WOHA33_2632393_187_AT-533100-200-860

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_187_393DIC 培训方式2632393通用类/GenericTitleGENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR37.1 AND FR47 FROM Y=-2390 TO Y=2390, COVERED BY BELLY FAIRING, EXTERNAL SURFACE, LH/RH.Mcd&Rev/厂家工卡&修订日期标题整体目视检查FR37.1到FR47从Y=-2390到Y=2390被机腹整流罩覆盖的机身蒙皮和机腹整流罩支撑结构下部外表面AMM 53-31-00-200-8602015-04-01A/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-533100-200-860HR001005机身/AirframeMDIC03:30MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-533035-01-2MPD533035-01-2,MRB533035-01-2Issue 2 Revision 5PVG2190 CA2190 CAAccess Panels/接近盖板Zones/区域Written/编写Approved/批准NONE1902015-05-292015-06-05TOOLS/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198D27803000000LOCKING TOOL - FLAP/SLAT CONTROL LEVERTO1ALL(必需/Necessary)215330-00WINGRIPTO1ALL(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1CML11-003丁酮METHYL-ETHYL-KETONETO1ALL(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1CML09-018SEALANTCH1ALL(必需/Necessary)2CML05-013ACOMPOUNDCH1ALL(必需/Necessary)3CML05-002Non Hardening Jointing Putty - Medium Temp. AreaCH1ALL(必需/Necessary)4CML09-012SEALENTCH1ALL(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1CML11-026SOLVENT GENERAL PURPOSECH1ALL(视情/As Necessary)or/或 08BAA92CML11-002CLEANERCH1ALL(视情/As Necessary)3CML09-014CORROSION INHIBITIVE COATINGCH1ALL(视情/As Necessary)4CML08-018ADHESIVECH1ALL(视情/As Necessary)5CML09-002FUEL TANK SEALANT POLYSULFIDECH1ALL(视情/As Necessary)或CML09-0166CML08-074MASKING TAPECH1ALL(视情/As Necessary)or/或 05RDA17CML04-012VASILINECH1ALL(视情/As Necessary)8CML07-001Varnish- Electrical Bonding StructureCH1ALL(视情/As Necessary)9CML15-009ANTICORROSIONCH1ALL(视情/As Necessary)or/或 12ADB110CML09-001FUEL TANK SEALANTCH1ALL(视情/As Necessary)11CML08-019FOIL, POLYESTER, PRESSURE SENSITIVECH1ALL(视情/As Necessary)or/或 05RCB112CML11-032Non 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-533100-200-860 HR001005 W/O:2632 AC:BLNV页码，2 / 10工卡Job card:HA33-533035-01-2TITLEGENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND BELLY FAIRING SUPPORT STRUCTURE LOWER PART BETWEEN FR37.1 AND FR47 FROM Y=-2390 TO Y=2390, COVERED BY BELLY FAIRING, EXTERNAL SURFACE, LH/RH.PerfInsp标题整体目视检查FR37.1到FR47从Y=-2390到Y=2390被机腹整流罩覆盖的机身蒙皮和机腹整流罩支撑结构下部外表面工作者检查者General Visual Inspection of Fuselage Skin and Belly Fairing Support Structure Lower Part between FR37.1 and FR47 from Y=-2390 to Y=2390 Covered by Belly Fairing, External Surface, LH/RH.整体目视检查FR37.1到FR47从Y=-2390到Y=2390被机腹整流罩覆盖机身蒙皮和机腹整流罩支撑结构下部外表面WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURERS INSTRUCTIONS AND YOUR LOCAL REGULATIONS. 警 告：使用消耗品时要当心，请遵守材料生产厂家使用说明和当地的使用规范1. Job Set-up/工作开始A. Get Access/接近 T (1) Put an ACCESS PLATFORM 2M (6 FT) in position below the belly fairing, between FR37.1 and FR47. 将接近平台放置在FR37.1到FR47的机腹下方。(2) Remove the belly-fairing access panels between FR37.1 and FR39.1 (Ref. AMM TASK 53-35-13-000-801) . 拆下FR37.1到FR39.1的机腹接近面板。(参考AMM TASK 53-35-13-000-801)(3) Remove the belly-fairing access panels between FR39.1 and FR47 (Ref. AMM TASK 53-35-13-000-802) . 拆下FR39.1到FR47的机腹接近面板。(参考AMM TASK 53-35-13-000-802)(4) Remove the wing-to-fuselage fairings between FR37.1 and FR47 (Ref. AMM TASK 53-35-11-000-801) . 拆下FR37.1到FR47翼上整流罩(参考AMM TASK 53-35-11-000-801) . B. Prepare the Inspection Area 检查区域的准备工作(1) Make sure that the inspection area is clean to do a satisfactory inspection of the area. M 确认检查区域足够清洁满足检查的需要 (2) If the inspection area is not clean, clean it with Material No. 08BAA9 (Non Aqueous M Cleaner-General) and a lint-free cotton cloth Material No. 14SBA1 (Textile-Lint free Cotton ) . 若检查区域不够清洁，请用清洁剂和抹布清洁(3) If you cannot do a satisfactory inspection because of the TPS layer, remove the TPS layer M (Ref. AMM TASK 51-78-00-916-801) .若TPS保护层影响检查，请去除TPS保护层（参考AMM TASK 51-78-00-916-801）2. Procedure/步骤A. Inspection/检查 (Ref. Fig. Fuselage Skin and Belly Fairing Structure SHEET 1) (Ref. Fig. Fuselage Skin and Belly Fairing Structure SHEET 2)(参考Fig. Fuselage Skin and Belly Fairing Structure SHEET 1) (参考Fig. Fuselage Skin and Belly Fairing Structure SHEET 2)(1) Do a general visual inspection between FR37.1 and FR47: T DIC 整体目视检查位于FR37.1到FR47之间的-of fuselage skin below the belly fairing 机腹整流罩下的机身蒙皮-of belly-fairing support structure below the belly fairing. 机腹整流罩下的机身蒙皮支撑结构。(2) Make sure that there is no/确保无: (a) Corrosion damage/腐蚀损伤: -If you find corrosion damage, refer to the Structural Repair Manual SRM 51220001 T for types of damage, inspection, removal and corrosion protection. 如果找到腐蚀损伤，参见SRM 512200确定腐蚀类型，检查，清除和后续腐蚀保护方法。 (b) Erode damage/风蚀损伤： T -If you find erode damage, refer to DMDOR330-53-003R00 for types of damage,inspection, maintenance program.The typical erode damage refer to Figure1、2、3. 如果发现风蚀损伤，参考DMDOR330-53-003R00确定其损伤类型，检查和修理方案。典型 的风蚀损伤详见图1、2、3所示。(c) Other damage (cracks, scratches, stress, marks, dents, bumps,.): 其他损伤（裂纹，划伤，应力，痕迹，凹坑，冲击）-If you find this type of damage, refer to the Structural Repair Manual SRM 51110001 T for types of damage and corrective action. 若发现这些类型的损伤，参见SRM 511100确定损伤类型，分类和纠正措施。 B. Temporary Protection System 临时保护系统CAUTION: DO NOT APPLY TEMPORARY PROTECTION SYSTEM (TPS) TYPE 3 TO THE MOVABLE COMPONENTS. ONLY TPS TYPE 1 GRADE 2 MUST BE USED. IF YOU DO NOT OBEY THIS INSTRUCTION, THE MECHANISMS WILL NOT OPERATE CORRECTLY. 注 意：禁止在活动部件上使用临时保护层TYPE 3，只能使用TPS TYPE 1 GRADE 2 若不遵守此使用说明，会使机构不能正确操作(1) If there is a TPS layer, make sure that it is in the correct condition T (Ref. AMM TASK 51-78-00-916-801) . 若有TPS保护层，请确保其处于良好的状态（参考AMM TASK 51-78-00-916-801）NOTE: Airbus recommends that you always apply a new layer of TPS. This is to make sure that the TPS layer continues to give satisfactory corrosion protection. If, after the check, you think that the TPS layer is in the correct condition, you can spray a new layer on the existing layer. 注释：空客建议使用全新的TPS保护层，这样能够确保持续良好的防腐效果，若检查后， 确认TPS保护层处于良好的状态，也可在已存在的保护层上喷涂新的保护层 (2) If the TPS layer has local damage, remove the damaged TPS layer T (Ref. AMM TASK 51-78-00-916-801) and apply a new layer of Material No. 12ADB1 (Corrosion Preventive Compound-Water Displacing & Heavy Duty Hard Film -) on the inspection area (Ref. AMM TASK 51-78-00-916-801) . 若TPS有局部损伤，去除损伤的TPS保护层，（参考AMM TASK 51-78-00-916-801）并在检查区域用No. 12ADB1建立新的保护层 (3) Apply a full new layer of Material No. 12ADB1 (Corrosion Preventive Compound-Water T Displacing & Heavy Duty Hard Film -) on the inspection area (Ref. AMM TASK 51-78-00-916-801) if, before the inspection: 若检查前进行了以下程序，请用No. 12ADB1建立全新保护层：- You removed the TPS layer, or 去除TPS保护层，或者- You cleaned the inspection area with high-pressure water, steam, solvents and/or cleaning agents. 用高压水，蒸汽，溶剂和/或清洁剂清洁检查区域3. Close-up/结束 A. Close Access/关闭接近 T (1) Install the belly-fairing access panels between FR37.1 and FR39.1 (Ref. AMM TASK 53-35-13-400-801) . 安装FR37.1到FR39.1的机腹接近面板。(参考AMM TASK 53-35-13-400-801)(2) Install the belly-fairing ac