WOHA33_1035BLNG 3C105_245_EOA33-51-0006

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WOHA331035_245_1051035105TitleInspect the Aircraft Exterior Skin Dent DamageMcd&Rev/厂家工卡&修订日期标题检查飞机外部凹坑损伤A/C/飞机号/组别EO JC No./EO工卡EO JC Rev/工卡版本Workarea/工作区域Skill/工种Man Hour/工时BLNG/1EOA33-51-0006R01机身/AirframeAIRP/ENG/ENIN02:00/00:30/02:00Baseline/依据Operator EO/营运人EOEO Rev/EO版本Work Type/工作类别Threshold/首检Interval/重复检AMM 05-21-00,05-22,05-23,05-24EOA33-HKG51-0002R01730CA,10000FH730CA,10000FHWritten/编写Reviewed/审核Approved/批准2013-11-012013-11-112013-11-11Accomplished完工签署Complete Date完工日期Station维修站HKGREASON & DESCRIPTION/原因及描述飞机外部的凹坑，不仅仅影响飞机的气动性能，还会显著缩短受损零部件的疲劳寿命。因此，下发此EO，检查飞机外部蒙皮上的凹坑损伤，为记录和管理飞机外部凹坑损伤提供数据。Unrepaired dent damage at aircraft exterior skin will be reflected in reduced aerodynamic performance,it also will shorten the material fatigue life of the skin parts.For the purpose of collecting the dent damage data, issue this EO to inspect the dent damage at aircraft exterior skin.R01版改版计划信息。R01 revises the plan.TOOLS/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 * 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:_工卡Job card:EOA33-51-0006TITLEInspect the Aircraft Exterior Skin Dent DamagePerfInsp标题检查飞机外部凹坑损伤工作者检查者A. 通用信息/ General Information1. 遵守手册中的所有警告和注意事项.Obey all of the warnings and cautions given in the specified manual sections.2. 一般目视检查是指:对内部或外部,安装或组件的目视检查以发现明显损伤,失效或异常.此检查是在能触及的距离进行的,除非有规定.检查在正常的光源下进行,如日光,吊灯,手电或机库灯光.需要拆下或打开接近盖板或接近门.可能要借助工作台或工作梯接近检查区域.A General Visual Inspection is defined as: A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or irregularity. This level of inspection is made from within touching distance unless otherwise specified. This level of inspection is made under normal available lighting conditions such as daylight, hangar lighting, flashlight or drop-light and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proximity to the area being checked.B. 工作步骤/Work Instruction1. 一般目视检查机身外部蒙皮表面，检查所有凹坑损伤。Do a detailed visual examination for fuselage exterior skin to ensure all dent damages.a. 对于未超出SRM可允许损伤的凹坑，详细目视检查或NDT检查（按需）确定凹坑无其他形式损伤(参考NTM TASK 51-10-08-250-802)。Make sure the unrepaired dents which are less than the allowable damage limits for the applicable SRM no other types of damage by detailed visual examination or using NTM TASK 51-10-08-250-802(as request).b. 对于超出SRM可允许损伤的凹坑，参考SRM或相关技术文件进行修理。Make sure the unrepaired dents which are more than the allowable damage limits for the applicable SRM，According with SRM or other technical docments to repair.2. 一般目视检查机翼外部蒙皮表面及控制舵面（前缘缝翼、克鲁格襟翼、后缘襟翼、副翼、扰流板）表面，检查所有凹坑损伤。Do a GVI for outer wing exterior skin and flight control surface(LE slat、LE flap、TE flap、aileron、spoiler) to ensure all dent damages.对于未超出SRM可允许损伤的凹坑，详细目视检查或NDT检查（按需）确定凹坑无其他形式损伤(参考NTM TASK 51-10-08-250-802)。Make sure the unrepaired dents which are less than the allowable damage limits for the applicable SRM no other types of damage by detailed visual examination or using NTM TASK 51-10-08-250-802(as request).a. 对于超出SRM可允许损伤的凹坑，参考SRM或相关技术文件进行修理。Make sure the unrepaired dents which are more than the allowable damage limits for the applicable SRM，According with SRM or other technical docments to repair.3. 一般目视检查尾翼外部蒙皮表面及控制舵面（升降舵、方向舵）表面，检查所有凹坑损伤。Do a GVI for empennage exterior skin and flight control surface(elevator、rudder) to ensure all dent damages. a. 对于未超出SRM可允许损伤的凹坑，详细目视检查或NDT检查（按需）确定凹坑无其他形式损伤(参考NTM TASK 51-10-08-250-802)。Make sure the unrepaired dents which are less than the allowable damage limits for the applicable SRM no other types of damage by detailed visual examination or using NTM TASK 51-10-08-250-802(as request).b. 对于超出SRM可允许损伤的凹坑，参考SRM或相关技术文件进行修理。Make sure the unrepaired dents which are more than the allowable damage limits for the applicable SRM，According with SRM or other technical docments to repair.4. 一般目视检查发动机进气道蒙皮、风扇包皮及反推包皮，检查所有凹坑损伤。Do a GVI for engine inlet cowl skin、fan cowl skin and thrust reverser outer skin to ensure all dent damages.a. 对于未超出SRM可允许损伤的凹坑，详细目视检查或NDT检查（按需）确定凹坑无其他形式损伤(非多孔材料参考NTM TASK 51-10-14-230-801执行渗透检查，铝合金、钛合金材料参考NTM TASK 51-10-08-250-802执行高频涡流检查)。Make sure the unrepaired dents which are less than the allowable damage limits for the applicable SRM no other types of damage by detailed visual examination or using penetrant inspection as per NTM 511014230801 on nonporous materials or HFEC inspection as per NTM 511008250802 on aluminum or titanium alloy materials (as request).b. 对于超出SRM可允许损伤的凹坑，参考SRM或相关技术文件进行修理。Make sure the unrepaired dents whi