WOHA33_11462C106_207_AT-722241-200-804

Hong Kong Airlines Limited香港航空03110-01Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA331146_207_106ETOPS 培训方式1146106通用类/GenericTitleGENERAL VISUAL INSPECTION OF SPLITTER FAIRING FIRE SEALSMcd&Rev/厂家工卡&修订日期标题整体目视检查分离器整流罩防火封严AMM 72-22-41-200-8042013-07-01A/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BLNVAT-722241-200-804HR000001动力/PowerplantAIRP02:00MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-722200-R2-1MPD 722200-R2-1,MRB 72.03.00/02-RRIssue 2 Revision 4PVG10000 FH10000 FHAccess Panels/接近盖板Zones/区域Written/编写Approved/批准415AL 416AR 417AL 418AR4132013-08-222013-09-09TOOLS/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198A24403000000CABLE HOLDING STRAPTO1ALL(必需/Necessary)2FK24273COVER - COMMON NOZZLE ASSEMBLYTO1ALL(必需/Necessary)3HU80955IMMOBILISERTO1ALL(必需/Necessary)或/or HU44525-14HU55148PUMP - 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-60/164202372410A3300002LH ENGINEPN-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 Applivable) 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,D101131* Other: * Signature:_ Authorization No.:_ Date:_AT-722241-200-804 HR000001 W/O:1146 AC:BLNV页码，2 / 9工卡Job card:HA33-722200-R2-1TITLEGENERAL VISUAL INSPECTION OF SPLITTER FAIRING FIRE SEALSPerfInsp标题整体目视检查分离器整流罩防火封严工作者检查者*检查/Inspect切片开始*General Visual Inspection of Splitter Fairing Fire Seals整体目视检查分离器整流罩防火封严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：在关车后的发动机部件上工作时必须小心，发动机部件可能会持续1小时高温。WARNING: YOU MUST NOT TOUCH HOT PARTS WITHOUT APPLICABLE GLOVES. HOT PARTS CAN CAUSE AN INJURY. IF YOU GET AN INJURY PUT IT IN COLD WATER FOR 10 MINUTES AND GET MEDICAL AID.警 告：在未戴手套的情况下禁止触碰高温部件，高温部件会导致人员受伤。如果被烫伤，请将烫伤处置于冷水十分钟并就医。1. Job Set-up/工作准备A. Energize the ground service network(Ref. TASK 24-42-00-861-801-A). T 接通地面电源（参照TASK 24-42-00-861-801-A）。B. Safety Precautions/安全防范 T (1) Make sure that the engine 1(2) shutdown occurred not less than five minutes before you do this procedure. 在工作前请确认左右发动机关车时间不少于5分钟。C. Get Access to the Avionics Compartment T 接近电子舱(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at access door 811. 放置工作梯于接近门811处。(2) Open access door 811. 打开接近门811.(3) Open the protective door of the AC/DC emergency power-center 740VU. 打开交/直流应急电源740VU的保护门。D. Open, safety and tag this(these) circuit breaker(s): T 拔出如下跳开关，安装跳开关保护夹并挂警告牌：PANELDESIGNATIONFINLOCATIONFOR4030EM1/对于1号发动机742VUFADECENG1A12KS1Q73722VUFADECENG1B13KS1D44FOR4030EM2/对于2号发动机742VUFADECENG2A12KS2Q74722VUFADECENG2B13KS2K49E. Get Access/接近 T WARNING: YOU MUST NOT OPEN THE FAN COWL DOORS WHEN THE WIND SPEED IS 60 MPH (96 KPH) OR MORE. AN INJURY AND/OR DAMAGE CAN OCCUR IF THE WIND MOVES THE FAN COWL DOORS.警 告：当风速超过60MPH (96 KPH)时请勿打开风扇整流罩，如果大风吹动整流罩会导致人员受伤或设备受损。WARNING: YOU MUST BE CAREFUL IF YOU OPEN THE FAN COWL DOORS WHEN THEWIND SPEED IS BETWEEN 30 MPH (48 KPH) AND 60 MPH (96 KPH). ANINJURY AND/OR DAMAGE CAN OCCUR IF THE WIND MOVES THE FAN COWLDOORS.警 告：当风速在30 MPH (48 KPH) 和60 MPH (96 KPH)之间，打开风扇整流罩时请小心。如果风吹动整流罩可能会导致人员受伤或设备受损。(1) Open the fan cowl doors(Ref. TASK 71-13-00-010-805-A): 打开风扇整流罩（参照TASK 71-13-00-010-805-A）：(a) FOR 4030EM1/对于1号发动机415AL, 416AR(b) FOR 4030EM2/对于2号发动机425AL, 426ARF. Deactivation of the Thrust Reverser T 反推限动WARNING: YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON OR AROUND IT.IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY AND/OR DAMAGE.警 告：在反推附近工作前必须对反推限动，否则，反推意外操作会导致人员受伤和设备受损。(1) Make the thrust reverser unserviceable(Ref. TASK 78-31-00-040-805-A). 使反推失效（参照TASK 78-31-00-040-805-A）G. Get Access/接近 T (1) Open the thrust reverser cowl-doors(Ref. TASK 78-30-00-010-803-A): 打开反推整流罩（参照TASK 78-30-00-010-803-A）：(a) FOR 4030EM1/对于1号发动机417AL, 418AR(b) FOR 4030EM2/对于2号发动机427AL, 428AR(2) Put the ACCESS PLATFORM 1M(3 FT) in position. 将1M(3 FT)接近平台放置到位。2. Procedure/步骤A. General/概述 T (1) It is not necessary to remove the fairings to do this inspection. Use an LIGHT SOURCE INSPECTION and an MIRROR - INSPECTION where necessary. 不需要拆下整流罩执行检查，按需使用手电筒和反光镜。(2) You must correctly identify the specified part conditions and/or types of damage(Ref. TASK 70-01-02-910-802-A). This will prevent errors which can occur when a part condition or type of damage is known incorrectly by two different names. 必须正确辨别指定部件的状况和/或损伤类型（参照TASK 70-01-02-910-802-A）。这样可防止对部件状况和损伤类型的误判。(3) Refer to Rolls-Royce if you find a defect that is not specified inthis procedure. 如果发现不明缺陷请咨询厂家Rolls-Royce。B. Do an Inspection of the Lower Splitter Fairing Fire Seals (Ref. Fig. T 601/TASK 72-22-41-991-012-A) 检查分离器整流罩防火封严下部（参照图601/TASK 72-22-41-991-012-A）。(1) Examine the fire seals for security of attachment. 检查防火封严部附件是否牢靠。(a) If the fire seals are loose or not there, reject them. 确认防火封严未出现松动或丢失。(2) Examine the general condition of the fire seals. 核查防火封严整体状况。(a) If the fire seals are damaged, reject them. 确认防火封严未损坏。C. Do an Inspection of the Upper Bifurcation Fairing Fire Seals (Ref. Fig. T 602/TASK 72-22-41-991-013-A) 检查防火封严上部支罩（参照图602/TASK 72-22-41-991-013-A）。(1) Examine the fire seals for security of attachment. 核查防火封严部附件是否牢靠。(a) If the fire seals are loose or not there, reject them. 确认防火封严未出现松动或丢失。(2) Examine the general condition of the fire seals. 核查防火封严整体状况。(a) If the fire seals are damaged, reject them. 确认防火封严未损坏。3. Close-up/结束A. Close Access/关闭接近 T (1) Make sure that the work area is clean and clear of tools and other items. 确认工作区域干净无工具和杂物。(2) Remove the access platform(s). 撤除接近平台。(3) Close the thrust reverser cowl-doors(Ref. TASK 78-30-00-410-803-A): 关闭反推整流罩（参照TASK 78-30-00-410-803-A）：(a) FOR 4030EM1/对于1号发动机417AL, 418AR(b) FOR 4030EM2/对于2号发动机427AL, 428ARB. Make the thrust reverser serviceable(Ref. TASK 78-31-00-440-805-A). T 将反推恢复至可用状态（参照TASK 78-31-00-440-805-A）。C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): T 取