WOHA33_116550_58_AT-352300-720-802

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WOHA331165_58_50DIC 培训方式116550通用类/GenericTitleFunctional Check of Automatic SystemMcd&Rev/厂家工卡&修订日期标题功能检查自动系统操作AMM352300-720-802 2014-02-01A/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BLNKAT-352300-720-802HR003005电气/ElectricMDIC01:12MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-352100-05-1MPD 352100-05-1,MRB 35.20.02/03Issue 2 Revision 3SHA730 CA730 CAAccess Panels/接近盖板Zones/区域Written/编写Approved/批准132AZ2002014-03-102014-03-17TOOLS/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198A24403000000CABLE HOLDING STRAPTO1ALL(必需/Necessary)298A35207599000HOSE - ADAPTER, ALTITUDE SWITCHTO1ALL(必需/Necessary)3995000TOOL -MANUAL RELEASETO1ALL(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)或MIL-T-815334CML08-005SEALING TAPECH1ALL(必需/Necessary)5CML08-013SEALANT, ANAEROBICCH1ALL(必需/Necessary)或MIL-S-224736CML08-001EPOXY ADHESIVECH1ALL(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:_HA33-352100-05-1 W/O:1165 AC:BLNK页码，2 / 9工卡Job card:HA33-352100-05-1TITLEFunctional Check of Automatic SystemPerfInsp标题功能检查自动系统操作工作者检查者Functional Check of Automatic System Operation 功能检查自动系统操作1. Job Set-up/开始工作 A. Aircraft Maintenance Configuration 航空器维护构型(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-801) M 接通飞机电源(参考AMM TASK 24-41-00-861-801) 。B. Get access to the avionics compartment. Then make sure that this(these) circuit T breaker(s) is (are) closed: 接近电子舱门，确认以下跳开关是闭合的：PANELDESIGNATIONFINLOCATIN 742VUPAX OXY CTL4WRC80 742VUPAX OXY CTL3WRC79 742VUPAX OXY CTL2WRC78 742VUPAX OXY CTL1WRC77 742VUQCCU901WRC67 742VUPAX OXY CTL & IND900WRC66C. Get Access/接近 (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the M forward cargo-compartment door. 在前货舱门下放置合适的接近平台。(2) Open the forward cargo-compartment door (Ref. AMM TASK 52-30-00-010-801). M 打开前货舱门(参考AMM TASK 52-30-00-010-801) 。(3) Set the CARGO COMPT LIGHT switch 6LU to the ON position. M 将货舱灯电门6LU置于ON位。(4) Remove the sidewall panels 132FX and 132UW (Ref. AMM TASK 25-52-00-000-801) M 拆下侧壁板132FX 和 132UW (参考 AMM TASK 25-52-00-000-801)。 (5) Remove the ceiling panel 262NC (Ref. AMM TASK 25-23-41-000-801) . M 拆下顶板262NC(参考 AMM TASK 25-23-41-000-801)。(6) Close the manual shutoff valves on the oxygen cylinders. M 关闭氧气瓶关断活门。(7) Put the WARNING NOTICE(S) on all the emergency oxygen cylinders to tell the persons M not to operate the manual shutoff valves.在应急氧气瓶上挂上警告牌警示他人禁止操作人工关断活门。D. Get access to the avionics compartment. Then open, safety and tag this T (these) circuit breaker(s): 接近电子舱，拔出以下跳开关，挂警告牌及安全夹：PANELDESIGNATIONFINLOCATION721VUCMC 1 SWTG4TM1U07722VUSDAC 22WV2H49742VUCMC 13TM1N72742VUSDAC 12WV1Q79E. Aircraft Maintenance Configuration 飞机维护构型(1) Disconnect the electrical connector 970WR-A from the low pressure T switch 970WR. 从低压电门970WR上断开电插头970WR-A。(2) Connect an electrical bridge between the pins A and C on the T electrical connector 970WR-A. 连接电插头970WR-A上的A和C销钉。F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): T 撤除安全夹、警告牌和闭合以下跳开关：PANELDESIGNATIONFINLOCATION721VUCMC 1 SWTG4TM1U07722VUSDAC 22WV2H49742VUCMC 13TM1N72742VUSDAC 12WV1Q79G. Connection of the Vacuum Source to the Altitude Pressure Switch 16WR 连接真空源到高度压力电门16WR。(1) Connect VACUUM EQUIPMENT 0 TO 1 BAR (15 PSI) to the altitude pressure T switch 16WR with the HOSE - ADAPTER, ALTITUDE SWITCH (98A35207599000) . 使用HOSE - ADAPTER, ALTITUDE SWITCH(98A35207599000)连接气源到备用压力电门16WR。WARNING: KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL SOURCES OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. 警 告：使碳氢化合物（比如燃油，润滑剂等等）远离氧气，否则会引起氧气爆炸。2. Procedure/步骤 (Ref. Fig. Oxygen Control and Indicating System SHEET 1)(参考. 图. Oxygen Control and Indicating System SHEET 1)A. Functional Test of the Automatic Control of the Passenger Gaseous Oxygen-System T DIC功能测试旅客氧气自动系统ACTION/操作RESULT/结果1. In the cockpit: - Do the EIS start procedure 31-60-00-860-801 . 在驾驶舱： -执行EIS启动程序31-60-00-860-801。On the DOOR/OXY page of the EWD of the ECAM: - Make sure that the message REGUL LO PR is not shown on the DOORS/OXY page of the ECAM. 在ECAM 的DOOR/OXY页面上：- 确认DOOR/OXY页面上不显示REGUL LO PR。2. At the vacuum source: - Operate the test equipment to slowly decrease the pressure to 15000 ft. (4571.91 m) . 在气源： -操作测试设备慢慢减少压力至15000 ft. (4571.91 m)。On the overhead panel 211VU: - The SYS ON indicator light comes on at 14000 +250 or-750 ft. (4267.12 +76.20m or-228.60 m) . 在头顶面板211VU：-当压力14000 +250 或-750 ft. (4267.12 +76.20m或 -228.60 m)时指示灯SYS ON亮。On the DOOR/OXY page of the ECAM- Memo PAX OXY ON comes on在ECAM的DOOR/OXY页面-备忘“PAX OXY ON”出现3. At the vacuum source: - Slowly increase the pressure to ground level. 在气源：-慢慢增加压力至海平面压力。4. On the panel 285VU: - Push the RESET pushbutton switch.在面板285VU：-按压复位电门。On the panel 285VU: - The ON indicator light on the RESET pushbutton switch comes on. 在面板285VU：复位电门上的ON指示灯亮。On the overhead panel 211VU: - The SYS ON indicator light goes off. 在头顶面板211VU：- SYS ON指示灯消失。5. On the panel 285VU: - Release the RESET pushbutton switch.在面板285VU：-释放复位电门。On the panel 285VU: - The ON indicator light on the RESET pushbutton switch goes off. 在面板285VU：-复位电门上的ON指示灯熄灭。On the DOOR/OXY page of the EWD of the ECAM: - No fault message is shown. 在ECAM 的DOOR/OXY页面上：- 确认没有故障信息。3. Close-up/结束工作 A. Disconnection of the Vacuum Source from the Altitude Pressure Switch 16WR(1) Disconnect the VACUUM EQUIPMENT 0 TO 1 BAR (15 PSI) and the T HOSE - ADAPTER, ALTITUDE SWITCH (98A35207599000) from the altitude pressure switch 16WR. 在备用压力电门16WR处断开气源及设备。B. Get access to the avionics compartment. Then open, safety and tag this(these) T circuit breaker(s): 接近电子舱门，拔出以下跳开关，挂警告牌及安全夹：PANELDESIGNATIONFINLOCATION721VUCMC 1 SWTG4TM1U07722VUSDAC 22WV2H49742VUCMC 13TM1N72742VUSDAC 12WV1Q79C. Put the Aircraft back to its Initial Configuration 恢复飞机至原始状态(1) Remove the electrical bridge from the electrical connector 970WR-A. T 断开电插头970WR-A的A和C销钉连线。(2) Make sure that the electrical connectors are clean and in the correct condition. T 确认电插头干净可用。(3) Connect the electrical connector 970WR-A. T 安装电插头970WR-A。D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): T 撤除安全夹，警告牌及闭合以下跳开关：PANELDESIGNATIONFINLOCATION721VUCMC 1 SWTG4TM1U07722VUSDAC 22WV2H49742VUCMC 13TM1N72742VUSDAC 12WV1Q79E. Put the Aircraft back to its Initial Configuration/将飞机恢复至初始构型 WARNING: KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL SOURCES OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES HYDROCARBONS. 警 告：使碳氢化合物（比如燃油，润滑剂等等）远离氧气，否则会引起氧气爆炸。(1) Release the pressure from the oxygen distribution system: T 释放氧气分配系统中的压力：WARNING: MAKE SURE THAT THE OXYGEN-DISTRIBUTION PRESSURE-RELEASE TASK IS FULLY COMPLETED. TO DO THIS, YOU MUST OPERATE THE BLEED/VENT VALVE 7503WR FOR A MINIMUM OF 10 MINUTES TO RELEASE THE RESIDUAL PRESSURE IN THE OXYGEN DISTRIBUTION SYSTEM. RESIDUAL PRESSURE IN THE OXYGEN DISTRIBUTION SYSTEM CAN PREVENT OPERATION OF THE SURGE MODE IN THE OXYGEN REGULATOR. THIS WILL KEEP THE OXYGEN MASK CONTAINERS CLOSED AND THE OXYGEN MASKS WILL NOT DEPLOY CORRECTLY IN AN EMERGENCY. 警 告：确保氧气分配系统中的压力完全释放。完成此项工作，至少操作放气/排气阀7503WR 10分钟，以便释放氧气分配系统中残留的压力。氧气分配系统中残留的压力能够阻止脱落模式的运行。在紧急情况下，使氧气面罩盒保持在关闭状态，氧气面罩不能正确展开。(a) Release the pressure through the bleed vent valve 7503WR with the TOOL-MANUAL RELEASE (995000) for 10 minutes. 使用人工释放工具(995000)打开排气阀7503WR 10 分钟。(2) If necessary, fill the emergency oxygen cylinders (Ref. AMM TASK 12-14-35-614-801) . T 按需给紧急氧气瓶充气(参考AMM TASK 12-14-35-614-801)(3) On the emergency oxygen cylinders: T 在应急氧气瓶上：(a) Open slowly but fully in one step the manual shutoff valves of all the emergency oxygen cylinders. 缓慢但要完全地一次性打开紧急氧气瓶上的人工关断活门。(b) Remove the warning notice(s). 撤除警告牌(4) Do a check of the EWD of the ECAM in the cockpit: T 在驾驶舱检查ECAM上的EWD：(a) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-801) . 执行EIS启