WOHA33_4919179_340_EOA33-53-0047

Hong Kong Airlines LimitedHong Kong Air Cargo Carrier Limited香港航空有限公司香港货运航空有限公司F-D-099Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA334919_340_179AD 4919179Training and Qualification/培训和资格Technical Record/技术记录NONEADTitleFuselage - 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/8EOA33-53-0047R05机身/AirframeAIRP /NDT01:00/07:30Baseline/依据Operator EO/营运人EOR05Work Type/工作类别Threshold/首检Interval/重复检SB A330-53-3228/R01,AD 2018-0147,CAD 2018-A330-04EOA33-HKG53-0035Written/编写Reviewed/审核Approved/批准2018-08-102018-08-222018-08-23Accomplished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。已对受影响的疑似和/或实际不符合设计定义的飞机结构执行详细的安全评估。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.版本变化/REVISION改版原因/REASON修改内容/CHANGE DESCRIPTIONR02-R031.航材属性显示错误。Parts properties are incorrect.2.施工步骤中部分标号和签署线显示错误。Some labels and sign lines in work instructions are incorrect.3.BLNV飞机组别错误需修改。The group of A/C BLNV is incorrect and need to change.1.将航材F5397460901451由“必需”修改为“视情”。Revise F5397460901451 from necessary to on condition.2.修正错误的标号和签署线。Revise incorrect labels and sign lines.3.将BLNV飞机组别从Group 2改为Group 3.Change group of A/C BLNV from Group 2 to Group 3.R03-R04SB 53-3228R01发布。SB 53-3228R01 issued.1.依据文件SB 53-3228R00更新为R01。Update source document SB 53-3228 from R00 to R01.2.将BLNM,BLNN,BLNO,BLNP由分组2修改为分组7，BLNV,BLNW由分组3修改为分组8.。Revise BLNM,BLNN,BLNO,BLNP from Group.2 to Group.7, BLNV,BLNW from Group.3 to Group.8.3.修改计划安排和版本关系，增加附加工作相关要求。Revise plan information and relation between revisions, to add the requirements of additional work.4.更新航材清单。Update the material list.5.修改施工步骤。增加附加工作。Revise work instructions and add the additional work.R04-R05AD 2018-0147发布，替代AD 2015-0212。AD 2018-0147 issued and supersede AD 2015-0212.1.依据文件AD2015-0212更新为AD2018-0147。Update baseline from AD2015-0212 to AD2018-0147.2.修改计划安排、版本间关系、施工步骤中关于附加工作的描述。Revise the plan information, relation between revisions, work instructions, about the description of additional work.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1F5377005220451ANGLEAS1ALL视情,数量按需/On condition and quantity as required2F5397460901451BRACKETAS1ALL视情,数量按需/On condition and quantity as required3F5397463600000BRACKETAS1ALL视情,数量按需/On condition and quantity as required4F5397463601000BRACKETAS1ALL视情,数量按需/On condition and quantity as required5F5397463622651BRACKETAS1ALL视情,数量按需/On condition and quantity as required6F5397605720000SECTIONAS1ALL视情,数量按需/On condition and quantity as required7F5397605720200SECTIONAS1ALL视情,数量按需/On condition and quantity as required8F5397605720400SECTIONAS1ALL视情,数量按需/On condition and quantity as required9F5397605720600SECTIONAS1ALL视情,数量按需/On condition and quantity as required10F5398903100051SUPPORTAS1ALL视情,数量按需/On condition and quantity as required11A2527036700051BRACKETAS1ALL视情,数量按需/On condition and quantity as required12A2527036700151BRACKETAS1ALL视情,数量按需/On condition and quantity as required13F5397460902051BRACKETAS1ALL视情,数量按需/On condition and quantity as required14F5398903300251SUPPORTAS1ALL视情,数量按需/On condition and quantity as required15F5398905700051SUPPORTAS1ALL视情,数量按需/On condition and quantity as required16G5397087601400BRACKETAS1ALL视情,数量按需/On condition and quantity as requiredIMPORTANT 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:_EOA33-53-0047 R05 W/O:4919 AC:BLNV页码：23 / 23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注 释：执行工作前请联系PPD确认该飞机的EO执行状态。NOTE: Please contact PPD to confirm the EO accomplishment condition before you start this task.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（电气性和机械性均可用）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 释：当本EO步骤中出现“refer to”字样时，如工作者有可被当地局方接受的替代程序，可以使用替代程序进行施工；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: 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 EO do not constitute or affect the technical intent of the EO. 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 EO is met within the set parameters.注 释：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已被或将要被适航指令（AD）定义为强制执行。施工步骤中的段落D为要求符合（RC）的段落，且必须被执行以符合AD。其他段落为推荐执行，且可以被偏离，作为其他措施的一部分来执行，或使用不同于本EO得其他可接受的方法，只要保证RC段落被执行且飞机能被恢复至可运行状态即可。NOTE: This EO is classified mandatory or expected to be classified mandatory by an Airworthiness Directive AD). The paragraphs D in these accomplishment instructions is 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：本EO包含为确保飞机持续适航所必须的机上维护说明。对于本EO的任何偏离，联系结构工程师获取进一步指示和批准。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.B. 标准施工/STANDARD PRACTICES(a) 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.(b) 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) 飞机接近盖板的识别，参考AMM 06-41-53, Page Block 001。For identification of access panels, refer to AMM 06-41-53, Page Block 001.C. 施工准备/PREPARATION1. 工作准备/Job Set-up注 释：对于基本飞机构型，参考AMM手册前言部分的“介绍-飞机维护状态”章节。NOTE: For the basic Aircraft configuration, refer to AMM Chapter Introduction - Aircraft status for maintenance in Manual Front Matter section.(a) 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.(b) 在工作区域下部放置接近平台。Put an access platform in position below the work areas. D. 施工步骤/PROCEDURE第一部分-完整工作 / Part.1 - COMPLETE WORK：注 释：以下步骤仅适用于未执行过本EO任何版本的飞机。NOTE: The below steps only applicable to aicrafts not incorporated any revision of this EO.注 释：执行工作前请联系PPD确认该飞机的EO执行状态。NOTE: Please contact PPD to confirm the EO accomplishment condition before you start this task.(1) 对前客舱顶部舱执行涡流电导率测试 - Subtask 533228-250-201-008Do an Eddy Current Conductivity Measurement of the Forward Cabin Overhead Compartment(a) 参考AMM 25-23-00按需拆下盖板。Remove panels as necessary, refer to AMM 25-23-00.(b) 按照NTM 51-60-00，附录01-检查程序和Fig. A-GFAAA，对涉及区域安装的结构件执行涡流电导率测量，参考Fig. A-GBAAC。In accordance with NTM 51-60-00, Appendix 01 - Inspection Procedure and Fig. A-GFAAA, do the Eddy Current Conductivity Test of the installed structural parts inthe involved areas, refer to Fig. A-GBAAC.注 释：使用探头直接接近结构件的平坦区域进行检查。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：If measured value 22 MS/m or 37.9% IACS:a 无需采取措施。 No action required.2 若测量值介于22-26 MS/m或者介于37.9-44.8% IACS之间：If the measured value is between 22 and 26 MS/m or 37.9 and 44.8 % IACS:a 检查NDT设备并重新进行测量。Check the NDT tool and perform a new measurement.b 若测量值仍然介于22-26 MS/m或者介于37.9-44.8% IACS之间，联系结构工程师获取进一步指示。If the measured value again is between 22 and 26 MS/m or 37.9 and 44.8 % IACS, contact structure engineer for further instructions.3 若测量值大于26 MS/m或者大于44.8% IACS：If measured value 26 MS/m or 44.8% IACS:a 参考附录02更换所需件。Replace the necessary parts, refer to Appendix 02.4 完成并反馈附录03-检查报告。Complete and feedback the Report Sheet, refer to Appendix 03 -Report Sheet .5 对此区域无需采取进一步措施。No further action in this area.(c) 安装所有拆下的件，参考AMM 25-23-00。Install all removed panels, refer to AMM 25-23-00.第二部分-附加工作 / Part.2 - ADDITIONAL WORK：注 释：以下步骤仅适用于已完成本EO R03或之前版本，且未执行过本EO R04及之后版本的飞机。NOTE: The below steps only applicable to aicrafts incorporated this EO R03 or previous revision, and not incorporated this EO R04 and later revision.注 释：执行工作前请联系PPD确认该飞机的EO执行状态。NOTE: Please contact PPD to confirm the EO accomplishment condition before you start this task.(1) 对前客舱顶部舱执行涡流电导率测试 - Subtask 533228-250-204-001Do an Eddy Current Conductivity Measurement of the Forward Cabin Overhead Compartment(a) 参考AMM 25-23-00按需拆下盖板。Remove panels as necessary, refer to AMM 25-23-00.(b) 按照NTM 51-60-00，附录01-检查程序和Fig. A-GFAAA，对涉及区域安装的结构件执行涡流电导率测量，参考Fig. A-GCAAB。In accordance with NTM 51-60-00, Appendix 01 - Inspection Procedure and Fig. A-GFAAA, do the Eddy Current Conductivity Test of the installed structural parts inthe involved areas, refer to Fig. A-GCAAB.注 释：使用探头直接接近结构件的平坦区域进行检查。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：If measured value 22 MS/m or 37.9% IACS:a 无需采取措施。 No action required.2 若测量值介于22-26 MS/m或者介于37.9-4