WOHA33_4451165_108_EOA33-29-0035

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03110-01Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA334451_108_165DIC DM 4451165Training and Qualification/培训和资格Technical Record/技术记录ETOPS DICNONETitleA330 - Modify Plug on Yellow and Blue HP ManifoldMcd&Rev/厂家工卡&修订日期标题A330 - 改装黄系统及蓝系统高压总管组件上的盲堵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BLNX/1EOA33-29-0035R03机身/AirframeAIRP /MDIC04:00/01:00Baseline/依据Operator EO/营运人EOR03Work Type/工作类别Threshold/首检Interval/重复检SB A330-29-3135/R01EOA33-HKG29-0031Written/编写Reviewed/审核Approved/批准2018-09-032018-09-062018-09-07Accomplished完工签署Complete Date完工日期Station维修站PVGREASON & DESCRIPTION/原因及描述完成此SB将减小黄系统高压总管C口及蓝系统高压总管F口的漏油风险。故下发EO执行此改装。The accomplishment of this Service Bulletin will reduce the occurrence of leakage in the yellow HP manifold at port C and the blue HP manifold at port F.So issue EO perform this modification.版本变化/REVISION改版原因/REASON修改内容/CHANGE DESCRIPTIONR00-R01根据一线反馈及空客TR，修改工卡内容。Based on the feedback form line maintenance and TR from airbus, revise the work step.修改工作步骤并增加相应注释和附图。Revise the work step and add the related notes and figures.R01-R02根据一线反馈及空客TR 80440265，修改工卡内容。Based on the feedback form line maintenance and Airbus TR 80440265, revise the work step.修改部分工作步骤并删除使用清漆的要求。Revise part of work step and delete the requirement of applying varnish.R02-R03根据SB A330-29-3135 R01版，修改工卡内容。Based on the SB A330-29-3135 R01 version,revise the work step.修改部分工作步骤并增加附图。Revise part of work step and add the Figure.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198F32204001001COLLAR, SAFETY - DOOR, NLGTO1ALL必需/Necessary2460007174PIN - GROUNDLOCK, MLGTO2ALL必需/Necessary3D23304000PIN-GROUNDLOCK, NLGTO1ALL必需/Necessary498F32104013000SAFETY COLLAR-DOOR MLGTO2ALL必需/NecessaryTOOLS 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173XBLACK INKCH1ALL必需/Necessary;或等效记号笔2CML02ABA1HYARAULIC FLUIDCH1ALL必需/Necessary3293135A01R00KITAS2ALL必需/NecessaryPARTS 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1CML14SBA1CLEANING ABSORCH1ALL视情/On condition2CML04SAB2PUTTYCH1ALL视情/On condition3CML08BBB1CLEANERCH1ALL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:_EOA33-29-0035 R03 W/O:4451 AC:BLNX页码，21 / 21工卡Job card:EOA33-29-0035TITLEA330 - Modify Plug on Yellow and Blue HP ManifoldPerfInsp标题A330 - 改装黄系统及蓝系统高压总管组件上的盲堵工作者检查者警 告： 遵守参考程序中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： 当系统的维护工作由同一个人完成时，禁止三个液压系统同时工作。这是为了防止对某个系统的维护不当也会对其他系统造成影响。两个以上系统的维护不当可导致多个系统的失效。如果必须要同时维护两个以上的系统并需要断开管路/部件，则每个系统必须要用不同的人员维护。CAUTION: DO NOT WORK ON ALL THREE HYDRAULIC SYSTEMS DURING THE SAMEMAINTENANCE INPUT WITH THE SAME MAINTENANCE PERSONNEL. THISIS TO MAKE SURE THAT A POSSIBLE MAINTENANCE ERROR ON ONESYSTEM IS NOT DONE AGAIN ON A DIFFERENT SYSTEM. A MAINTENANCEERROR ON MORE THAN ONE HYDRAULIC SYSTEM CAN CAUSE SYSTEMFAILURE ON MULTIPLE SYSTEMS. IF MAINTENANCE IS NECESSARY ONMORE THAN ONE SYSTEM AT THE SAME TIME AND INVOLVES LINES /COMPONENTS DISCONNECTION, DIFFERENT MAINTENANCE PERSONNELMUST BE USED FOR EACH SYSTEM.注 意: 遵守以下预防措施，使得电线处于一种安全状态（电气和机械可用状态）。当你在做维护工作的时候，修理或者改装，保持导线束，部件和工作区域尽可能的干净。执行以下步骤： 执行保护措施，比如塑料布，棉布等导线束和部件上必须的保护措施。 均匀的除去所有毛边，不需要的材料和其他污物。 参考ESPM20-55-00，这些预防措施能减小需安装导线束的污染和损坏的风险。CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY ANDMECHANICALLY 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 ELECTRICAL WIRING AND COMPONENTS.- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL ANDOTHER 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.A.通用信息/GENERAL(1) 标准施工/ Standard Practices(a) 对于区域的识别，参考AMM06-20-00,Page Block 001.。For the identification of zones, refer to AMM 06-20-00,Page Block 001.(b) 管路接头紧固力矩，参考AMM Task 20-21-12-911-801。To torque tighten pipe unions, refer to AMM Task 20-21-12-911-801.(c) 对于本EO中所提供材料的规格，参考CML。For the specification of materials (Mat. No.) given in this EO, refer to Consumable Materials List (CML).B.准备/PRERATION(1) 工作准备/ Job Set-up注 释：本注释中的内容是进行维护工作之前飞机的基本构型。NOTE: The items given in this note shall be considered as the basic Aircraftconfiguration before you start a maintenance task:-飞机停放在地面靠起落架支撑(地面安全销在位，挡好轮挡) Aircraft on the ground resting on landing gear (the ground safetylocks and the wheel chocks are in position on the landing gear)-发动机停车，反推收起并锁定。 Engine shut down, thrust reversers are closed and locked-飞机处于干净的构型。Aircraft in clean configuration-设置了停留刹车。Parking brake applied-飞机断电。 Aircraft electrical network de-energized-液压系统释压。Hydraulic systems depressurized-可接近驾驶舱和客舱。Access to the cockpit and cabin is available-所有的跳开关都在关闭位All circuit breakers are in closed position-所有的控制在NORM,AUTO或OFF位 All controls in NORM, AUTO or OFF position.(a) 确保飞机接地，参考AMM Task 12-34-24-860-802。Make sure that the aircraft is electrically grounded, refer to AMM Task12-34-24-860-802.(b) 参考AMM Task 29-12-53-000-805，执行拆下蓝液压系统高压总管的准备工作。 Do the job set-up procedure as specified in the removal of the blue HP manifold,refer to AMM Task 29-12-53-000-805.(c) 参考AMM Task 29-13-53-000-803，执行拆下黄液压系统高压总管的准备工作。 Do the job set-up procedure as specified in the removal of the yellow HP manifold,refer to AMM Task 29-13-53-000-803.C.工作步骤/PROCEDURE(1) 更换蓝系统高压总管F口的管帽，接头及封圈。Replace the cap,Union and Packing at Port F of the Blue HP Manifold(a) 拆下管帽，接头及封圈，参考Fig. A-FBAAA。Remove the cap,union and packing, refer to Fig. A-FBAAA.数量/Number 名称/Designation 位置/Location 处理方式/Treatment1 Cap Item (4) 报废/Discard1 Union Item (3) 报废/Discard1 Packing Item (2) 报废/Discard (b) 安装堵头及封圈，参考Fig. A-FBCAA。Install the plug and packing, refer to Fig. A-FBCAA.1 参考AMM Task 20-29-00-911-801，在堵头（项目1）上安装封圈（项目2）。 Install the packing item 2 on the plug item 1, refer to AMM Task 20-29-00-911-801.数量/Number 名称/Designation件号/P/N 位置/Location1 Packing NAS1612-10A Item 22 安装堵头（项目1）至蓝系统高压总管F口。 Install the plug item 1 on the blue HP manifold port F.数量/Number 名称/Designation件号/P/N 位置/Location1 Plug AS5169J10 Item 13 将堵头（项目1）力矩磅至5.03和5.14 m.daN (37.09-37.91 lbf.ft)之间。 Torque the plug item 1 to between 5.03 and 5.14 m.daN (37.09 and 37.91 lbf.ft). 填写实际使用的力矩值为/ Fill the actual torque value：_(c) 重新标识蓝系统高压总管及组件(FIN 6103JM)件号，参考PMS 01-06-20和Fig.A-FBEAA。Re-identify the blue HP manifold and manifold assembly(FIN 6103JM), refer to Process and Material Specification (PMS) 01-06-20 and Fig. A-FBEAA. 注 释：PMS 01-06-20 可通过如 下路径“文件 管理系统 OEM 空客 空客通用类手册 SUPPLIER”查询。NOTE: Operator can find PMS 01-06-20 from “ 文件管理系统 OEM 空客 空客通用类手册 SUPPLIER”.1 清洁蓝系统高压总管(FIN 6103JM)标牌部分(如有)，使用：If installed, clean the Manifold identification PN located on the body of the Blue HPManifold (FIN 6103JM) use:名称/Designation件号/P/N数量/NumberTextile - Lint Free Cotton14SBA1按需/As required 使用/made moist with名称/Designation件号/P/N数量/NumberNon Aqueous CleanerPetroleum Based08BBB1按需/As required2 使用不退色的笔重新标识蓝系统高压总管的新件号，依据下表和Fig. A-FBEAA Sheet 02。Mark the Blue HP manifold with the new blue HP manifold body part number and thenew blue HP manifold assembly part number using indelible ink. refer to followingtable and Fig. A-FBEAA Sheet 02.FIN 6103JM注 释：部分飞机在执行SB A330-29-3125改装后，高压总管上Assembly件号没有正确修改，故无法在上表中找到，则参考下表进行标识。NOTE: For part of aircraft, the PN of Assembly on HP Manifold have not been revisedcorrectly after having accomplished SB A330-29-3125, so it cant be found in the abovelist，so unify the PN as shown in sheet below.名称/Designation旧件号/Old PN新件号/New PNBlue HP Manifold AssemblyF2911086300600F2911086300800F2911086302000F2911303600000F2911086300500F2911086301000F2911303600200F2911086300400F2911086301200F2911303600400F2911086300200F2911086301400F2911303600600F2911086300100F2911086301600F2911303600800F2911086300000F2911086301800F2911303601000注 释：如果不能在高压总管上找到Body件号，直接标识新件号F2911303700000；如果不能在高压总管上找到Assembly件号，直接标识新件号F2911303600000。NOTE: if you can not find the Body PN of Manifold on HP Manifold, directly identify it with newPN F2911303700000; if you can not find the Assembly PN of Manifold on HP Manifold, directly identify it with new PN F2911303600000.(2) 更换黄系统高压总管C口的管帽，接头及封圈。Replace the Cap,Union and Packing at Port C of the Yellow HP Manifold(a) 拆下管帽，接头及封圈，参考Fig. A-FBBAA。Remove the cap,union and packing, refer to Fig. A-FBBAA.数量/Number 名称/Designation 位置/Location 处理方式/Treatment1 Plug Item (4) 报废/Discard1 Union Item (3) 报废/Discard1 Packing Item (2) 报废/Discard (b) 安装堵头及封圈，参考Fig. A-FBDAA。Install the plug and packing, refer to Fig. A-FBDAA.1 参考AMM Task 20-29-00-911-801，在堵头（项目1）上安装封圈（项目2）。 Install the packing item 2 on the plug item 1, refer to AMM Task 20-29-00-911-801.数量/Number 名称/Designation件号/P/N 位置/Location1 Packing NAS1612-10A Item 22 安装堵头（项目1）至黄系统高压总管C口。 Install the plug item 1 on the yellow HP manifold port C.数量/Number 名称/Designation件号/P/N 位置/Location1 Plug AS5169J10 Item 13 将堵头（项目1）力矩磅至5.03和5.14 m.daN (37.09-37.91 lbf.ft)之间。 Torque the plug item 1 to between 5.03 and 5.14 m.daN (37.09 and 37.91 lbf.ft). 填写实际使用的力矩值为/ Fill the actual torque value：_(c) 重新标识黄系统高压总管及组件(FIN 7103JM),件号，参考PMS 01-06-20和Fig.A-FBFAA。Re-identify the yellow HP manifold and manifold assembly (FIN 7103JM), refer to Process and Material Specification (PMS) 01-06-20 and Fig. A-FBFAA. 注 释：PMS 01-06-20 可通过如 下路径“文件 管理系统 OEM 空客 空客通用类手册 SUPPLIER”查询。NOTE: Operator can find PMS 01-06-20 from “ 文件管理系统 OEM 空客 空客通用类手册 SUPPLIER”.1 清洁黄系统高压总管(FIN 7103JM)标牌部分(如有)，使用：If installed, clean the Manifold identification PN located on the body of the Yellow HPManifold (FIN 7103JM) , use:名称/Designation件号/P/N数量/NumberTextile - Lint Free Cotton14SBA1按需/As required 使用/made moist with名称/Designation件号/P/N数量/NumberNon Aqueous CleanerPetroleum Based08BBB1按需/As required注 释：由于邻近油箱，应特别注意清洁Fig.A-FBFAA Sheet 03中所示的高压总管标牌部分。NOTE: Cleaning of the HP manifold body PN shown in Fig. A-FBFAA Sheet 03 is to be performed with special attention due to proximity of tank.2 使用不退色的笔重新标识黄系统高压总管的新件号，依据下表和Fig. A-FBFAA Sheet 02。Mark the yellow HP manifold with the new yellow HP manifold body part number and thenew yellow HP manifold assembly part number using indelible ink. refer to followingtable and Fig. A-FBFAA Sheet 02. FIN 7103JM注 释：部分飞机在执行SB A330-29-3125改装后，高压总管上Assembly件号没有正确修改，故无法在上表中找到，则参考下表进行标识。NOTE: For part of aircraft, the PN of Assembly on HP Manifold have not been revisedcorrectly after having accomplished SB A330-29-3125, so it cant be found in the abovelist，so unify the PN as shown in sheet below.名称/Designation旧件号/Old PN新件号/New PNYellow HP Manifold AssemblyF2911086600000F2911086602000F2911305300200F2911086600100F2911086601800F2911305300400F2911086600200F2911086601600F2911305300600F2911086600300F2911086601400F2911305300800F2911086600400F2911086601200F2911305301000F2911086600500F2911086601000F2911305301200F2911086600600F2911086600800F2911086602200F2911305301400注 释：如果不能在高压总管上找到Body件号，直接标识新件号F2911305400000；如果不能在高压总管上找到Assembly件号，直接标识新件号F2911305301400。NOTE: if you can not find the Body PN of Manifold on HP Manifold, directly identify it with newPN F2911305400000; if you can not find the Assembly PN of Manifold on HP Manifold, directly identify it with new PN F2911305301400.D.测试/TEST (1) 测试蓝系统和黄系统高压总管 Leak Tes