WOHA33_103754_260_AT-352200-710-803

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WOHA331037_260_54培训方式103754通用类/GenericTitleOPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEMMcd&Rev/厂家工卡&修订日期标题操作检查发动机非包容保护系统AMM 352200-710-803 2014-07-01A/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BLNLAT-352200-710-803HR004006电气/ElectricAIRP08:00MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-352200-07-2MPD 352200-07-2,CMR* 352002-00001-1-C,MRB 35.20.02/13Issue 2 Revision 4HKG1825 CA,15000 FH1825 CA,15000 FHAccess Panels/接近盖板Zones/区域Written/编写Approved/批准132QW 261UW2102014-09-302014-09-30TOOLS/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1110111-36COUPLING - OXYGEN QUICK DISCONNECTTO1ALL(必需/Necessary)298A52307628000LOCK - SAFETY, CARGO DOOR ACTUATORSTO1ALL(必需/Necessary)398F52308227002SUPPORT STRUT - CARGO DOORTO2ALL(必需/Necessary)或 98F523082790004CML11-003丁酮METHYL-ETHYL-KETONETO1ALL(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1CML09-016SEALANTCH1ALL(必需/Necessary)2CML11-026SOLVENT GENERAL PURPOSECH1ALL(必需/Necessary)3CML11-004CLEANERCH1ALL(必需/Necessary)4CML19-003CLEANING ABSORCH1ALL(必需/Necessary)5995000TOOL -MANUAL RELEASEAS1ALL(必需/Necessary)6CML08-005SEALING TAPECH1ALL(必需/Necessary)7CML08-013SEALANT, ANAEROBICCH1ALL(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1CML08-001EPOXY ADHESIVECH1ALL(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 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,D101131* Other: * Signature:_ Authorization No.:_ Date:_AT-352200-710-803 HR004006 W/O:1037 AC:BLNL页码，2 / 23工卡Job card:HA33-352200-07-2TITLEOPERATIONAL CHECK OF ENGINE BURST PROTECTION SYSTEMPerfInsp标题操作检查发动机非包容保护系统工作者检查者Operational Check of the Engine-Burst Protection System操作检查发动机非包容保护系统WARNING：IF, DURING ACCOMPLISHMENT OF THIS TASK, DISCREPANCIES ARE DETECTED,WITHIN THE APPLICABLE COMPLIANCE TIME SPECIFIED IN THE AIRBUS MAINTENANCE DOCUMENTATION, ACCOMPLISH THE APPLICABLE CORRECTIVEACTIONS IN ACCORDANCE WITH INSTRUCTIONS SPECIFIED (OR INCORPORATED BY REFERENCE) IN THE APPLICABLE AIRBUS MAINTENANCE DOCUMENTATION. IF NO COMPLIANCE TIME IS IDENTIFIED IN AIRBUS MAINTENANCE DOCUMENTATION, BEFORE NEXT FLIGHT, ACCOMPLISH THE APPLICABLE CORRECTIVE ACTION(S), OR CONTACT AIRBUS FOR APPROVED INSTRUCTIONS AND WITHIN THE COMPLIANCE TIME SPECIFIED THEREIN, ACCOMPLISH THOSE INSTRUCTIONS ACCORDINGLY. IF ANY OF THE DISCREPANCIES DETECTED DURING ACCOMPLISHMENT OF ANY TASK, IS NOT IDENTIFIED IN THE AIRBUS MAINTENANCE DOCUMENTATION, BEFORE NEXT FLIGHT, CONTACT AIRBUS FOR APPROVED INSTRUCTIONS AND ACCOMPLISH THOSE INSTRUCTIONS ACCORDINGLY.(THE ABOVE REQUIREMENT IS ACCORDING TO AD 2013-0245)警 告：如果在执行此工作时发现任何故障、缺陷，在空客维护手册要求的时间范围内，按照适用的空客维护手册采取相应的纠正措施。 如果在空客维护手册中未明确完成期限，那么，在下一次飞行前完成相应纠正措施，或者要求工程联系空客提供经批准的维护方案并在维护方案中要求的完成期限内，完成相关措施。 如果在执行此工作时发现的问题，空客没有相关的维护手册提及，那么，在下一次飞行前，要求工程联系空客提供经批准的维护方案，并参照维护方案完成相关措施。（以上要求来源于AD 2013-0245的要求）。WARNING: KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL SOURCES OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. 警 告：保持所有的碳氢化合物（燃油，润滑脂，等）远离所有氧气源。否则会导致爆炸。WARNING: CLEAN THE TOOLS AND MAKE SURE YOUR HANDS ARE CLEAN TO PREVENT CONTAMINATION OF THE OXYGEN SYSTEM. 警 告：确保双手和工具保持清洁，以防止污染氧气系统。1. Job Set-up / 开始工作A. Aircraft Maintenance Configuration / 飞机维护构型 T (1) Obey the special precaution when you work on a gaseous oxygen system (Ref. AMM TASK 35-00-00-860-801) .对气态氧气系统执行工作时，请遵守特殊防范要求(参考AMM TASK 35-00-00-860-801)。(2) Energize the ground service network (Ref. AMM TASK 24-42-00-861-801) . 接通地面勤务电源 (参考AMM TASK 24-42-00-861-801)。(3) In the cockpit, on the OXYGEN section of the overhead panel 211VU: 在驾驶舱内，头顶板211VU的氧气（OXYGEN）部分：(a) Put the WARNING NOTICE(S) to tell persons not to operate the emergency oxygen system. 悬挂警告牌，禁止操作应急氧气系统。B. Get access to the avionics compartment. Then make sure that this(these) circuit T breaker(s) is (are) closed:进入电子舱。确认下列跳开关闭合：PANELDESIGNATIONFINLOCATION742VUPAX OXY CTL4WRC80742VUPAX OXY CTL3WRC79742VUPAX OXY CTL2WRC78742VUPAX OXY CTL1WRC77742VUQCCU901WRC67742VUPAX OXY CTL & IND900WRC66 C. Get Access/接近 T (1) Put the a WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the emergency oxygen system. 在驾驶舱中放置警告牌在位，禁止操作应急氧气系统。(2) Open the forward cargo-compartment door (Ref. AMM task 52-30-00-010-801) 打开前货舱门(参考. AMM task 52-30-00-010-801)(3) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the forward cargo-compartment door.在前货舱门处放置一合适工作梯。(4) In the forward cargo compartment, on service panel 5022VE, set theCARGO COMPT LIGHT switch to the ON position.在前货舱勤务面板5022VE上，将CARGO COMPT LIGHT电门设置在ON位。(5) Remove the sidewall panels 132NW, 132FX, 132UW and 132WW (Ref. AMMtask 25-52-00-000-801) 拆除侧壁板132NW, 132FX, 132UW 和132WW (参考AMM task 25-52-00-000-801)(6) Remove the ceiling panels 262NC, 252AC and 252LC (Ref. AMM task 25-23-41-000-801).拆下天花板262NC, 252AC 和 252LC(参考 AMM task 25-23-41-000-801) 。(7) On all of the emergency oxygen containers, pull out test button and turn them 90 degrees to the TEST position.在所有应急氧气盒上，拉出测试旋钮并旋转90度到测试位。(8) Close the manual shutoff valves of all emergency oxygen cylinders.关闭所有应急氧气瓶上的人工关断活门。(9) Put a WARNING NOTICE(S) on the emergency oxygen cylinders to tell persons not to operate the manual shutoff valves.在应急氧气瓶上挂警告牌，禁止操作人工关断活门。D. Get access to the avionics compartment. Then open, safety and tag this(these) T circuit breaker(s): 进入电子舱，拔出下列跳开关，设置安全夹并挂上安全标牌：PANELDESIGNATIONFINLOCATION721VUCMC1 SWTG4TM1U07722VUSDAC 22WV2H49742VUCMC 13TM1N72742VUSDAC 12WV1Q79742VUPAX OXY ACTUATION5WRP76742VUPAX OXY ACTUATION6WRP75E. Aircraft Maintenance Configuration / 飞机维护构型 T (1) Disconnect the electrical connector 970WR-A from the low pressure switch 970WR.从低压电门970WR上断开电接头970WR-A。(2) Connect an electrical bridge between the pins A and C on the electrical connector 970WR-A.在电气接头970WR-A的销钉A和C之间连接电桥。(3) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-801) .执行EIS启动程序 (参考AMM TASK 31-60-00-860-801)。(4) Make sure that there are no failure messages shown on the DOORS/OXY page of the ECAM.确认在ECAM的DOORS / OXY页面没有显示失效信息。F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): T 摘除安全夹和安全标牌，闭合下列跳开关：PANELDESIGNATIONFINLOCATION721VUCMC 1 SWTG4TM1U07722VUSDAC 22WV2H49742VUCMC 13TM1N72742VUSDAC 12WV1Q79 G. Installation of the Ground Service Equipment T 安装地面勤务设备。WARNING: MAKE SURE THAT THE GROUND SUPPORT EQUIPMENT IS APPROVED FOR THE OXYGEN SYSTEM. EQUIPMENT THAT IS NOT APPROVED CAN CAUSE CONTAMINATION OF THE SYSTEM AND INJURY. 警 告：确认氧气系统的地面支持设备经过检验。未经检验的设备可引起系统污染并对人有害。CAUTION: DO NOT INSTALL A BLANKING PLUG IN THE PRESSURE SENSING PORT OF THE OXYGEN PRESSURE REGULATOR. IF A BLANKING PLUG IS INSTALLED, THE REGULATOR VALVE WILL NOT OPERATE CORRECLY. THUS THERE IS A RISK THAT THE OXYGEN SUPPLY TO THE PASSENGERS WILL NOT BE SUFFICIENT. 注 意：不要在氧气压力调节器的压力探测口上安装堵塞，如果安装了堵塞，该调节活门将无法正常工作，这存在无法向旅客供应足够氧气的风险。(1) Remove the cap from the test port 7504WR1. 从测试口7504WR1上拆下盖子。(2) Connect the NITROGEN COMPRESSED SOURCE - GROUND with the devices that follow to the test port 7504WR1: 将带有下列设备的氮气压力源连接到测试口7504WR1：- A GAGE 20 BAR (290 PSI) - PRESSURE 20 BAR (290 PSI)的压力表- A VALVE - SHUT OFF 关断活门- A DEVICE - VENT 通风装置- A DEVICE - OVERPRESSURE 超压装置- A COUPLING - OXYGEN QUICK DISCONNECT (110111-36) . 氧气快卸接头(110111-36)NOTE: The volume of the test equipment between the shutoff valve and the test port must be as small as possible. If the volume is too large, it will have an effect on the test results. 注 释：在关断活门和测试口之间连接的测试设备的体积应该尽可能的小，如果体积过大，将影响测试结果。2. Procedure / 步骤(Ref. Fig. Test Port 7504WR1 and Bleed Vent Valve 7503WR SHEET 1) (Ref. Fig. Test Port 7504WR1 and Bleed Vent Valve 7503WR SHEET 2)(参考图. Test Port 7504WR1 and Bleed Vent Valve 7503WR SHEET 1) (参考图. Test Port 7504WR1 and Bleed Vent Valve 7503WR SHEET 2)A. Functional Test of the Engine-Burst Protection System 功能检查发动机非包容保护系统ACTIONRESULT T 1. In the avionics compartment / 在电子舱：- Open the circuit breakers 3WR and 4WR.拔出跳开关3WR和4WR。 T 2. At the differential pressure switch 950WR: 在压差电门950WR处：- Remove the electrical connector 950WRA. 拆下电接头950WRA- Install an electrical bridge between the connections 950WRA-E and 950WRA-F. 在950WRA-E 和 950WRA-F之间连接电桥。 T 3. In the avionics compartment: 在电子舱内：- Close the circuit breakers 3WR and 4WR.闭合跳开关3WR和4WR。 T 4. On the overhead panel 211VU: 在头顶板211VU上：- Lift the guard and push the MASK MAN ON pushbutton switch.提起保护盖并按压MASK MAN ON 按钮电门。At the shutoff-valve 920WR2: 在关断活门920WR2：- The main distribution shutoff-valve 920WR2 closes. 主分配关断活门920WR2关闭。At the shutoff-valve 920WR1: 在关断活门920WR1：- The main distribution shutoff-valve 920WR1 is open.主分配关断活门920WR1打开。In the cabin / 在客舱：- If PRAM or I-PRAM is installed, the emergency announcement is heard.如果安装了PRAM 或 I-PRAM，可听到紧急通告。 T 5. In the avionics compartment: - Open the circuit breakers 3WR and 4WR.在电子舱，拔出跳开关3WR 和 4WR。 T 6. At the differential pressure switch 950WR: 在压差电门950WR处：- Remove the electrical bridge. 拆除电桥- Make sure that the electrical connectors are clean and in the correct condition. 确认电接头清洁，处于正常状况。- Connect the electrical connector 950WRA.连接电接头950WRA。7. At the main distribution shutoff valve 920WR2: 在主分配关断活门920WR2处：- Disconnect the electrical connector 920WR2A.断开电接头920WR2A。 T T 8. In the avionics compartment / 在电子舱中：- Close the circuit breakers 3WR and 4WR.闭合跳开关3WR和4WR。 T 9. On the maintenance panel 285VU: 在维护面板285VU上：- Push the RESET pushbutton switch.按压RESET按钮电门At the shutoff-valve 920WR1: 在关断活门920WR1处：- The main distribution shutoff-valve 920WR1 is open.主分配关断活门920WR1打开。At the shutoff-valve 920WR2: 在关断活门920WR2处：- The main distribution shutoff-valve 920WR2 is closed.主分配关断活门920WR2关闭。On the DOOR/OXY page of the EWD of the ECAM: 在ECAM 的 EWD 的 DOOR/OXY页面：- The message REGUL LO PR is shown for the PAX OXY.显示 PAX OXY 的 REGUL LO PR 信息。NOTE: In CMC a class 1 error is generated.注 释：将生成CMC class 1 错误信息。 T 10. At the test port 7504WR1: 在测试口7504WR1：- Open the shutoff valve at the pressure source and pressurize the system to 9 +1 -1 bar (130.5 +14.5 -14.5 psi) 打开压力源关断活门，将系统增压到9 +1 -1 bar (130.5 +14.5 -14.5 psi)。 T 11. At the overhead panel 211VU: 在头顶板211VU上：- Lift the guard and push the MASK MAN ON pushbutton switch.提起保护盖并按压MASK MAN ON 按钮电门。In the cabin / 在客舱中：- If PRAM or I-PRAM is installed, the emergency announcement is heard. 如果安装了PRAM 或 I-PRAM，可听到紧急通告。In the cabin / 在客舱中：- The emergency oxygen containers open to the limit permitted by test button. . 应急氧气盒打开至测试旋钮限制的位置。NOTE: The emergency oxygen containers that are supplied by the overfloor supply line stay closed. 注 释：由地板上供气管供应的应急氧气盒保持在关闭状态。NOTE: The oxygen containers open with some delay. The delay increases with a higher system volume of the gas distribution system and decreases with a lower system volume of the gas distribution system. The ground service equipment used also has an effect on this delay.注 释：氧气盒打开会有些延迟。当气体分配系统容积较高时延迟会增加，容积较低时延迟会下降。地面勤务设备的使用也会对延迟有影响。On the DOOR/OXY page of the EWD of the ECAM: 在ECAM 的 EWD 的 DOOR/OXY 页面：- The no fault message is shown for the PAX OXY.显示PAX OXY 无故障信息。 T 12. At the connector 920WR2A of the main distribution shutoff-valve 920WR2: 在主分配管关断活门920WR2的接头920WR2A处：- Measure the voltage between the connections 920WR2A-B and 920WR2A-C with a MULTIMETER - STANDARD通过万用表测量920WR2A-B和920WR2A-C之间的电压。At the connector 920WR2A of the main distribution shutoff-valve 920WR2: 在主分配管关断活门920WR2的接头920WR2A处：- The measured voltage is approximately 28VDC.测量的电压大约是28VDC。 T 13. At the test port 7504WR1: 在测试口7504WR1：- Close the shutoff valve at the pressure source.关闭压力源处的关断活门。 T 14. At the bleed/vent valve 7503WR: 在引气/通气活门7503WR处：- Release the pressure from the system with the TOOL - MANUAL RELEASE.通过人工释放工具释放系统压力。On the DOOR/OXY page of the EWD of the ECAM: 在ECAM 的 EWD 的 DOOR/OXY 页面：- The message REGUL LO PP is shown for the PAX OXY.显示PAX OXY 的 REGUL LO PP 信息。 T 15. On the maintenance panel 285VU: 在维护面板285VU上：- Push the RESET pushbutton switch.按压 RESET 按钮电门。On the DOOR/OXY page of the EWD of the ECAM: 在 ECAM 的 EWD 的 DOOR/OXY 页面：- The message REGUL LO PR is shown for the PAX OXY.显示 PAX OXY 的 REGUL LO PR 信息。NOTE: In CMC a class 1 error is generated.注 释：将生成 CMC class 1 错误信息。 T 16. In the avionics compartment: - Open the circuit breakers 3WR and 4WR.在电子舱：拔出跳开关3WR和4WR。 T 17. At the main distribution shutoff-valve 920WR2: 在主分配关断活门920WR2上：- Make sure that the electrical connectors are clean and in the correct condition. 确认电接头清洁并处于正常状况。- Connect the electrical connector 920WR2A.连接电接头920WR2A。 T 18. At the differential pressure switch 950WR: 在压差电门 950WR 处：- Disconnect the electrical connector 950WRA. 断开电接头950WRA。- Connect an electrical bridge between the connections 950WRA-B and 950WRA-C and between the connections 950WRA-E and 950WRA-F.在 950WRA-B 与 950WRA-C 之间以及在 950WRA-E 与 950WRA-F 之间连接电桥 T 19. In the avionics compartment / 在电子舱：- Close the circuit breakers 3WR and 4WR. 闭合跳开关3WR和4WR。 T 20. On the overhead panel 211VU: 在头顶板211VU上：- Lift the guard and push the MASK MAN ON pushbutton switch.提起保护盖并按压MASK MAN ON 按钮电门。At the shutoff-valve 920WR1: 在关断活门 920WR1 处：- The main distribution shutoff-valve 920WR1 closes.主分配关断活门920WR1关闭。At the shutoff-valve 920WR2: 在关断活门 920WR2 处：- The main distribution shutoff-valve 920WR2 closes.主分配关断活门920WR2关闭。In the cabin / 在客舱中：- If PRAM or I-PRAM is installed, the emergency announcement is heard.如果安装了PRAM 或 I-PRAM，可听到紧急通告。On the DOOR/OXY page of the EWD of the ECAM: 在ECAM 的 EWD 的 DOOR/OXY 页面：- The message REGUL LO PR is shown for the PAX OXY.显示PAX OXY 的 REGUL LO PR 信息。NOTE: In CMC a class 1 error is generated.注 释：将生成 CMC class 1 错误信息。 T 21. In the cabin: - Close all of the emergency oxygen containers.在客舱中，关闭所有的应急氧气盒。 T 22. In the avionics compartment: - Open the circuit breakers 3WR and 4WR.在电子舱中，拔