WOHA33_4846178_147_EOA33-53-0039

Hong Kong Airlines Limited香港航空有限公司F-D-099Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA334846_147_178AD 4846178Training and Qualification/培训和资格Technical Record/技术记录NONEADTitleFuselage - Main Structure - Inspection of Cargo Parts Following Material Non ConformityMcd&Rev/厂家工卡&修订日期标题机身-主结构-货舱使用不合格材料制造的部件的检查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BLHD/1EOA33-53-0039R06机身/AirframeAIRP /NDT50:00/05:00Baseline/依据Operator EO/营运人EOR06Work Type/工作类别Threshold/首检Interval/重复检ASB A330-53-3261/R01,AD 2017-0021,CAD 2017-MULT-09EOA33-HKG53-0030Written/编写Reviewed/审核Approved/批准2017-11-072017-11-142017-11-21Accomplished完工签署Complete Date完工日期Station维修站SHAREASON & DESCRIPTION/原因及描述空客质量控制部门发现使用错误的铝合金或者错误的热处理制造的部件进入了供应链。已对被怀疑的结构和/或确切的不合格设计定义进行详细的评估，对于宽 体机项目飞机，460架飞机的11个件号有潜在影响。因此下发此EO对不合格部件 进行检查并采取相关纠正措施。AIRBUS quality control identified that items manufactured with wrong aluminium alloy or wrong heat treatment may have entered the supply chain. Detailed assessment of the impact on aircraft structure of suspected and/or actual non conformance to design definition has been performed. For the Long Range program this is 11 Part Numbers (PNs) for 460 aircraft that are potentially affected. So issue this EO to perform inspection and do relative corrections. R01改版原因/Reason of R01：1. 依据文件中增加AD 2015-0206/CAD 2015-MULT-54。 Add AD 2015-0206/CAD 2015-MULT-54 to the SOURCE.2. 依 据AD 2015-0206/CAD 2015-MULT-54修改计划安排。 Revise PLAN according to AD 2015-0206/CAD 2015-MULT-54.R02改版原因/Reason for R02： 飞机引进，增加BLNN飞机的适用性。Add the applicability of A/C BLNN due to aircraft delivery.R03改版原因/Reason for R03：飞机引进，增 加BLNR、BLNS、BLNT和BLNU飞机的适用性。Add the applicability of A/C BLNR, BLNS, BLNT, BLNU due to aircraft delivery. R04改版原因/Reason for R04：1.修改依据文件，从SB A330-53-3261R00改为SB A330-53-3261R01.Revise the Source from SB A330-53-3261R00 to SB A330-53-3261R01.2.依据SB A330-53-3261R01，增加附加工作。Add additional work, according to SB A330-53-3261R01.3.依据SB A330-53-3261R01，修改施工步骤，更新附图。Revise work instructions and figures, according to SB A330-53-3261R01.4.依据SB A330-53-3261R01，将航材G5367131300000、G5367173700000、G5367173800000数量修改为8个，删除航材F5397096620200。Revise G5367131300000、G5367173700000、G5367173800000 quantity to 8, delete F5397096620200, according to SB A330-53-3261R01.5.依据SB A330-53-3261R01 ，修改EO计划信息。Revise EO plan information, according to SB A330-53-3261R01. R05改版原因/Reason of R05：1.更新AD依据文件，将AD2015-0206更新为AD2017-0021。Update AD references, revise AD2015-0206 to AD2017-0021.2.依据AD2017-0021修改计划信息。Revise plan information according to AD2017-0021.版本变化/REVISION改版原因/REASON修改内容/CHANGE DESCRIPTIONR05-R06BLHD飞机引进。A/C BLHD importing.增加BLHD飞机的适用性。Add the applicability of A/C BLHD.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PARTS 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1F5347170420400STRAPAS2ALL视情/On condition2F5347170420600STRAPAS1ALL视情/On condition3F5377004320351BEAMAS1ALL视情/On condition4G5367131300000SHEETAS8ALL视情/On condition5G5367173700000PLATEAS8ALL视情/On condition6G5367173800000PLATEAS8ALL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:_EOA33-53-0039 R06 W/O:4846 AC:BLHD页码：34 / 34工卡Job card:EOA33-53-0039TITLEFuselage - Main Structure - Inspection of Cargo Parts Following Material Non ConformityPerfInsp标题机身-主结构-货舱使用不合格材料制造的部件的检查工作者检查者警 告：必须遵守相关程序中的所有警告和注意。WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES注 意： 始终遵守预防措施确保电线处于可用状态（电气性和机械性均可用）。执行维护，修理或改装时，始终保持电缆，部件和工作区域清洁。执行下列工作：-利用塑料布，抹布对线缆和部件进行保护-定期清除碎屑，不需要的材料和其他污染物。这些预防措施可以降低对电线污染和损害风险。如果污染，参考ESPM 20-55-00CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS:- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; ASNECESSARY ON WIRING AND COMPONENTS.- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION.THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATIONAND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.注 释：本EO的施工步骤包含其他文件或本EO其他区域的程序。当出现“参考”（refer to）字样时，工作者可使用当地局方可接受的程序作为替代程序。当出现“按照”（in accordance with）字样时，必须按照规定的步骤执行。NOTE: The accomplishment instructions of this EO include procedures given in other documents or in other sections of the EO. When the words refer to are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words in accordance with are used then the given procedure must be followed.注 释：接近和关闭步骤不包含返回使用测试，在本EO中，不构成或影响本EO的技术意图。因此，只要本EO的技术意图符合设定的参数，工作者可以视情况忽略或增加接近和/或关闭步骤以增加维修工作的灵活性。NOTE: The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters.注 释：施工步骤中的手册名以缩写表示。NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.注 释：本EO被或即将被适航指令（AD）定义为强制执行。施工步骤中的段落C为符合性要求（RC）且必须被严格执行以符合AD。其他段落为推荐执行，可以被偏离，即作为其他工作的一部分来执行，或使用异于EO中所给步骤的其他方法执行，只要保证RC段落被执行且飞机可以被恢复至可运营状态。NOTE: This EO is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs C. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the EO, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition.注 释：报废的零件须由工作者妥善处理。NOTE: Discarded parts must be managed at the operators discretion.注 释：本EO包含确保飞机持续适航性的必需机上维护工作说明。对于发生的偏离情况，联系结构工程师获取进一步指示。NOTE: This EO contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft. For any deviations to the instructions contained herein, contact structure engineer for further instructions and approval.A. 通用信息/GENERAL1. 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. 隔框（FR）的识别，参考AMM 06-31-53, Page Block 001。For Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.3. 接近盖板的识别，参考AMM 06-41-53, Page Block 001。For the identification of access panels, refer to AMM 06-41-53, Page Block 001.B. 准备工作/PREPARATION1. 工作准备/Job Set-up注释：在开始维护工作前以下项目必须作为基础构型加以考虑：-发动机关闭，反推关闭并锁住-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-驾驶舱和客舱可接近-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 configuration before you start a maintenance task:- 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. 确保飞机电源接地，参考AMM Task 12-34-24-860-802.Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802.b. 放置接近平台到位：货舱门下方。Put an access platform in position below the Cargo Compartment Doors.c. 按需拆除/打开接近。Remove/open for access.C. 施工步骤/PROCEDURE注释 1： 未执行过依据SB A330-53-3261R00编写的EO的飞机不需执行第二部分，只需执行第一部分。Note 1： For aircracft which has not been accomplished the EO in according with SBA330-53-3261R00, no need to take measure for Part II，perform Part I only.注释2： 执行过依据SB A330-53-3261R00编写的EO，且在附录2中需要检查Item 6- Section 15、或Item 7或Item 8的飞机不需再执行第一部分，只需执行第二部分。Note 2： No more work for Part I is necessary for aircraft which has been accomplished the EO In according with A330-53-3261R00, and need to check Item 6-Section 15 or Item 7 or Item 8 according to Appendix 2, perform Part II noly.注释 3：执行过依据SB A330-53-3261R00编写的EO，但在附录2中无需检查Item 6-Section 15、和Item 7和Item 8的飞机无需再执行本EO（包括第一部分和第二部分）。Note 3： For aircracft which has been accomplished the EO in according with SB A330-53-3261R00, but no need to check Item 6-Section 15 and Item 7 and Item 8 according to Appendix 2, no need to perform this EO again（including Part I & II）.注释 4： 执行本EO前，请同PPD确认EO版本状态。Note 4： Please consult PPD to verify the status of revision of this EO before performing this EO.第一部分/Part I: （未执行过依据SB A330-53-3261R00编写EO的飞机/For aircraft which has not been accomplished the EO in according with SB A330-53-3261R00）1. 在FR72处执行涡流电导率测量Do an Eddy Current Conductivity Measurement at FR72a. 对在相关区域安装的结构件进行涡流电导率测量，参考Fig. A-GFAAA Sheet 01, Fig. A-GFAAA Sheet 02, Fig.A-GRAAA Sheet 01, Fig. A-GRAAA Sheet 02, Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02, Appendix01 - Assessment for Wrong Material using Eddy Current Conductivity Measurement(COT) on Aluminum Alloys,Appendix 02 - Effectivity By Part Number and Appendix 03 - Replacement Parts.Do the Eddy Current Conductivity Measurement of the installed structural parts in the involved areas,refer to Fig. A-GFAAA Sheet 01, Fig. A-GFAAA Sheet 02, Fig.A-GRAAA Sheet 01, Fig. A-GRAAA Sheet 02, Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02, Appendix01 - Assessment for Wrong Material using Eddy Current Conductivity Measurement(COT) on Aluminum Alloys,Appendix 02 - Effectivity By Part Number and Appendix 03 - Replacement Parts .注释：探头需要垂直于部件的平坦区域。NOTE: The inspection requires direct access to a flat area of the part with a probe.注释：流程图给出检查错误部件的指南。NOTE: The flow chart gives instructions to detect wrong parts.(1) 如果没发现不合格部件：If you have no findings:（a）完成并发送检查报告页至TS结构科（），参考Fig. A-GRAAA Sheet 01 和 Fig. A-GRAAA Sheet 02.Complete and send the Report Sheet to TS Structure Office（）, refer to Fig. A-GRAAA Sheet 01 and Fig. A-GRAAA Sheet 02.（b）无需进一步措施No further action.(2) 如果发现不合格部件：If you have findings:(a) 联系结构工程师，获取航材信息，然后更换部件，参考Appendix 03 - Replacement Parts，按照 SRM 51-72-11。Contact structure engineer for spare information, then replace parts, refer to Appendix 03 - Replacement Parts , in accordance with SRM 51-72-11.(b) 完成并发送检查报告页至TS结构科（），参考Fig. A-GRAAA Sheet 01 和 Fig. A-GRAAA Sheet 02.Complete and send the Report Sheet to TS Structure Office（）, refer to Fig. A-GRAAA Sheet 01 and Fig. A-GRAAA Sheet 02.(c) 无需进一步措施No further action.记录检查结果/Record inspection result_2. 在FR73到FR76处执行涡流电导率测量Do an Eddy Current Conductivity Measurement at FR73 to FR76a. 对在相关区域安装的结构件进行涡流电导率测量，参考Fig. A-GFAAA Sheet 01, Fig. A-GFAAA Sheet 02, Fig.A-GRAAA Sheet 01, Fig. A-GRAAA Sheet 02, Fig. A-GBBAA Sheet 01, Appendix01 - Assessment for Wrong Material using Eddy Current Conductivity Measurement(COT) on Aluminum Alloys,Appendix 02 - Effectivity By Part Number and Appendix 03 - Replacement Parts.Do the Eddy Current Conductivity Measurement of the installed structural parts in the involved areas,refer to Fig. A-GFAAA Sheet 01, Fig. A-GFAAA Sheet 02, Fig.A-GRAAA Sheet 01, Fig. A-GRAAA Sheet 02, Fig. A-GBBAA Sheet 01, Appendix01 - Assessment for Wrong Material using Eddy Current Conductivity Measurement(COT) on Aluminum Alloys,Appendix 02 - Effectivity By Part Number and Appendix 03 - Replacement Parts .注释：探头需要垂直于部件的平坦区域。NOTE: The inspection requires direct access to a flat area of the part with a probe.注释：流程图给出检查错误部件的指南。NOTE: The flow chart gives instructions to detect wrong parts.(1) 如果没发现不合格部件：If you have no findings:（a）完成并发送检查报告页至TS结构科（），参考Fig. A-GRAAA Sheet 01 和 Fig. A-GRAAA Sheet 02.Complete and send the Report Sheet to TS Structure Office（）, refer to Fig. A-GRAAA Sheet 01 and Fig. A-GRAAA Sheet 02.（b）无需进一步措施No further action.(2) 如果发现不合格部件：If you have findings:(a) 联系结构工程师，获取航材信息，然后更换部件，参考Appendix 03 - Replacement Parts，按照 SRM 51-72-11。Contact structure engineer for spare information, then replace parts, refer to Appendix 03 - Replacement Parts, in accordance with SRM 51-72-11 .(b) 完成并发送检查报告页至TS结构科（），参考Fig. A-GRAAA Sheet 01和Fig. A-GRAAA Sheet 02.Complete and send the Report Sheet to TS Structure Office（）, refer to Fig. A-GRAAA Sheet 01 and Fig. A-GRAAA Sheet 02.(c) 无需进一步措施No further action.记录检查结果/Record inspection result_3. 在地板处执行涡流电导率测量Do an Eddy Current Conductivity Measurement at Floor Panelsa. 对在相关区域安装的结构件进行涡流电导率测量，参考Fig. A-GFAAA Sheet 01, Fig. A-GFAAA Sheet 02, Fig.A-GRAAA Sheet 01, Fig. A-GRAAA Sheet 02, Fig. A-GBDAA Sheet 01, Appendix01 - Assessment for Wrong Material using Eddy Current Conductivity Measurement(COT) on Aluminum Alloys,Appendix 02 - Effectivity By Part Number and Appendix 03 - Replacement Parts.Do the Eddy Current Conductivity Measurement of the installed structural parts in the involved areas,refer to Fig. A-GFAAA Sheet 01, Fig. A-GFAAA Sheet 02, Fig.A-GRAAA Sheet 01, Fig. A-GRAAA Sheet 02, Fig. A-GBDAA Sheet 01, Appendix01 - Assessment for Wrong Material using Eddy Current Conductivity Measurement(COT) on Aluminum Alloys,Appendix 02 - Effectivity By Part Number and Appendix 03 - Replacement Parts .注释：探头需要垂直于部件的平坦区域。NOTE: The inspection requires direct access to a flat area of the part with a probe.注释：流程图给出检查错误部件的指南。NOTE: The flow chart gives instructions to detect wrong parts.注释：Appendix 02给出根据飞机MSN号，在不同区域安装在地板上的部件件号。使用Appendix 02定位相关项目。NOTE: The part numbers given in Appendix 02 are attached to the floorboards in different sections of the aircraft depending on MSN. Use Appendix 02 to locate the relevant items.(1) 如果没发现不合格部件：If you have no findings:（a）完成并发送检查报告页至TS结构科（），参考Fig. A-GRAAA Sheet 01 和Fig. A-GRAAA Sheet 02.Complete and send the Report Sheet to TS Structure Office（）, refer to Fig. A-GRAAA Sheet 01 and Fig. A-GRAAA Sheet 02.（b）无需进一步措施No further action.(2) 如果发现不合格部件：If you have findings:(a) 联系结构工程师，获取航材信息，然后更换部件，参考Appendix 03 - Replacement Parts，按照SRM 51-72-11。Contact structure engineer for spare information, then replace parts, refer to Appendix 03 - Replacement Parts , in accordance with SRM 51-72-11.(b) 完成并发送检查报告页至TS结构科（），参考Fig. A-GRAAA Sheet 01 和 Fig. A-GRAAA Sheet 02.Complete and send the Report Sheet to TS Structure Office（）, refer to Fig. A-GRAAA Sheet 01 and Fig. A-GRAAA Sheet 02.(c) 无需进一步措施No further action.记录检查结果/Record inspection result_第二部分/Part II: （执行过依据SB A330-53-3261R00编写的EO的飞机，且依据附录2需检查Item 6-Section 15或Item 7或Item 8 的飞机 / For aircraft which has been accomplished the EO in according with SB A330-53-3261R00, and need to check Item 6-Section 15 or Item 7 or Item 8 according to Appendix 2）1. 在地板处执行涡流电导率测量Do an Eddy Current Conductivity Measurement at the Floor Panels Section 15a. 对在相