WOHA33_181524AMini Pack29_31_AT-H52-00-00-001

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WOHA331815_31_29适航指令(AD) 培训方式181529通用类/GenericTitleDETAILED VISUAL INSPECTION OF OUTER SKIN RIVETS AND WHOLE INNER FORKS AT THE FRAME FORK END OF FR21 AND FR20B OF THE FORWARD CARGO DOOR.Mcd&Rev/厂家工卡&修订日期标题详细目视检查前货舱门FR 21和FR 20B隔框叉端处整个内部叉端和外蒙皮处的铆钉AOT A330-A52L003-12EASA AD 2012-0274A/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BLNZAT-H52-00-00-001HR001001机身/AirframeAIRP00:30MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-523108-01-1MPD 523108-01-1,EASA AD 2011-0007,AOT A330-A52A3085Issue 2 Revision 5PVGNOTE800 CYAccess Panels/接近盖板Zones/区域Written/编写Approved/批准821AR 821CR 821DR8212015-07-082015-07-08TOOLS/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 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,D.101131* Other: * Signature:_ Authorization No.:_ Date:_AT-H52-00-00-001 HR001001 W/O:1815 AC:BLNZ页码，2 / 7工卡Job card:HA33-523108-01-1TITLEDETAILED VISUAL INSPECTION OF OUTER SKIN RIVETS AND WHOLE INNER FORKS AT THE FRAME FORK END OF FR21 AND FR20B OF THE FORWARD CARGO DOOR.PerfInsp标题详细目视检查前货舱门FR 21和FR 20B隔框叉端处整个内部叉端和外蒙皮处的铆钉工作者检查者DETAILED VISUAL INSPECTION OF OUTER SKIN RIVETS AND WHOLE INNER FORKS AT THE FRAME FORK END OF FR21 AND FR20B OF THE FORWARD CARGO DOOR.详细目视检查前货舱门FR 21和FR 20B隔框叉端处整个内部叉端和外蒙皮处的铆钉A. GENERAL INFORMATION：/通用信息 WARNING: PLEASE OBEY ALL WARNING AND CAUTION OF REFERENCE MANUAL,OTHERWISE IT SHOULD CAUSE PERSONAL INJURE OR DAMAGE TOEQUIPMENTS.警 告：请遵守所参考手册的所有警告和注意事项，否则会造成人员伤害或设备损坏。1. Remove applicable parts to get access inspection area as required按需拆除相应的部件以接近检查区域。2. Obey all of the warnings and cautions given in the specified manual sections.工作中严格遵守相关手册中所有的警告和注意事项要求。3. If the length of fasteners specified in this TASK does not meet the installation standards, fasteners of the same specification, or an approved substitute, one grip length longer or shorter may be used.如果此工卡中给定的紧固件长度不符合安装标准，可选用长度上增加或减少一级的同规格或允许替代的紧固件。4. A Detailed Inspection is defined as: An intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors magnifying lenses, etc. may be necessary. Surface cleaning and elaborate procedures may be required.“详细检查”定义如下：对特定的结构区域、装置或组件进行充分细致的检查以发现有无损伤、失效或异常。检查需要有良好的光源直接照射在检查部位以帮助工作者获得合适的光照强度，可能需要借助反光镜、放大镜等工具，同时可能需要进行表面清洁或其他复杂接近程序。5. These work instructions refer to procedures included on other documents. When the words “refer to” are used and the operator has an accepted alternative procedure, the accepted alternative procedure can be used. When the words “as given in” or “per” are included in the instruction, the procedure in the document must be used.工作步骤中涉及其他文件时，如果使用的是“参照”字样且有其他可接受的替代方法时，该替代方法可以被使用；如果使用的是“按照”字样时，工作者必须使用指定文件中的工作步骤。6. If an airplane has a existing modification or repair that affects a component or system also affected by this task, the technician is responsible for informing Engineer before incorporating this task. If deviation is found during performing this task, the technician is responsible for informing Engineer before continue this task.如果飞机上现有的改装或修理影响到本工卡所涉及的部件或系统，工作者有责任在执行本工卡之前告知工程师。如果本工卡在实际施工过程中有偏离，工作者有责任在采取进一步措施之前告知工程师。B. WORK INSTRUCTIONS /施工步骤1. Close and lock the forward cargo door T 关闭和锁上前货舱门。2. Perform a detailed inspection of outer skin rivets at FR 21 and FR 20B fork ends for loose, T DIC sheared or missing rivets (Refer to APPENDIX 01)参考APPENDIX 01详细检查FR 21和FR 20B隔框叉端外蒙皮处的铆钉是否松动、剪断或丢失。Existing loose, sheared or missing rivets or not/ 是否存在铆钉松动、剪断或丢失：YES / 是 NO/否 3. Remove handle access panels 821CR and 821DR (Refer to APPENDIX 02 and IPC 52-31-11). T 参考APPENDIX 02和IPC 52-31-11拆除接近盖板821CR和821DR.4. Perform an internal detailed inspection of the whole FR 20B and FR 21 forks for cracks and T DIC for loose, sheared or missing rivets at frame web and flanges (Refer to APPENDIX 03).参考APPENDIX 03对整个FR 20B和FR 21隔框进行内部详细检查，检查隔框腹板和缘条是否存在裂纹，铆钉是否存在松动、剪断或丢失。Existing cracks or loose, sheared or missing rivets or not/是否存在裂纹或铆钉松动、剪断或丢失 YES /是 NO /否 a. If crack findings or rivets found sheared, loose