WOHA33_17264C482_539_EOA33-57-0014

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WOHA331726_539_4821726482TitleWing-Flap-Inspection of Flap Parts Following Material Non ConformityMcd&Rev/厂家工卡&修订日期标题大翼-襟翼-襟翼部件材料不符检查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BLNZ/1EOA33-57-0014R01机翼/WingAIRP/NDT/SMTL02:00/00:30/02:00Baseline/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 A330-57-3120R00EOA33-HKG57-0008R01Written/编写Reviewed/审核Approved/批准2016-02-252016-03-232016-03-25Accomplished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使用了错误的铝合金或者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 with wrong aluminium alloy or without heat treatment 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. Accomplishment of this EO will allow detection of the affected parts. R01改版原因/Reason for R01：二手飞机引进，增加BLNN飞机的适用性。Add the applicability of A/C BLNN due to used aircraft importing.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1CML08BAA9SOLVENT GENERAL PURPOSECH1ALL数量按需/Quantity as required2CML14SBA1CLEANING ABSORCH1ALL数量按需/Quantity as required3CML04EAC2ANTI-CORROSION PRIMER (POLYURETHANE)CH1ALL数量按需/Quantity as required4G5757123020000PLUGAS10ALLN/A5CML04JMF1TOPCOATCH1ALL数量按需/Quantity as requiredPARTS 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IMPORTANT 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 * HNAT Approval No.: JMM 076, D3039 * HNAT Approval No.: JMM 047, D101115* HNAT Approval No.: JMM 049, D500023 * CASL Approval No: AI / 101 / 798 * TAECO Approval No.: DAI / 89 / 1295 * HAECO Approval No: DAI / 1 / 853 * SIAEC Approval No: AWI / 01 * STARCO Approval No.: JMM 039, D.200078 * SMECO Approval No: JMM 081, D.400009 * AMECO Approval No.: JMM001,D.101131* Other: * Signature:_ Authorization No.:_ Date:_工卡Job card:EOA33-57-0014TITLEWing-Flap-Inspection of Flap Parts Following Material Non ConformityPerfInsp标题大翼-襟翼-襟翼部件材料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 CAUTIONSINCLUDED 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.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. 将接近平台放置于左右内襟翼下部。Put an access platform in position below the inboard flap LH and RH.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. 参考AMM Task 27-50-00-866-802，完全收回襟翼。Fully retract the flaps, refer to AMM Task 27-50-00-866-802.d. 在襟翼控制杆上放置警告牌，禁止任何人操控襟翼/缝翼。Put the warning notices in position on the flap levers to tell persons not to operate the flap/slat controls.D. 施工步骤/PROCEDURE1. 制作新检查孔（左右侧）。Make New Inspection Holes (LH and RH Wing).注 ：以下程序步骤同时适用于左右大翼。NOTE: These instructions are applicable to both the Left Hand (LH) and Right Hand (RH) wings.a. 为检查接近需要而制作检查孔。In order to allow access for the inspection it is necessary to make new inspection holes.注 意： 当钻新孔时，务必当心不要损伤到此结构的其他部件。CAUTION: TAKE CARE WHEN DRILLING THE NEW HOLE THAT YOU DO NOT DAMAGE OTHER PARTS OF THE STRUCTURE.1) 如图Fig. A-GDAAA Sheet 01所示，在左右大翼6号和7号肋之间，襟翼下表面小心的钻3个孔，直径为11-11.20mm（0.433-0.441in.）。Between Ribs 6 and 7 LH/RH carefully drill three holes 11.00 mm to 11.20 mm (0.433 in. to 0.441 in.) diameter in the Flap Lower Skin, as shown on figure Fig. A-GDAAA Sheet 01.2) 对孔两侧去毛刺。Deburr both sides of the holes.3) 去除襟翼内的所有金属屑/钻屑。Remove all swarf/drilling chips from inside the flap.4) 清洁工作区域使用：Clean the work area.Use：5) 如果需要，参考AMM Task 51-75-12-300-801或者AMM Task 51-75-12-300-802修复漆层。修复面漆和底漆。使用：If necessary, repair the paint finish. Repair top coat and primer, refer to AMM Task 51-75-12-300-801 or AMM Task 51-75-12-300-802. Use:注 ：若仅损伤面漆，则仅需要修复面漆。Note：If top coat damaged only，repair top coat only.b. 对左右大翼6号和7号肋之间内襟翼桁条联接处11-19位置执行涡流电导率测量。Do an Eddy Current Conductivity Measurement of the Inboard Flap Stringer Coupling 11 - 19 Between Rib 6 and 7 (LH and RH Wing)注 ：以下程序步骤同时适用于左右大翼。NOTE: These instructions are applicable to both the Left Hand (LH) and Right Hand (RH) wings.1) 参考Fig. A-GBAAA Sheet 01，附录01-左右大翼内襟翼6号和7号肋之间桁条联接处错误热处理状态涡流电导率测量评估，附录2-受影响MSN MSN/SN/件号，对在受影响区域安装的结构件执行涡流电导率检查。Do the Eddy Current Conductivity Measurement of the installed structural parts inthe involved areas, refer to Fig. A-GBAAA Sheet 01, Appendix 01 - Assessment for Wrong Heat Treatment using Eddy Current Conductivity Measurement (COT) on Stringer Coupling Between Rib 6 and Rib 7, Inboard Flap, LH/RH and Appendix 02 - Effectivity by MSN/SN/Part Number .注 ：检查要求探头能直接到达部件的平面区域。NOTE: The inspection requires direct access to a flat area of the part with a probe.a) 若测量值大于25.5 MS/m 或者大于44% IACS，联系结构工程师。If measured value 25.5 MS/m or 44% IACS, contact structure engineer.(11号桁条/STGR 11) 测量值 / Measured value:_(12号桁条/STGR 12) 测量值 / Measured value:_(13号桁条/STGR 13) 测量值 / Measured value:_(14号桁条/STGR 14) 测量值 / Measured value:_(15号桁条/STGR 15) 测量值 / Measured value:_(16号桁条/STGR 16) 测量值 / Measured value:_(17号桁条/STGR 17) 测量值 / Measured value:_(18号桁条/STGR 18) 测量值 / Measured value:_(19号桁条/STGR 19) 测量值 / Measured value:_b) 否则，执行步骤D.c。If not , perform procedure D.c.c. 标记/Marking1) 完成检查和所有措施以后，参考PMS 01-06-12，在襟翼上使用不可擦油性笔写下SB号A330-57-3120。After inspection and completion of all actions write this Service Bulletin number A330-57-3120adjacent to the existing identification label on the flap, refer to Process and MaterialSpecification (PMS) 01-06-12. Use: Indelible Ink MarkerE. 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. 遮盖原有及新检查孔，安装：Cover the existing and new inspection holes. Install:4. 移走接近平台。Remove the access platforms.5. 拆下警告牌。Remove the warning notices.6. 恢复飞机至正常可用状态。Put the aircraft back to its initial configuration. 附录03 / Appendix 01技术文件反馈单/Technical Feedback Form工程师填写以下内容/Eng