WOHA33_4451325_97_AT-H28-00-00-002

Hong Kong Airlines LimitedHong Kong Air Cargo Carrier Limited香港航空有限公司香港货运航空有限公司03110-01Hong Kong Airlines MEDHong Kong Airlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA334451_97_325DM DIC AD 4451325Training and Qualification/培训和资格Technical Record/技术记录ETOPS DICAD CAOTitleA330 Aircraft Inspection of Fuel Pump(FIN 600QL1/600QL2/112QA1/112QA2)Cavitation ErosionMcd&Rev/厂家工卡&修订日期标题A330飞机检查燃油泵（FIN 600QL1/600QL2/112QA1/112QA2）空腔腐蚀AOT A28L006-17/R2,AD 2017-0224,CAD2017-MULT-67,VSB 8810-28-06/R1A/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BLNXAT-H28-00-00-002HR000004机翼/WingAIRP/MINP02:00/01:00MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-28-COME-010EASA AD 2017-0224,AOT A28L006-17,VSB 8810-28-06ISS 3 REV 0PVG10000 FH,NOTE 15000 FH,NOTE 2Access Panels/接近盖板Zones/区域Written/编写Approved/批准NONENONE2018-12-042018-12-14TOOLS/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198A28201003000FUEL PUMP, SHROUD TOOLTO1ALL(必需/Necessary)或/or 98F28001075000TOOLS 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1754-4-24860-013RING-SEALINGAS1ALL(必需/Necessary)2754-4-25183-176RING-SEALINGAS1ALL(必需/Necessary)3754-4-25183-179RING-SEALINGAS1ALL(必需/Necessary)4CML08BAA9SOLVENT GENERAL PURPOSECH1ALL(必需/Necessary)5CML14SBA1CLEANING ABSORCH1ALL(必需/Necessary)6CML03FAB1VASILINECH1ALL(必需/Necessary)7CML14QFB1LOCKWIREAS1ALL(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1NAS1790-3R4BOLTAS5ALL(视情/As Necessary) FIN 112QA1/22NAS1790-3R5BOLTAS2ALL(视情/As Necessary) FIN 112QA1/23MS21075-3NNUT-LOCKAS1ALL(视情/As Necessary)FIN 112QA1/24568-1-28300-103PUMP-FUELXFR ELEMENT TK4AS1ALL(视情/As Necessary)5NSA5067-3-2NUT-CLIPAS5ALL(视情/As Necessary)FIN 112QA1/26AGS2067-308RIVETAS2ALL(视情/As Necessary)FIN 112QA1/27568-2-28372-000SCREWAS6ALL(视情/As Necessary)PARTS INFORMATION/部件信息:NOTE: The component in PN,SN form is need to do periodic maintenance. For the return repair or retrofit，the form is PN,SN of the removed component. And the PN-IN,SN-IN would be written according to new parts after finish. For the non- returns(such as weight, test)，the form is PN,SN of the on-wing maintenance component. And fill the PN-IN,SN-IN with bias after finish.注释：件号、序号栏指需要定期执行维修工作的部件。对于要求更换拆下返厂工作的部件，该栏指拆下件、序号信息。完成工作后装上件号和序号栏请填写相关装机件信息；对于在位执行工作的（如称重、测试等），该栏指在位工作部件件、序号信息，完成工作后装上件号和序号请用斜线画去。PN/件号SN/序号ATA/章节ZONE/区域FIN/代码LOCATION/装机位置568-1-28300-103A074592821640A3300915112QA2PN-IN装上件号SN-IN装上序号REMOVAL REASON AND COMPONENT TASK REQUEST拆件原因及其部件工作要求TASK NOTE工作注释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-H28-00-00-002 HR000004 W/O:4451 AC:BLNX页码，2 / 16工卡Job card:HA33-28-COME-010TITLEA330 Aircraft Inspection of Fuel Pump(FIN 600QL1/600QL2/112QA1/112QA2)Cavitation ErosionPerfInsp标题A330飞机检查燃油泵（FIN 600QL1/600QL2/112QA1/112QA2）空腔腐蚀工作者检查者WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.警 告：确保遵守相关程序中所有的警告和注意事项。Note: Verify the position of the fuel pump that the card requires,If the part fitted on position of FIN 600QL1/600QL2,apply the procedure A and feedback; If the part fitted on position of FIN 112QA1/112QA2,apply the procedure B and feedback;If the location specified by EO is not FIN 600QL1/600QL2/112QA1/112QA2, then directly sign N/A to close work ,without completing the feedback form and sending the email.注释：核实工卡要求检查的燃油泵的安装位置。如果安装位置在FIN 600QL1/600QL2，则采用步骤A完成检查和反馈工作；如果燃油泵的安装位置在FIN 112QA1/112QA2，则采用步骤B完成检查和反馈工作；如果工卡要求检查的燃油泵不在FIN 600QL1/600QL2/112QA1/112QA2位置上，则直接签署N/A关闭工卡，无需填写反馈表格和邮件反馈。A. FIN 600QL1/600QL2 pump checkIN 600QL1/600QL2燃油泵检查Note:If you find the actual PN or SN is not same with the one required by this job card, please continue to perform this inspection for the specific position required by this job card.Record in the feedback form.注释：如果发现装机实物同此份工卡要求检查的件序号不符，仍需要对工卡中指定的位置执行检查，并记录在反馈表中。1. Remove the pump from the A/C refer to AMM 28-26-51-000-801-A. T 参考AMM 28-26-51-000-801-A，从飞机上拆下燃油泵。2. Perform a detailed visual inspection of the vane of the pump at the location indicated T DIC on Figures 1 and Figures 2.Taking pictures. 参考图1和图2位置对燃油泵进行详细目视检查，并拍照记录。Case 1: Light Erosion (blemishing):样例1：轻度腐蚀（缺陷）- Surface blemishing with grey anodise treatment removed from web表面缺陷，灰色阳级涂层脱落- Base material has begun to erode with light blemishing without pitting or cavity.基底材料开始轻度腐蚀，但没有点蚀或者洞。Case 2: Medium Erosion (pitting):样例2：中度腐蚀（点蚀）- An extensive surface blemishing with grey anodise treatment removed from web较大范围表面缺陷，灰色阳级涂层脱落 - Base material has eroded with pitting or single or multiple shallow cavities T 基底材料有点蚀，或者单个或多个的浅洞 Case 3: Severe Erosion : 样例3：严重腐蚀- Base material is heavily eroded with pitting and single, multiple deep cavities or breakthrough.基底材料由严重腐蚀，发现点蚀和单个或多个深洞，或穿透。 a. No findings or Light erosion findings (blemishing): the pump is acceptable for flight. 无发现或轻度腐蚀：泵是可接受的。 b. Medium erosion findings (pitting): the pump is not acceptable for flight and must bereplaced immediately.中度腐蚀（点蚀）：泵是不可接受的，需要立即更换。c. Severe erosion findings : the pump is not acceptable for flight and must bereplaced immediately.严重腐蚀: 泵是不可接受的，需要立即更换。Note：For Center tank, it is possible to deactivate the pump. Refer to MEL Items 28-26-02 can be applied provided that respectively the circuit breaker 1QL1(2) is pulled and tagged for the duration of the MEL Item .注释：对于中央油箱，在没有航材的情况下可以保留燃油泵，参考MEL 28-26-02且对应的跳开关1QL1(2)需要被拔出并贴标牌。3. Perform a detailed visual inspection of the vane of the pump at the location indicated T on Figures 3.If there are any vane plate cavitation erosions out of limit refer to Case 4,then the pump must be replaced.参考图3位置对燃油泵叶轮盘进行详细目视检查，如发现超出样例4中标准的叶轮盘空腔腐蚀，则需要更换泵。 Case 4: Vane Plate Cavitation Erosion 样例4：叶轮盘空腔腐蚀Acceptable/可接受标准: Any extensive surface blemishing with grey anodise treatment removed from the vane.-表面缺陷，灰色阳级涂层从叶轮盘脱落 Base material has eroded with pitting or single or multiple shallow cavities.-基底材料有点蚀，或者单个或多个的浅洞 Guidance: Cavity depths less than approximately 1.5mm (0.030)-凹坑深度小于1.5mm(0.030英寸)4. Install the Fuel pump refer to AMM 28-26-51-400-801-A. T DIC 安装燃油泵参考AMM 28-26-51-400-801-A。5. Record the result to appendix 1. Send the photo and appendix 1 to Email： T T； ；；;在附录1表格中记录检查结果。将检查的实物照片和附录1，反馈至Email：T； ；；;Note：Feedback title: AD2017-0224+AC REG+PN&SN.Feedback attachment: name with PN&SN. The Email need less than 10MB. TSN and CSN can find in amicos refer to figure 3.注释：反馈标题：AD2017-0224+飞机号+件序号。反馈附件：命名使用件序号。邮件不能大于10MB。TSN和CSN可参考图3在amicos系统中查询。B. FIN 112QA1/112QA2 pump check112QA1/112QA2燃油泵检查Note:If you find the actual PN or SN is not same with the one required by this job card, please continue to perform this inspection for the specific position required by this job card.Record in the feedback form.注释：如果发现装机实物同此份工卡要求检查的件序号不符，仍需要对工卡中指定的位置执行检查，并记录在反馈表中。1. Remove the pump from the A/C refer to AMM TASK 28-21-51-000-802-A. T 参考AMM 28-21-51-000-802-A，从飞机上拆下燃油泵。2. Perform a detailed visual inspection of the vane of the pump at the location indicated T DIC on Figures 1 and Figures 2.Taking pictures. 参考图1和图2位置对燃油泵进行详细目视检查，并拍照记录。Case 1: Light Erosion (blemishing):样例1：轻度腐蚀（缺陷）- Surface blemishing with grey anodise treatment removed from web表面缺陷，灰色阳级涂层脱落- Base material has begun to erode with light blemishing without pitting or cavity. T 基底材料开始轻度腐蚀，但没有点蚀或者洞。Case 2: Medium Erosion (pitting):样例2：中度腐蚀（点蚀） - An extensive surface blemishing with grey anodise treatment removed from web较大范围表面缺陷，灰色阳级涂层脱落 - Base material has eroded with pitting or single or multiple shallow cavities基底材料有点蚀，或者单个或多个的浅洞Case 3: Severe Erosion 样例3：严重腐蚀- Base material is heavily eroded with pitting and single, multiple deep cavities or breakthrough.基底材料由严重腐蚀，发现点蚀和单个或多个深洞，或穿透。a. No findings or Light erosion findings (blemishing): the pump is acceptable for flight. 无发现或轻度腐蚀：泵是可接受的。b. Medium erosion findings (pitting): the pump is not acceptable for flight and must be replaced immediately.中度腐蚀（点蚀）：泵是不可接受的，需要立即更换。 c. Severe erosion findings : the pump is not acceptable for flight and must be replaced immediately.严重腐蚀: 泵是不可接受的，需要立即更换。3. Perform a detailed visual inspection of the vane of the pump at the location indicated T on Figures 3.If there are any vane plate cavitation erosions out of limit refer to Case 4,then the pump must be replaced.参考图3位置对燃油泵叶轮盘进行详细目视检查，如发现超出样例4中标准的叶轮盘空腔腐蚀，则需要更换泵。 Case 4: Vane Plate Cavitation Erosion 样例4：叶轮盘空腔腐蚀Acceptable/可接受标准: Any extensive surface blemishing with grey anodise treatment removed from the vane.-表面缺陷，灰色阳级涂层从叶轮盘脱落 Base material has eroded with pitting or single or multiple shallow cavities.-基底材料有点蚀，或者单个或多个的浅洞 Guidance: Cavity depths less than approximately 1.5mm (0.030)-凹坑深度小于1.5mm(0.030英寸)4. Install the Fuel pump refer to 28-21-51-400-802-A. T DIC 安装燃油泵参考AMM 28-21-51-400-802-A。5. Record the result to appendix 1. Send the photo and appendix 1 to Email： T T； ；；;在附录1表格中记录检查结果。将检查的实物照片和附录1，反馈至Email：T； ；；;Note：Feedback title: AD2017-0224+AC REG+PN&SN.Feedback attachment: name with PN&SN. The Email need less than 10MB. TSN and CSN can find in amicos refer to figure 3.注释：反馈标题：AD2017-0224+飞机号+件序号。反馈附件：命名使用件序号。邮件不能大于10MB。TSN和CSN可参考图3在amicos系统中查询。AT-H28-00-00-002 HR000004 2018-12-04页码/Page9 / 16工卡Job card:HA33-28-COME-010TITLEA330 Aircraft Inspection of Fuel Pump(FIN 600QL1/600QL2/112QA1/112QA2)Cavitation ErosionPerfInsp标题A330飞机检查燃油泵（FIN 600QL1/600QL2/112QA1/112QA2）空腔腐蚀工作者检查者图1/Figure 1图2/Figure 2图3/Figure 3图3/Figure 3技术文件反馈单/TECHNICAL FEEDBACK FORM工程师填写以下内容/FILLED BY ENGINEER：技术文件号/TECH NO.AT-H28-00-00-002技术文件标题/TITLEA330飞机检查燃油泵(FIN 600QL1/600QL2 /112QA1/112QA2)空腔腐蚀A330 Airc