WOHA33_2632216_289_MAOTS711756

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_289_216DIC 2632216TitleInspection of the Tubes for Trent700 FleetMcd&Rev./厂家工卡&修订日期标题普查Trent700管路A/C/飞机号Subtask No/工卡号JC Rev/工卡版本号Workarea/工作区域Skill/工种Man Hour/工时BLNVMAOTS711756R0200动力/PowerplantAIRP/MDIC04:00/01:00MAO Item/MAO号Baseline/依据MAO REV/ 版本号Work Type/工作类别Threshold/首检Interval/重复检MAOTS720534Issue 2 Revision 0Access Panels/接近盖板Zones/区域Written/编写Approved/批准2017-05-082017-05-09Accomplished完工签署Complete Date完工日期Station维修站PVGREASON & DESCRIPTION/原因及描述机队曾发生一起燃油管和气管磨损漏油的事件，下发该MAO进行机队状态普查/A fuel leakage case occured as a result of a fuel tube and an air tube chafing,this MAO was issued to do the inspection for the fleet. 注释：R01版改版原因与内容：MAO工卡内容及到期日期修改/Note：Change and revise reason in issue R01: Amend task deadline and the content of subtask. R02版改版原因与内容：修改MAO工卡工具航材清单和工卡内容/Note：Change and revise reason in issue R02: Amend the subtask material list and working steps. R03版改版原因与内容：修改到期日期/Note：Change and revise reason in issue R03: Amend the task deadline.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1FK24273COVER - COMMON NOZZLE ASSEMBLYTO1ALL(必需/Necessary)2HU44525-1IMMOBILIZERTO1ALL(必需/Necessary)(互换/Interchange:HU80955)3HU55148PUMP - HAND, HYDRAULIC TRUTO1ALL(必需/Necessary)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1AS20624(非ETOPS)NUTAS1ALL(视情/As Necessary)2AS48408BOLT BIHEX HDAS1ALL(视情/As Necessary)3AS48412BOLT BIHEX HDAS1ALL(视情/As Necessary)4AS62424CLIPAS1ALL(视情/As Necessary)5K8831(非ETOPS)WASHER THKAS1ALL(视情/As Necessary)6LK39523CLIPAS1ALL(视情/As Necessary)7UL12506CLIP ASSYAS1ALL(视情/As Necessary)8UP10478SPACERAS1ALL(视情/As Necessary)9UP10480SPACERAS1ALL(视情/As Necessary)10UP12006CLIPAS1ALL(视情/As Necessary)11FK22809TUBE ASSY(该件可用1EA KH33133+1EA KH33130取代)AS1ALL(视情/As Necessary)12FW35915TUBE ASSY HP FUEL DUMPLINE-DISCONN TO BIFURCATIONAS1ALL(视情/As Necessary)13KH33133TUBEAS1ALL(视情/As Necessary)14KH33130TUBEAS1ALL(视情/As Necessary)PARTS INFORMATION/部件信息:NOTE: The component in PN,SN form is need to do periodic maintenance. For the return repair or retrofit，the form is PN,SN of the removed component. And the PN-IN,SN-IN would be written according to new parts after finish. For the non- returns(such as weight, test)，the form is PN,SN of the on-wing maintenance component. And fill the PN-IN,SN-IN with bias after finish.注释：件号、序号栏指需要定期执行维修工作的部件。对于要求更换拆下返厂工作的部件，该栏指拆下件、序号信息。完成工作后装上件号和序号栏请填写相关装机件信息；对于在位执行工作的（如称重、测试等），该栏指在位工作部件件、序号信息，完成工作后装上件号和序号请用斜线画去。PN/件号SN/序号ATA/章节ZONE/区域FIN/代码LOCATION/装机位置TRENT772B-60/164202472420A3300003PN-IN装上件号SN-IN装上序号REMOVAL REASON AND COMPONENT TASK REQUEST拆件原因及其部件工作要求TASK NOTE工作注释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 * 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:MAOTS720534TITLEInspection of the Tubes for Trent700 FleetPerfInsp标题普查Trent700管路工作者检查者警 告：在发动机关车后进行发动机部件的维护工作必须小心烫伤。发动机部件的余热会保持将近1小时。WARNING: YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR.警 告：不戴劳保手套不能接触发动机未冷却部件，否则会造成烫伤。若发生烫伤，将烫伤部位浸在凉水中10分钟，然后寻求医疗救治。WARNING: YOU MUST NOT TOUCH HOT PARTS WITHOUT APPLICABLE GLOVES. HOT PARTS CAN CAUSE INJURY. IF YOU GET AN INJURY, PUT IT IN COLD WATER FOR 10 MINUTES. THEN GET MEDICAL AID.注 释：本普查中发现任何不正常情况，请先留存照片并第一时间通知发动机工程师。N O T E : Please report any abnormal finding to Powerplant Engineer and take pictures.注 释：如果发现装机气管件号为KH33133和KH33130，请记录发动机序号，并在异常情况概要中说明：装机气管件号为KH33133/KH33130。其余步骤无需执行，签署“N/A”即可。N O T E : If you confirm the installed air tube P/N is KH33133 and KH33130, please feedback engine ESN and also record in summry for anomaly with:Installed air tube P/N is KH33133/KH33130. Other steps would not required, signN/A.1. 依据AMM TASK 71-13-00-010-805，打开风扇包皮。Ref .AMM TASK 71-13-00-010-805,Open the fan cowl doors. 2. 依据AMM TASK 78-31-0“0-040-805，执行反推限动。Ref. AMM TASK 78-31-00-040-805,Deactivate the thrust reverser. 3. 依据AMM TASK 78-30-00-010-803，打开反推。Ref. AMM TASK 78-30-00-010-803,Open the thrust reverser. 4. 检查如图1和图2所示燃油管路上下管接头之间的所有管卡子和管路（P/N：FW35915）是否存在磨损或破裂。Check the wear or damage on the tube and all the clips of the fuel tube(P/N:FW35915) between the upper and lower plug in Figure.1 and Figure.2. 5. 检查如图3和图4所示气管上下管接头之间的所有管卡子和管路（P/N：FK22809）是否存在磨损或破裂。Check the wear or damage on the tube and all the clips of the air tube(P/N:FK22809) between the upper and lower plug in Figure.3 and Figure.4. 6. 重点检查图2中的卡子CP4074和卡子CP4073是否存在破裂。Check carefully the damage on clip CP4074 and clip CP4073. 7. 如图5所示位置，确保两根管路存在间隙。如果间隙小于5mm，拍照并通报发动机工程师（）。Make sure there is a clearance between the two tubes in Figure.5., take photos and report to powerplant enginner immediately for any clearance lower than 5MM.注释：如果涉及管路（P/N：FW35915）或者（P/N：FK22809）安装请执行步骤8或者9，否则请在步骤8或者9签署栏签“N/A”。NOTE：If the installation of tube （P/N：FW35915）or （P/N：FK22809）is required,please refer to step 8 or 9, otherwise,input “N/A” at the column. 8. 对于管路（P/N：FW35915）的安装程序，请参照图7，并参考AMMTASK71-00-00-700-827-A完成燃油渗漏测试。The installation procedure for tube（P/N：FW35915）can be refered to Fig.7 and refer to AMMTASK71-00-00-700-827-A to accomplish the Fuel Leak Test. DIC9. 对于管路（P/N：FK22809）的安装程序，请参照图6。The installation procedure for tube（P/N：FK22809）can be refered to Fig.6. DIC10. 依据AMM TASK 78-30-00-410-803，关闭反推。Ref. AMM TASK 78-30-00-410-803,Close the thrust reverser. 11. 依据A