WOHA33_4846368_221_AT-572000-220-873

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WOHA334846_221_368DIC 4846368Training and Qualification/培训和资格Technical Record/技术记录DICNONETitleSPECIAL DETAILED INSPECTION (US) OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGES.Mcd&Rev/厂家工卡&修订日期标题特别详细检查外侧机翼1至7号肋间的后梁前表面，包括上下法兰AMM 572000-220-8732019-01-01A/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BLHDAT-572000-220-873HR001004机翼/WingMDIC24:00MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-572052-03-7MPD 572052-03-7,ALI 572052-03-07ISS 3 REV 0SHA12500 CY,37600 FH5600 CY,16800 FHAccess Panels/接近盖板Zones/区域Written/编写Approved/批准541BB 541CB 641BB 641CB541 6412019-04-162019-04-16TOOLS/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198A28007570000ADAPTER - VENT AND DRAIN VALVE, APUTO1ALL(必需/Necessary)298D27803000000LOCKING TOOL - FLAP/SLAT CONTROL LEVERTO1ALL(必需/Necessary)30U191067MECHANICAL INPUT - RIGGING PINTO1ALL(必需/Necessary)4PRG224MODULAR PURGE AIR SYSTEMTO1ALL(必需/Necessary)5MSWQC250124591PROBETO1ALL(必需/Necessary)697A28002117002PURGING TOOLTO2ALL(必需/Necessary)799F57204106000REFERENCE BLOCKTO1ALL(必需/Necessary)899F57204135000REFERENCE BLOCKTO1ALL(必需/Necessary)999F57204136000REFERENCE BLOCKTO1ALL(必需/Necessary)1099F57204137000REFERENCE BLOCKTO1ALL(必需/Necessary)1199F57204138001REFERENCE BLOCKTO1ALL(必需/Necessary)120545010SEARCH UNITTO1ALL(必需/Necessary)1398F57103001000SLEEVE,PROTECTIVE-CARBON RODSTO1ALL(必需/Necessary)14MSWQCA01105940WEDGETO1ALL(必需/Necessary)15USN52L超声波仪TO1ALL(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198D27903500000PIN-SIDE STICK LOCKINGTO2ALL(视情/As Necessary)298A53003500000REMOVAL TOOL OF PHILLIPS TORQ-SET FASTENERTO1ALL(视情/As Necessary)or 98A57304002000398F27401000000PITCH TRIM CONTROL LOCKINGTO1ALL(视情/As Necessary)498F28109007000RING, PROTECTIVE - STABILIZER HANDHOLESTO1ALL(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1CML05-002Non Hardening Jointing Putty - Medium Temp. AreaCH1ALL(必需/Necessary)(06LCG9)2CML09-001FUEL TANK SEALANTCH1ALL(必需/Necessary)(06ABA1)3F5725009020000RING-SEALINGAS6ALL(必需/Necessary)4F5725408900200GASKET-KNITTEDAS2ALL(必需/Necessary)5F5725408900000GASKET-KNITTEDAS4ALL(必需/Necessary)6CML06LCG9SINGLE PART CHROMATED JOINTED COMPOUNDCH1ALL(必需/Necessary)708BAA9SOLVENT GENERAL PURPOSECH1ALL(必需/Necessary)814SBA1CLEANING ABSORCH1ALL(必需/Necessary)9CML14CCB6Testing Medium - Leak Detection Oxygen SystemCH1ALL(必需/Necessary)10CML05JBC9ADHESIVECH1ALL(必需/Necessary)11CML03GBD1SYNTHETIC GREASECH1ALL(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1CML15-007CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUNDCH1ALL(视情/As Necessary)(12ACC1)2CML15-008COMPOUNDCH1ALL(视情/As Necessary)(12ACB1)3CML04-024SYNTHETIC GREASECH1ALL(视情/As Necessary)(03GBD1)不适用于所有飞机，具体适用性见AMM 57-27-11-400-801-A/Not applicable to all aircraft, for specific applicability see AMM 57-4CML05-004TESINGCH1ALL(视情/As Necessary)(14CCB6)5CML11-002CLEANERCH1ALL(视情/As Necessary)(08BBB1) or CML11-008(08BBC1)6CML09-002FUEL TANK SEALANT POLYSULFIDECH1ALL(视情/As Necessary)(06ABB1)7CML08-074MASKING TAPECH1ALL(视情/As Necessary)(05RDA1)8CML09-026FLUOROSILICONE SEALANT(DC1200+RTV730)CH1ALL(视情/As Necessary)(06CDD1)9CML04-012VASILINECH1ALL(视情/As Necessary)(03FAB1)10CML15-009ANTICORROSIONCH1ALL(视情/As Necessary)(12ADB1)11CML04-037GENERAL PURPOSE LITHIUM GREASECH1ALL(视情/As Necessary)(03GBC1)不适用于所有飞机，具体适用性见AMM 57-27-11-400-801-A/Not applicable to all aircraft, for specific applicability see AMM 57-12CML15-005CORROSION PREVENTIVE COMPOUND, TEMPORARYCH1ALL(视情/As Necessary)(12ABC1) or CML15-006(12ABB1)13CML04-013ANTI-FRETTING GREASECH1ALL(视情/As Necessary)(03FDG1)不适用于所有飞机，具体适用性见AMM 57-27-11-400-801-A/Not applicable to all aircraft, for specific applicability see AMM 57-14CML05-013RELEASE AGENTCH1ALL(视情/As Necessary)(14DBB1)15CML03FAB1VASILINECH1ALL(视情/As Necessary)16CML03FDG1ANTI-FRETTING GREASECH1ALL(视情/As Necessary)17CML11-032Non Aqueous Cleaner - Wax and grease removerCH1ALL(视情/As Necessary)(08BDA1)18CML14QDB1LOCKWIREAS1ALL(视情/As Necessary)19CML14QBE1WIRE-LOCKINGAS1ALL(视情/As Necessary)(14QBE1)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-572000-220-873 HR001004 W/O:4846 AC:BLHD页码：3 / 13工卡Job card:HA33-572052-03-7TITLESPECIAL DETAILED INSPECTION (US) OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGES.PerfInsp标题特别详细检查外侧机翼1至7号肋间的后梁前表面，包括上下法兰工作者检查者Special Detailed Inspection (US) of Outer Wing Rear Spar Forward Face between Rib 1 and Rib 7 including Top and Bottom Flanges 特别详细检查外侧机翼1至7号肋间的后梁前表面，包括上下法兰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：开始工作前确认安全设备和警告牌在位：- 飞行控制- 飞行控制舵面- 起落架和其相关门- 移动的部件部件的移动可能导致人员伤亡并/或导致设备损坏。WARNING: OBEY THE FUEL SAFETY PROCEDURES. THIS CAN PREVENT INJURY AND DAMAGE. 警 告：遵守燃油安全程序。防止伤害和损伤。WARNING: OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK. THIS WILL PREVENT DEATH, INJURY OR DAMAGE. 警 告：在油箱中工作时需遵守安全程序。防止死亡、伤害或者损伤。WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURERS INSTRUCTIONS AND YOUR LOCAL REGULATIONS. 警 告：使用消耗品时需谨慎。遵守材料制造商和局方规定。1. Job Set-up/工作准备Subtask57-20-00-941-102-A A. Safety Precautions/安全措施 M (1) Obey the fuel safety procedures (Ref.AMMTASK28-10-00-910-801) . 遵守燃油安全程序（参考 AMMTASK28-10-00-910-801）。(2) Put the SAFETY BARRIER(S) in position. 将SAFETY BARRIER(S)放置到位。(3) Install the LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (98D27803000000) on the flap/slat control lever on panel 114VU.在114VU面板上的襟翼/缝翼控制杆上安装LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION (98D27803000000)(4) Put the WARNING NOTICE(S) in these positions:在以下位置放置WARNING NOTICE(S)- On panel 245VU, to tell persons not to operate the fuel system245VU面板上，告知工作者勿操作燃油系统- On panel 990VU, to tell persons not to refuel the aircraft 990VU面板上，告知工作者禁止为飞机加油- On panel 114VU, to tell persons not to operate the flaps. 114VU面板上，告知工作者勿操作襟翼。Subtask57-20-00-865-106-A B. Open, safety and tag this(these) circuit breaker(s): T 打开以下跳开关，并安装跳开关夹及安全标签：Subtask57-20-00-650-093-AC. Defuel/放油 T (1) Defuel the applicable wing fuel tanks (Ref.AMMTASK28-25-00-650-801)(Ref.AMMTASK28-25-00-650-802)(Ref.AMMTASK28-25-00-650-803) .给适当的大翼油箱放油(参考AMMTASK28-25-00-650-801)(参考AMMTASK28-25-00-650-802)(参考AMMTASK28-25-00-650-803)(2) Do the access to fuel tanks and work areas procedure (Ref.AMMTASK28-10-00-910-802) .执行接近油箱及工作区域的准备(参考 AMMTASK28-10-00-910-802)Subtask57-20-00-010-199-A D. Get Access/接近 M (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE below the zone 541(641).在区域541(641)下放置接近梯ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE。(2) Remove the fuel pump fairings (Ref. AMM TASK 28-21-49-000-801).拆下燃油泵整流罩(参考 AMM TASK 28-21-49-000-801)(3) Remove the access panels (Ref.AMMTASK57-27-11-000-801) :拆下接近盖板(参考AMMTASK57-27-11-000-801)- 541AB (641AB), 541BB (641BB) and 541CB (641CB).541AB (641AB), 541BB (641BB) 和 541CB (641CB)(4) Remove the wing internal panel (Ref.AMMTASK57-27-11-000-802) : 拆下大翼内侧盖板(参考AMMTASK57-27-11-000-802)- 541CZ (641CZ). - 541CZ (641CZ)(5) Put a LIGHT SOURCE - SPARK-PROOF in the zone to be inspected. 在区域内放置LIGHT SOURCE - SPARK-PROOF用于检查。Subtask57-20-00-210-141-AE. Preparation of the Inspection Area/检查区域的准备 T (1) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection ofthe area.确保检查区域清洁以便对该区域进行充分的检查。(2) If necessary, clean the inspection area with Non Aqueous Cleaner-General - - (MaterialNo.08BAA9 ) and a Textile-Lint free Cotton - (MaterialNo.14SBA1 ) .如有必要，使用Non Aqueous Cleaner-General - - (MaterialNo.08BAA9 ) 和Textile-Lint free Cotton - (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层且影响检查，移除TPS层(参考AMMTASK51-78-00-916-801)(4) Remove the sealant and/or paint from the inspection area if this is necessaryfor Ref. NTM572052 . 参考NTM572052，如有必要，移除检查区域的封严和/或漆层。2. Procedure/步骤(Ref.Fig.Outer Wing Rear Spar Forward Face Between Rib 1 and Rib 7 Including Top and Bottom Flanges - Location and Detail) (参考图Outer Wing Rear Spar Forward Face Between Rib 1 and Rib 7 Including Top and Bottom Flanges - Location and Detail)Subtask57-20-00-270-073-A A. Inspection/检查 (1) Do the special detailed inspection (US) for damage or discontinuities of the: T 对于下列项目的损伤或断点进行特别详细检查：- Outer-wing rear-spar forward face between RIB1 and RIB7 including top and bottom flanges, Ref. NTM572052 .外侧机翼1至7号肋间的后梁前表面，包括上下法兰，参考NTM572052(2) Make a report of the damage after the NTM inspection: T DICNTM检查后记录损伤：(a) Corrosion damage:腐蚀损伤：- If you find corrosion, refer to the Structural Repair Manual Ref. SRM 51-22-00 for the corrosion types, inspection, removal and subsequent corrosion protection. 若发现腐蚀，参考结构维修手册SRM 51-22-00中腐蚀的类型，检查、清除腐蚀并做防腐措施。Found damage /发现损伤 Yes/是 No/否Repair Document/修理文件号_(b) Other damage (scratches, cracks, gouges, dents, creases): 其他损伤（划痕、裂缝、凿痕、凹痕、折痕）：- If you find this type of damage, refer to the Structural Repair Manual Ref. SRM 51-11-00 for the damage types, classification and corrective action.若发现以上类型损伤，参考结构维修手册SRM 51-11-00中损伤的类型，分类并执行正确的措施。Found damage /发现损伤 Yes/是 No/否If found other damage,please record the damage type若有其他损伤，请记录损伤类型_ Repair Document/修理文件号_Subtask57-20-00-916-053-A 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：禁止将3型临时保护系统（TPS）涂抹在可移动部件上。只能使用1型2级TPS。否则， 机构将不能正确运行。B. Check and Application of the TPS Layer T TPS层的检查和应用NOTE: There is no special requirement about the TPS layer application in this area. The operator can apply the TPS or keep the surface without protection. 注 释：在此区域中，TPS层没有特殊的要求。工作者可以选择应用TPS或保持表面无保护。(1) If the TPS was removed at the Preparation of the Inspection Area, and you select to apply a TPS layer (Ref.AMMTASK51-78-00-916-801) . 若在步骤“Preparation of the Inspection Area”中移除TPS，并选择应用TPS层(参考AMMTASK51-78-00-916-801)。(2) If the TPS was not removed at the Preparation of the Inspection Area, and you select to apply a TPS layer, do a check of the condition and integrity of the TPS layer(Ref.AMMTASK51-78-00-916-801)若在步骤“Preparation of the Inspection Area”中没有移除TPS，并选择应用TPS层，检查TPS层的状态和完整性。(参考AMMTASK51-78-00-916-801)(3) If the TPS layer has local damage, remove the damaged TPS layer and apply a new layer of TPS (Ref.AMMTASK51-78-00-916-801) . 若TPS层存在局部损伤，移除有损伤的TPS层并使用一层新的TPS。(参考 AMMTASK51-78-00-916-801)。NOTE: If, after the check of the condition and integrity, the TPS layer is in the correct condition, and you select to apply a TPS layer, AIRBUS recommends that you apply a new layer as a spray on the existing layer. This is to make sure that the TPS layer continues to give satisfactory corrosion protection. 注 释：若在完成检查状态和完整性后，TPS层状态良好，空客建议在现有TPS层上喷涂 一个新层。为了确保TPS层可以继续提供良好的腐蚀保护。3. Close-up/结束工作Subtask57-20-00-910-051-A A. Sealant or Paint Application T 封严或漆层的应用(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. 若已按NTM步骤要求移除检查区域的封严和/或漆层，在检查区域参考SRM512400涂抹封严或参考SRM512300涂抹漆层。Subtask57-20-00-410-187-A B. Close Access M 关闭接近盖板(1) Make sure that the work area is clean and clear of tools and other items. 确保工作区域清洁并且无工具和其他设备遗留。(2) Install the wing internal panel 541CZ (641CZ) (Ref.AMMTASK57-27-11-400-802) . 安装大翼内侧盖板541CZ (641CZ) (参考AMMTASK57-27-11-400-802)(3) Install the access panels 541AB (641AB), 541BB (641BB) and 541CB (641CB) (Ref.AMMTASK57-27-11-400-801) . 安装接近盖板541AB (641AB), 541BB (641BB) 和541CB (641CB)(参考AMMTASK57-27-11-400-801)(4) Install the fuel pump fairings Ref. AMM TASK 28-21-49-400-801.安装燃油泵整流罩，参考AMM TASK 28-21-49-400-801。Subtask57-20-00-650-094-A C. Refuel /加油 T (