A-GBFAA Sheet 01，附录1-铝合金热处理后涡流电导率测试和附录2-更换件，对涉及的区域所安装的结构件执行涡流电导率测量。Do the Eddy Current Conductivity Test of the installed structural parts in the involved areas, refer to Fig. A-GBFAA Sheet 01, Appendix 01 - Assessment for Heat Treatment Using Eddy Current Conductivity Measurement (COT) on Aluminum Alloys and Appendix 02 - Replacement Parts .注 ：使用探头直接接近扁平区域进行检查。NOTE: The inspection requires direct access to a flat area of the part with a probe.1) 若测量值小于22 MS/m或者小于37.9% IACS，执行步骤E：If measured value 22 MS/m or 37.9% IACS,perform procedure E.2) 若测量值大于26 MS/m或者大于44.8% IACS，更换部件。If measured value 26 MS/m or 44.8% IACS, replace parts.3) 若发现其他测量值，请检查NDT 工具并重新测量，若仍保持此测量值，联系结构工程师。If other measured value found, please check ndt tool and perform new measurement. if measured value is confirmed, please contact structure engineer. D. 结束工作/Close-up1. 填写附录3 的反馈单并发送给“TS 结构科” （ ） 和“ 适航评估科”（Ae_ ）Fill the Appendix 3 of feedback form and send to and Ae_ .2. 确保工作区域清洁，没有其他设备或工具残留。Make sure that the work areas are clean and clear of tools and other items of equipment.3. 拆下接近平台。Remove the access platforms.4. 恢复飞机至正常可用状态。Put the aircraft back to its initial configuration. 附录 03 / Appendix 03技术文件反馈单/Technical Feedback Form工程师填写以下内容/Engineer fill in：技术文件号/Technical document numberEOA33-CHH53-0035EOA33-HKG53-0035技术文件标题/Technical document title机身-主结构-客舱件热处理状态不符检查Fuselage - Main Structure - Inspection of Cabin Compartment Parts Following Heat Treatment Non Conformity所需反馈信息/Feedback information检查结果/Inspection result反馈对象/Feedback object 技术服务部结构科/ Engineering Management Center, TSD, HNAT 适航评估科 / Airworthness Evaluation, QMD, HNAT反馈途径/Feedback way发送邮件到TS结构科/Sent to 发送邮件到适航评估科Ae_ /Sent to Ae_反馈目的/Feedback purpose TS据此收集数据/ TSD accordingly to gather data工作者填写以下内容/ Mechanic fill in：反馈记录单/ Feedback Form飞机号/AC： 工作者/ Mechanic：日期/Date：检查结果Inspection Result项目/ Item件号/ PN.区域/ Zone位置/Location电导率测量/COT 换件/Replace Part1F5397460901400 230FR22 STGR3LH (REFER TO FIG AGBAAB, SHEET 01)是/YES 否/NO 2FR26 STGR12LH STGR13LH (REFER TO FIG AGBAAB, SHEET 02)是/YES 否/NO 4FR26 STGR12RH STGR13RH (REFER TO FIG AGBAAB, SHEET 02)是/YES 否/NO 6F5397460902001230FR26.4 STGR1LH STGR2LH (REFER TO FIG AGBAAB, SHEET 02)是/YES 否/NO 7F5397463600000230FR25 STGR4LH STGR5LH (REFER TO FIG AGBBAB, SHEET 02)是/YES 否/NO 8FR26.1 STGR3LH STGR4LH (REFER TO FIG AGBBAB, SHEET 03)是/YES 否/NO 9FR26.3 STGR3LH STGR4LH (REFER TO FIG AGBBAB, SHEET 03)是/YES 否/NO 12F5397463601000230FR20 STGR2LH STGR3LH (REFER TO FIG AGBBAB, SHEET 02)是/YES 否/NO 13FR20 STGR3LH STGR4LH (REFER TO FIG AGBBAB, SHEET 02)是/YES 否/NO 14FR19 STGR2LH STGR3LH (REFER TO FIG AGBBAB, SHEET 02)是/YES 否/NO 15FR19 STGR2RH STGR3RH (REFER TO FIG AGBBAB, SHEET 02)是/YES 否/NO 16FR20 STGR3RH STGR4RH (REFER TO FIG AGBBAB, SHEET 02)是/YES 否/NO 17FR20 STGR1LH STGR1RH (REFER TO FIG AGBBAB, SHEET 02)是/YES 否/NO 18FR22 STGR3RH STGR4RH (REFER TO FIG AGBBAB, SHEET 03)是/YES 否/NO 19FR24 STGR3RH STGR4RH (REFER TO FIG AGBBAB, SHEET 03)20F5397463622600230FR18 FR19 STGR5RH (REFER TO FIG AGBBAB, SHEET 02)是/YES 否/NO 21FR18 FR19 STGR7RH (REFER TO FIG AGBBAB, SHEET 01)是/YES 否/NO 22FR18 FR19 STGR7LH (REFER TO FIG AGBBAB, SHEET 01)是/YES 否/NO 23FR18 FR19 STGR8LH (REFER TO FIG AGBBAB, SHEET 01)是/YES 否/NO 24F5397471500800230FR26.1 FR26.2 STGR13LH STGR14LH (REFER TO FIG AGBCAA, SHEET 01)是/YES 否/NO 25F5397471500900230FR26.1 FR26.2 STGR13RH STGR14RH (REFER TO FIG AGBCAA, SHEET 01)是/YES 否/NO 30F5397605720000230FR20 STGR8LH STGR9LH (REFER TO FIG AGBDAA, SHEET 01)是/YES 否/NO 29FR20 STGR6RH STGR7RH (REFER TO FIG AGBDAA, SHEET 01)是/YES 否/NO 35F5397605