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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WOHA331054_129_88培训方式105488通用类/GenericTitleGeneral Visual Inspection Of Fixed Structure Seals-No.1 Engine Thrust ReverserMcd&Rev/厂家工卡&修订日期标题整体目视检查固定结构封严-左发反推AMM 78-30-00-210-807-A 2010-10-01A/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BLNIAT-783000-210-807LHR001002动力/PowerplantAIRP00:30MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-783200-P3-1LMPD 783200-P3-1,MRB 78.32.00/03-PWIssue 2 Revision 3PVG545 CA545 CAAccess Panels/接近盖板Zones/区域Written/编写Approved/批准415AL 415BL 416AR 416BR 417AL 418AR4102011-03-152011-03-18TOOLS/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)2PWA88014PIN LOCK-THRUST REVERSER ACTUATORTO1ALL(必需/Necessary)3PWA88013PIN UNLOCK-THRUST REVERSER ACTUATORTO1ALL(必需/Necessary)4PWA88012PIN-LOCK,DIRECTIONAL CONTROL VALVETO1ALL(必需/Necessary)5PWA88003PUMP, HYDRAULIC - THRUST REVERSER DOORTO1ALL(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1TT-I-735异丙醇-Non Aqueous Cleaner-Isopropyl AlcoholTO1ALL(视情/As Necessary)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:_HA33-783200-P3-1L W/O:1054 AC:BLNI页码,2 / 17工卡Job card:HA33-783200-P3-1LTITLEGeneral Visual Inspection Of Fixed Structure Seals-No.1 Engine Thrust ReverserPerfInsp标题整体目视检查固定结构封严-左发反推工作者检查者General Visual Inspection Of Fixed Structure SealsNo.1 Engine Thrust Reverser整体目视检查固定结构封严左发反1. Job Set-up / 开始工作 A. Energize the ground service network M 给飞机提供地面电源。(Ref. AMM TASK 24-42-00-861-801) . B. Safety Precautions M 安全警示(1) Make sure that the engine 1, (2) shutdown occurred not less than 5 minutes before you do this procedure. 执行此工作时确保1号,2号发动机均关车至少5分钟。C. Get Access to the Avionics Compartment T 接近电子舱(1) Put the access platform in position at the access door 811 . 放置工作梯到位。(2) Open the access door 811 . 打开接近门811。(3) Open the protective door of the AC/DC emergency power-center 740VU. 打开740VU组件的保护门。D. Open, safety and tag this(these) circuit breaker(s): T 拔出以下跳开关,安装保险卡子,并挂上警告牌,挂签:PANEL DESIGNATION FIN LOCATION FOR 4030EM1 722VU FADEC B ENG 1 13KS1 D44 742VU FADEC A ENG 1 12KS1 Q73 FOR 4030EM2 722VU FADEC B ENG 2 13KS2 K49 742VU FADEC A ENG 2 12KS2 Q74 E. Get Access M 接近工作(1) Open the left and right aft fan cowl doors : 打开左右侧后风扇整流罩。(Ref. AMM TASK 71-13-00-010-802)(a) FOR 4030EM1 415BL 416BR (b) FOR 4030EM2 425BL 426BR F. Make the thrust reverser unserviceable. M 执行反推限动工作。(Ref. AMM TASK 78-30-00-040-804)G. Get Access M 接近(1) Open the left and right thrust reverser cowl doors: 打开左右侧反推整流罩。(Ref. AMM TASK 78-30-00-010-801)(a) FOR 4030EM1 417AL 418AR (b) FOR 4030EM2 427AL 428AR (2) Manually deploy the translating cowls . 人工放出反推。(Ref. AMM TASK 78-30-00-860-801)(3) Put the adjustable access platform in position. 放置工作梯到位。2. Procedure / 步骤 T (Ref. Fig. Fixed Structure Seals SHEET 1) (Ref. Fig. Fixed Structure Seals SHEET 2) (Ref. Fig. Fixed Structure Seals SHEET 3) (Ref. Fig. Fixed Structure Seals SHEET 4) (Ref. Fig. Fixed Structure Seals SHEET 5) (Ref. Fig. Fixed Structure Seals SHEET 6) (Ref. Fig. Fixed Structure Seals SHEET 7) (Ref. Fig. Fixed Structure Seals SHEET 8) (Ref. Fig. Fixed Structure Seals SHEET 9) (Ref. Fig. Fixed Structure Seals SHEET 10)A. With A White Light, And Mirror, Do A Visual Inspection Of The Thrust Reverser Fixed Structure Seals To The Limits Shown In Table 601. 使用照明灯和反光镜,目视检查反推固定结构封严,表601为结构标准。表601EXAMINE / 检查位置RESULTS / 现象DISPOSITION / 处置REPAIR / 修补措施Latch Beam Seals, Firewall Seal, Lower Seal End Plug, Torque Box Seal . See detail B(参考图2) 锁扣桁条封严,防火墙封严,底部封严末端堵塞,扭矩盒封严(参考图2)Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-62-350-801.小于0.5 inch (12.70mm)的缺口参考78-32-62-350-801修补Inner Vee Groove Seal .See detail C (参考图3)内侧V型槽封严(参考图3)Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-64-350-801.小于0.5 inch (12.70mm)的缺口参考78-32-64-350-801修补Upper Bondment Strut Cover Seal, Forward Pylon Seal, Spiral Transition Seal. See detail D(参考图4)顶部贴合支柱保护封严,前吊架封严,过渡螺旋封严(参考图4)Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-65-350-801.小于0.5 inch (12.70mm)的缺口参考78-32-65-350-801修补Lower Inner Cowl Seal, Lower Seal Retainer Filler. See details E and F(参考图5)整流罩内侧底部封严,底部封严保持块填充物(参考图5)Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-67-350-801小于0.5 inch (12.70mm)的缺口参考78-32-67-350-801修补Forward Lower Inner Cowl Seal and Rear Lower Inner Cowl Seal. See details G and H (参考图6)整流罩内侧底部前封严和后封严(参考图6)Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-62-350-801小于0.5 inch (12.70mm)的缺口参考78-32-62-350-801修补Upper Rear Inner Seal . See detail J (参考图7 )内侧顶部后封严(参考图7 )Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-69-350-801.小于0.5 inch (12.70mm)的缺口参考78-32-69-350-801修补Inner Cowl/Lower Sidewall Seal and Lower Sidewall Seal . See detail K (参考图8)整流罩内侧/底部侧壁封严和底部侧壁封严(参考图8)Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-71-350-801.小于0.5 inch (12.70mm)的缺口参考78-32-71-350-801修补Upper Sidewall Seal and Upper Inner Sidewall Seal . See detail L (参考图9 )顶部侧壁封严和顶部内侧壁封严(参考图9 )Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-72-350-801.小于0.5 inch (12.70mm)的缺口参考78-32-72-350-801修补Fire Shield . See detail M (参考图 10)防火罩(参考图10)Cuts, Holes, Loose, Worn Parts出现缺口,孔,松动,磨损的部位None Permitted以上四种现象均不允许Small cuts if less than 0.5 inch (12.70mm) 78-32-82-300-801.小于0.5 inch (12.70mm)的缺口参考78-32-82-300-801修补3. Close-up / 结束工作 A. Close Access / 关闭接近 M (1) Make sure that the work area is clean and clear of tools and other items. 确认工作区域干净,无工具和外来物。(2) Close the left and right thrust reverser cowl doors : 关闭左右侧反推整流罩。(Ref. AMM TASK 78-30-00-410-801)(a) FOR 4030EM1 417AL 418AR (b) FOR 4030EM2 427AL 428AR B. Make the thrust reverser serviceable. M 解除反推限动。(Ref. AMM TASK 78-30-00-440-804)C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): T 撤除警告牌,挂签,拆下保险卡子,闭合以下跳开关:

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