WOHA33_472517_8_AT-533100-250-865

Hong Kong Airlines Limited香港航空有限公司F-D-099Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA334725_8_17472517Training and Qualification/培训和资格Technical Record/技术记录NONENONETitleSPECIAL DETAILED INSPECTION ( LFEC) OF SKIN AND SPLICE PLATE IN CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 FROM STR 5 TO STR 15 AND FROM STR 26 TO STR 30, EXTERNAL SURFACE, LH/RHMcd&Rev/厂家工卡&修订日期标题特别详细检查(LFEC) FR 53.6 和 FR53.7之间，从STR 5 到 STR 15 及从STR 26 到 STR 30的周向拼接处的拼接板及蒙皮外表面，左侧/右侧AMM TASK 53-31-00-250-8652018-10-01A/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BLNSAT-533100-250-865HR001002机身/AirframeAIRP/NDT01:30/01:30MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-533180-02-3MPD 533180-02-3,ALI 533180-02-03ISS 3 REV 0SHA10400 CY,31200 FH2100 CY,7400 FHAccess Panels/接近盖板Zones/区域Written/编写Approved/批准NONE2002018-11-162018-12-05TOOLS/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199F53307305001REFERENCE BLOCKTO1ALL(必需/Necessary)29218430连接线TO1ALL(必需/Necessary)3SPO1958探头TO1ALL(必需/Necessary)4M2涡流探伤设备TO1ALL(必需/Necessary)or NORTEC 600 or equivalent/或NORTEC 600或等效工具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1CML06AEA1SEALANTCH1ALL(必需/Necessary)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1CML08BAA9SOLVENT GENERAL PURPOSECH1ALL(视情/As Necessary)2CML14SBA1CLEANING ABSORCH1ALL(视情/As Necessary)3CML08BBB1CLEANERCH1ALL(视情/As Necessary)或/Or CML08BBC14CML08BDA1Non Aqueous Cleaner - Wax and grease removerCH1ALL(视情/As Necessary)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:_AT-533100-250-865 HR001002 W/O:4725 AC:BLNS页码，2 / 8工卡Job card:HA33-533180-02-3TITLESPECIAL DETAILED INSPECTION ( LFEC) OF SKIN AND SPLICE PLATE IN CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 FROM STR 5 TO STR 15 AND FROM STR 26 TO STR 30, EXTERNAL SURFACE, LH/RHPerfInsp标题特别详细检查(LFEC) FR 53.6 和 FR53.7之间，从STR 5 到 STR 15 及从STR 26 到 STR 30的周向拼接处的拼接板及蒙皮外表面，左侧/右侧工作者检查者SPECIAL DETAILED INSPECTION ( LFEC) OF SKIN AND SPLICE PLATE IN CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 FROM STR 5 TO STR 15 AND FROM STR 26TO STR 30, EXTERNAL SURFACE, LH/RH.特别详细检查(LFEC) FR 53.6 和 FR53.7之间，从STR 5 到 STR 15 及从STR 26 到STR 30的周向拼接处的拼接板及蒙皮外表面，左侧/右侧。WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.警 告： 执行工作前，请确保在工作区域及其附近放置安全装置和警告牌： - 飞控系统 - 飞控舵面 - 起落架及相应舱门 - 活动部件 部件移动会造成人员的伤亡或者设备的损坏。WARNING: WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A FALL CAN KILL OR INJURE YOU.警 告：在高空工作请系好安全带，坠落会造成伤亡。WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURERS INSTRUCTIONS AND YOUR LOCAL REGULATIONS.警 告：当使用耗材时，请遵守制造商说明和当地规章。1. Job Set-up/工作准备A. Get Access/接近(1) Put on and attach a safety harness before you start work in the work area. 在检查区域开始工作前，佩戴并系上安全带。(2) Put an ACCESS PLATFORM 10M (33 FT) ADJUSTABLE in position at zone 250. M 在区域250放置一个合适工作梯。(3) Remove the access panels 197AT and 198AT(Ref.AMMTASK53-35-13-000-801). M 拆下接近盖板197AT和198AT（参考AMMTASK53-35-13-000-801）。* ON A/C CRK 401-500/适用于CRK手册有效号为401-500的飞机Subtask53-31-00-020-251-AB. Removal of the Components/部件的移除(1) Remove the scuff plate,(Ref.AMMTASK53-35-15-000-801). M 拆除防磨板（参考AMM TASK 53-35-15-000-801）* ON A/C ALL C. Prepare the Inspection Area检查区域准备工作：(1) Make sure that the inspection area is sufficiently clean to do a satisfactory for M inspection of the area. 确保检查区域足够干净，以便检查。(2) If not, clean the inspection area with Non Aqueous Cleaner-General M (MaterialNo.08BAA9 ) and a Textile-Lint free Cotton (MaterialNo.14SBA1).按需用清洁剂(MaterialNo.08BAA9 )和抹布 (MaterialNo.14SBA1 )清洁检查区域。 (3) If there is a TPS layer and if it does not let you do a satisfactory inspection, remove the TPS layer(Ref.AMMTASK51-78-00-916-801). 若存在TPS保护层且阻碍检查，则移除TPS保护层(参考AMMTASK51-78-00-916-801)。(4) Remove the sealant and/or paint from the inspection area if this is necessary for the M Nondestructive Testing Manual (NTM) task. 若NTM程序要求，去除检查区域的密封胶和/或漆层。2. Procedure/程序A. Inspection (door type 1) / 检查（1类门）(Ref.Fig.Skin in Circumferential Splice and Stringer Coupling Areas (Door Type 1)SHEET1)(参考Fig.Skin in Circumferential Splice and Stringer Coupling Areas (Door Type 1)SHEET1)(1) Do a special detailed inspection (LFEC) of the skin and the splice plate in the T circumferential splice, external surface. Do this inspection between FR53.6 and FR53.7, from STR5 to STR15 and from STR26 to STR30, left and right sides, for damageor discontinuities Ref. NTM533180 特别详细检查(LFEC) FR 53.6和 FR53.7之间，从STR 5 到 STR 15 及从STR 26到STR 30的周向拼接处拼接板及蒙皮外表面，左侧/右侧，对于损伤或断裂，参考NTM533180。(2) Make a report (Ref. NDT REPORT) of the damage after the NTM inspection:NTM检查后记录损伤（参考无损探伤报告）：(a) Corrosion damage: T 腐蚀损伤：If you find corrosion, refer to the Structural Repair Manual Ref. SRM512200 for the corrosion types, inspection, removal and subsequent corrosion protection. 如发现腐蚀，参考SRM 512200确定腐蚀类型、检查方式、去除方法以及后续腐蚀防护措施。Repair Document/修理文件号_(b) Other damage (scratches, cracks, gouges, dents, creases): T 其他损伤（划伤，裂纹，凿伤，凹坑，褶皱）If you find this type of damage, refer to the Structural Repair Manual Ref. SRM511100 for the damage types, classification and corrective action. 如发现此类型损伤，参考SRM 511100确定确定损伤类型，损伤等级和修理方法。Repair Document/修理文件号_(c) Paint layer damage: T 漆层损伤：If you find this type of damage, refer to the Structural Repair Manual Ref. SRM512300 for general data for paint layers. 如果发现这类损伤，参考SRM512300的漆层的相关信息。Repair Document/修理文件号_B. Sealant or Paint Application密封胶或漆层的应用：(1) If the NTM procedure asked to remove the sealant and/or paint from the inspection area,Apply sealant (Ref. SRM512400)or paint (Ref. SRM512300) on the inspection area. T 如NTM步骤要求拆下检查区域的密封胶和/或漆层，在检查区域涂上密封胶(Ref.SRM512400)或漆层(Ref.SRM512300)。3. Close-up/关闭 * ON A/C CRK 401-500/适用于CRK手册有效号为401-500的飞机Subtask53-31-00-420-244-AA. Installation of the Components/部件的安装 T (1) Installation the scuff plate,(Ref.AMMTASK53-35-15-400-801). 安装防磨板（参考AMM TASK 53-35-15-400-801） * ON A/C ALL B. Close Access关闭接近(1) Make sure that the work area is clean and clear of tools and other items. M 确保工作区域干净没有工具和其他物品。(2) Install the access panels 197AT and 198AT (Ref.AMMTASK53-35-13-400-801). M 安装接近面板197AT和198AT (参考 AMMTASK53-35-13-400-801)。C. Put the Aircraft back to its Initial Configuration恢复飞机至初始构型(1) Remove all the fixtures, tools, tes