finished已完成c检正式工卡包

1、AT-242400-710-806 HR005013W/O:1726AC:BLNZ1 / 34页码，Airlines Limited03110-01航空Airlines MEDAirlines LimitedWO NO/工作指令号SEQ NO/序列号WOHA331726_601_621培训方式1726621通用类/GenericTitleOperational Test of the Emergency Generator Automatic ConnectionMcd&Rev/厂家工卡&修订日期标题应急发电机自动连接操作测试AMM 24-24-00-710-8062016-0

2、1-01A/C/飞机号Subtask No/工JC Rev/工卡版本号Workarea/工作区域Skill/工种Man Hour/工时BLNZAT-242400-710-806HR005013电气/ElectricAIRP00:22MP Item/MP 号Baseline/依据MP REV/ MP 版本号Station/维修站Threshold/首检Interval/重复检HA33-242400-04- 2MPD242400-04-2,CMP2 4-2-0000-002,CMR*242000-00004-1-C,MRB24.20.00/10Issue 2 Revision 5PVG730 CA

3、,4000 FH730 CA,4000 FHAccess Panels/接近盖板Zones/区域Written/编写Approved/批准NONE2102016-03-292016-03-29TOOLS/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互换及备注1D23304000ROUNDLOCK, NLGTO1ALL(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Condi

4、tions note互换及备注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互换及备注PARTS AND MATERIALIF NECESSARY/视情航材ITEM项目P/N件号DESCRIP

5、TION名称EQTP类型QTY数量APP适 用性Conditions note互换及备注IMPORTANT NOTE:In the event of any discrepes betweeninstruction and the English instruction, the English procedure should prevail.ETOPSAT-242400-710-806 HR005013W/O:1726AC:BLNZ2 / 34页码，Record Additional Work/Findings(If Applivable) Reference No. of Release

6、 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-145 and in respect to that work, The aircraft / aircraft components are consideredy for Release

7、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 * STARC

8、O 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-242400-710-806 HR005013 2016-03-293 / 34页码，工卡 Job card:HA33-242400-04-2TITLEOperational Test of the Emergency Generator Automatic ConnectionPerf

9、Insp标题应急发电机自动连接操作测试工作者检查者Operational Test of the Emergency Generator Automatic Connection应急发电机自动连接操作测试WARNING: OPEN THE PROBE HEATER CIRCUIT-BREAKERS OF AOA (1, 2 AND 3), TAT (1, 2),PITOT (1, 2 AND 3), AND STAT (1, 2 AND 3), BEFORE YOU OPEN THEPHC (1, 2 AND 3) CIRCUIT BREAKERS. IF YOU DO NOT OBEY TH

10、IS SEQUENCE:- THE PROBES WILL BECOHOT.- THIS CAN CAUSE DAMAGE TO EQUIPMENT AND INJURY TO MAINTENANCE NEL.警告：在拔出 PHC (1, 2 和 3)跳开关之前，拔出探头加温跳开关 AOA (1, 2 和 3), TAT (1, 2),PITOT (1, 2 和 3), 和 STAT (1, 2 和 3)，如果不遵循此顺序：- 探头将变得太热- 可能导致受伤和损坏。WARNING: DO NOT TOUCH THE PROBES DURING OR IMMEDIATELY AFTER THIS

11、 PROCEDURE. THE PROBES AOT AND CAN BURN YOU.警告：此项工作进行中不要触摸探头，工作结束后也不要立即触摸探头，探头很热可能导致烫伤。CAUTION: REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE TEST.注意：执行此项工作前移除探头上的保护盖。WARNING: IF, DURING ACCOMPLISHMENT OF THIS TASK, DISCREPES ARE DETECTED, WITHIN THE APPLICABLE COMPLIANCE TIME SPECI

12、FIED IN THE AIRBUS MAINTENANCE DOCUMENTATION, ACCOMPLISH THE APPLICABLE CORRECTIVE ACTIONS 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

13、 FLIGHT, ACCOMPLISH THE APPLICABLE CORRECTIVE ACTION(S), OR CONTACT AIRBUS FOR APPROVEDINSTRUCTIONS AND WITHIN THE COMPLIANCETIME SPECIFIED THEREIN, ACCOMPLISH THOSE INSTRUCTIONS ACCORDINGLY IF ANY OF THE DISCREPES DETECTED DURING ACCOMPLISHMENTOF ANY TASK, IS NOT IDENTIFIED IN THE AIRBUS MAINTENANC

14、E DOCUMENTATION, BEFORE NEXT FLIGHT, CONTACTAIRBUS 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 空客提供经批准的维护方案并在维护方案中

15、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）。* ON /适用于手册有效号为 CHH 051-103 的飞机.AT-242400-710-806 HR005013 2016-03-294 / 34页码，工卡 Job card:HA33-242400-04-2TITLEOperational Test of the Emergency Generator Automatic ConnectionPerfInsp标

16、题应急发电机自动连接操作测试工作者检查者* ON /适用于手册有效号为 CRK 005-400 的飞机Subtask 24-24-00-941-051-AA. Safety Precautions/安全措施WARNING: YOU MUST PUT SAFETY BARRIERS IN POSITION TO PREVENT ACCESS TO THE TRAVEL RANGES OF ALL THE LANDING GEAR DOORS.THE AIRCRAFT IS IN SIMULATED FLIGHT CONDITION AND THE DOORS CAN OPEN AUTOMATIC

17、ALLY.警告：必须将安全护栏放置到位，接近所有的起落架舱门活动区域。飞机处于模拟飞行状态并且所有的可以自动打开。(1) Install the safety devices on the Landing Gears (L/G) (Ref. AMM TASK 32-00-00-481-801) .在起落架上安装安全装置(参考 AMM TASK 32-00-00-481-801)。(2) Put the SAFETY BARRIER(S) in position to prevent access to the area where the landing gear doors operate.

18、将安全护栏（网）放置到位，接近所有的起落架舱门操纵区域。(3) On the right-center instrument-panel 312VU:在右侧仪表板 312VU：- Put a WARNING NOTICE(S) in position to tells not to operate the landing gear.放置警告牌警告不要操作起落架。- Make sure that the landing gear lever is in the DOWN position.确保起落架手柄放置在 DOWN 位。(4) Make sure that the ground door o

19、pening handles of the L/G doors agree with the position of the L/G doors.确保起落架地面门手柄位置和起落架门位置一致。CAUTION: YOU MUSTTHE CIRCUIT BREAKERS OPENED FOR AIRCRAFT FLIGHT CONFIGURATION WHEN THE MAINTENANCE WORK IS COMPLETED. DAMAGE TO THE AIRCRAFT CAN OCCUR IF THEY STAY OPEN.注意：当维修工作完成以后必须关闭所有为飞机飞行状态而开的电路开关。否则

20、有可能对飞机造成损坏。(5) Put a WARNING NOTICE in position to tells not to enter the area.放置警告牌提醒人们不要进入该区域。* ON /适用于手册有效号为 CHH 001-050, 104-150 的飞机* ON /适用于手册有效号为 CRK 001-004 的飞机Subtask 24-24-00-860-060-BWARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN

21、 CAUSE INJURY TOS AND/OR DAMAGE.警告：确认飞控行程范围内无，否则会引起受伤或损坏。CAUTION: DO NOT OPERATE THE FLAPS AND SLATS WHEN ONE OR MORE "LEAK MEASUREMENT VALVES" PUSHBUTTON SWITCHES ARE IN THE RELEASED POSITION ("OFF" LEGEND ON).OPERATION OF THE FLAPS AND SLATS IN THIS CONFIGURATION CAN CAUSE JAMO

22、F THE MECHANICAL TRANSMISSION.注意：当一个或多个“LEAK MEASUREMENT VALVES”电门在位时（OFF 字） TAT-242400-710-806 HR005013 2016-03-295 / 34页码，工卡 Job card:HA33-242400-04-2TITLEOperational Test of the Emergency Generator Automatic ConnectionPerfInsp标题应急发电机自动连接操作测试工作者检查者不要操作襟翼和缝翼，否则会引起机械传输机构干扰。B. Aircraft Maintenance Co

23、nfiguration飞机维护构型NOTE: Do not do this test when you refuel the aircraft. This test will stop the refueling.注 释：加油时不要做此测试，此测试会停止加油。(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-801) .连接飞机电源(参考 AMM TASK 24-41-00-861-801)。(2) Do the EIS start procedure (EWD DU, SD DU only)(R

24、ef. AMM TASK 31-60-00-860-801) .启动 EIS (仅 EWD DU, SD DU) 程序(参考 AMM TASK 31-60-00-860-801)。(3) On the maintenance panel 285VU:- push the CMC1 pushbutton switch (the OFF legend comes on)在 285VU 面板上：- 按压 CMC1 电门（OFF 字）。(4) Pressurize the Green hydraulic system (Ref. AMM TASK 29-00-00-863-801) .增压绿系统(参考

25、 AMM TASK 29-00-00-863-801)。(5) On the FLAPS control panel 114VU, make sure that the flap and slat control lever is in 0 position.在 FLAPS面板 114VU 面板上，确认襟翼和缝翼手柄在 0 位。(6) On the HYD section of the maintenance panel 285VU, release the LEAK MEASUREMENT VALVE/G pushbutton switch (the OFF legend comes on)

26、.在 285VU 面板 HYD 部分，LEAK MEASUREMENT VALVE/G 电门（OFF 字）。(7) On the ENG-START control panel 145VU, make sure that the ENG MODE selector switch is set to NORM.在 ENG-START面板 145VU 上，确认 ENG MODE 选择电门在 NORM 位。(8) On the ENG-MASTER control panel 125VU, make sure that the ENG MASTER 1, (2) switch is in the O

27、FF position.在 ENG-MASTER面板 125VU 上，确认 ENG MASTER 1, (2)电门在 OFF 位。* ON /适用于手册有效号为 CHH 051-103 的飞机* ON /适用于手册有效号为 CRK 005-400 的飞机Subtask 24-24-00-860-060-EWARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TOS AND/OR DAMAGE.警告：确认飞控行

28、程范围内无，否则会引起受伤或损坏。CAUTION: DO NOT OPERATE THE FLAPS AND SLATS WHEN ONE OR MORE "LEAK MEASUREMENT VALVES" PUSHBUTTON SWITCHES ARE IN THE RELEASED POSITION ("OFF" LEGEND ON).OPERATION OF THE FLAPS AND SLATS IN THIS CONFIGURATION CAN CAUSE JAMOF THE MECHANICAL TRANSMISSION.注意：当一个或多个“

29、LEAK MEASUREMENT VALVES”电门在位时（OFF 字）不要操作襟翼和缝翼，否则会引起机械传输机构干扰。B. Aircraft Maintenance Configuration/飞机维修构型NOTE: Do not do this test when you refuel the aircraft.This test will stop the refueling. T TAT-242400-710-806 HR005013 2016-03-296 / 34页码，工卡 Job card:HA33-242400-04-2TITLEOperational Test of the

30、Emergency Generator Automatic ConnectionPerfInsp标题应急发电机自动连接操作测试工作者检查者注 释：加油时不要做此测试，此测试会停止加油。(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-801) .连接飞机电源(参考 AMM TASK 24-41-00-861-801)。(2) Do the EIS start procedure (EWD DU, SD DU only) (Ref. AMM TASK 31-60-00-860-801) .启动 EI

31、S (仅 EWD DU, SD DU) 程序(参考 AMM TASK 31-60-00-860-801)。(3) Pressurize the Green hydraulic system (Ref. AMM TASK 29-00-00-863-801) .增压绿系统(参考 AMM TASK 29-00-00-863-801)。(4) On the FLAPS control panel 114VU, make sure that the flap and slat control lever is in 0 position.在 FLAPS面板 114VU 面板上，确认襟翼和缝翼手柄在 0

32、位。(5) On the HYD section of the maintenance panel 285VU, release theLEAK MEASUREMENT VALVE/G pushbutton switch (the OFF legend comes on).在 285VU 面板 HYD 部分，LEAK MEASUREMENT VALVE/G 电门（OFF 字）。(6) On the ENG-START control panel 145VU, make sure that the ENG MODE selector switch is set to NORM.在 ENG-STA

33、RT面板 145VU 上，确认 ENG MODE 选择电门在 NORM 位。(7) On the ENG-START control panel 125VU, make sure that the ENG MASTER 1, (2) switch is in the OFF position.在 ENG-START面板 125VU 上，确认 ENG MASTER 1, (2)电门在 OFF 位。* ON A/C ALL /适用于所有的飞机C. Get Access/接近(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position a

34、t the access door 811.在接近门 811 下放置接近工作梯 ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE。(2) Open the access door 811 .打开接近门 811。(3) Open the protective door of the AC/DC emergency power center 740VU.打开 AC/DC 应急电源中心 740VU 保护门。D. Make sure that this(these) circuit breaker(s) is(are)d:确认如下跳开关闭合：PANELDESIGNATION

35、FINLOCATION721VU1XP VOLT REF/TEST29XED04721VUL/G SAFETY VLV3GAS12722VU2XP VOLT REF/TEST30XED49722VUFADEC B ENG 113KS1D44722VUFADEC B ENG 213KS2K49722VULGCIU 22GAU38742VU401XP CTL17XHA77742VUHP FUEL SOV ENG 11KC1C68742VUHP FUEL SOV ENG 21KC2D70742VUAC EMER DET RLY25XEE77742VUCSM/G AUTO START17XEJ7874

36、2VULGCIU 11GAL63742VU801/805PP SHED CTL4PHN64 T TAT-242400-710-806 HR005013 2016-03-297 / 34页码，工卡 Job card:HA33-242400-04-2TITLEOperational Test of the Emergency Generator Automatic ConnectionPerfInsp标题应急发电机自动连接操作测试工作者检查者742VU801/805PP CTL3PHN63O T742VUCSM/G OFF CTL24XEN62742VUCSM/G MAN START22XEN61

37、742VUFADEC A ENG 212KS2Q74742VUFADEC A ENG 112KS1Q73WARNING: OPEN THE PROBE HEATER CIRCUIT-BREAKERS OF AOA (1, 2 AND 3), TAT (1, 2),PITOT (1, 2 AND 3), AND STAT (1, 2 AND 3), BEFORE YOU OPEN THEPHC (1, 2 AND 3) CIRCUIT BREAKERS. IF YOU DO NOT OBEY THIS SEQUENCE:- THE PROBES WILL BECOHOT.- THIS CAN C

38、AUSE INJURY TO MAINTENANCENEL AND/OR DAMAGE T EQUIPMENT.警告：在拔出 PHC (1, 2 和 3)跳开关之前，拔出探头加温跳开关 AOA (1, 2 和 3), TAT (1, 2),PITOT (1, 2 和 3), 和 STAT (1, 2 和 3)。如果不遵循此顺序：- 探头将变得过热。- 造成和的损伤。CAUTION: IN THE LIST OF CIRCUIT BREAKERS THAT FOLLOWS, MAKE SURE THAT YOU OPEN THESE CIRCUIT BREAKERS LAST:2DA1, 2DA

39、2, 2DA3, 5DG1, 5DG2.THIS WILL PREVENT UNWANTED OPERATION OF THE PROBE AND WINDOW HEATING SYSTEMS.注意：在下面的跳开关中，必须最后拔出跳开关 2DA1, 2DA2, 2DA3, 5DG1, 5DG2。这样可以避免不必要的探头和窗户加热系统操作。E. Open, safety and tag these circuit breakers in this sequence:按照以下顺序拔出如下跳开关，夹上安全夹并挂警告牌：PANELDESIGNATIONFINLOCATION722VUICE AOA 2

40、1DA2F48742VUICE PITOT1OR33DAQ72721VUICE PITOT 34DA1L07722VUICE PITOT 24DA2F43721VUICE STAT 111DA1W09722VUICE STAT 211DA2X41721VUICE STAT 311DA3W10721VUICE TAT 112DA1B06722VUICE TAT 212DA2E43742VUICE AOA 1 OR 331DA1Q68721VUICE AOA 331DA3C05721VUICE DET 12DD1B07722VUICE DET 22DD2F47740VUICE WSHLD L1DG

41、1T74715VUICE WSHLD R1DG2R57721VUICE WINDOWS L4DG1D03722VUICE WINDOWS R4DG2D43AT-242400-710-806 HR005013 2016-03-298 / 34页码，工卡 Job card:HA33-242400-04-2TITLEOperational Test of the Emergency Generator Automatic ConnectionPerfInsp标题应急发电机自动连接操作测试工作者检查者742VUCPC 11HLA66 T T722VUCPC 22HLU44721VUTURBO FAN

42、CTL3HRT06742VURAT MAN ON2JRK74742VUHYD RAT EXT SOL 25JRD76742VUAPU START CTL1KAC72742VU28VDC ESS BUS5QCF64742VU28VDC ESS BUS6QCF65742VUHF 12RE1J63721VURA 12SA1L14722VURA 22SA2E46742VUATC 13SH1Q64722VUATC 23SH2E47* ON /适用于 CHH 所有的飞机* ON /适用于手册有效号为 CRK 101-400 的飞机721VUTCAS4SGB05* ON /适用于手册有效号为 CRK 101

43、-400 的飞机721VUT2CAS104SGB12* ON A/C ALL /适用于所有的飞机721VULA/DAR/QAR 28VDC9TUU11* ON /适用于手册有效号为 CHH 001-050, 104-150 的飞机* ON /适用于手册有效号为 CRK 001-100 的飞机742VUSDCU CHAN 111WHL75722VUSDCU CHAN 212WHT38* ON A/C ALL /适用于所有的飞机721VUPHC 12DA1P12722VUPHC 22DA2X40721VUPHC 32DA3N07742VUWHC 15DG1G64722VUWHC 25DG2X39F

44、. Table of the circuit breakers used in this procedure:在这一步骤中用到的电路开关：2. Procedure /步骤* ON /适用于手册有效号为 CHH 001-050, 104-150 的飞机Subtask 24-24-00-710-057-HA. Operational Test of the CSM/G Automatic Connection CSM/G 自动连接操作测试ACTION/操作RESULT/结果NOTE: Ignore all the other warnings, ECAM status, amber indicat

45、ions that can come into view andPANELDESIGNATIONFINLOCATION721VU1XP VOLT REF/TEST29XED04722VU2XP VOLT REF/TEST30XED49AT-242400-710-806 HR005013 2016-03-299 / 34页码，工卡 Job card:HA33-242400-04-2TITLEOperational Test of the Emergency Generator Automatic ConnectionPerfInsp标题应急发电机自动连接操作测试工作者检查者are not giv

46、en in this test procedure.注 释：忽略此没有列出的所有其他警告，ECAM 状态，琥珀色。 T1. On the center pedestal, on the ECAM control panel:-Push the HYD key在中心基座，ECAM面板上：-按压HYD按键。On the SD, on the HYD page:-Make sure that the normal configuration comes into view.-Make sure that the actual system pressure indication below the

47、GREEN indication is of 3000-200 psi or +200 psi (206.84 -13.79 bar or +13.79 bar).NOTE: A minimum hydraulic pressure is necessary for the CSM/G to start and operate correctly在SD上的HYD页面：-确认正常的页面状态出现。- 确认 GREEN 指示下面的真实系统指示在3000±200 psi（206.84±13.79 bar）。注 释：对于CSM/G必须有最低，以正常启动和操作。2.On the ECA

48、M control panel:- push the EL/AC key.在 ECAM面板：- 按压 EL/AC 键。On the SD, ELEC AC page:- the normal configuration comes into view.在 SD，ELEC AC 页面：- 显示正常构型。3.On the left overhead control-panel 211VU, EMER ELEC section-push the LAND RECOVERY pushbutton switch.在左侧头顶板 211VU 上 EMER ELEC部分：- 按压 LAND RECOVERY

49、电门。On the left overhead control-panel 211VU- the ON legend of the LAND RECOVERY pushbutton switch comes on.On the SD, ELEC AC page :- the green LAND RCVRY indication comes into view on the left of the AC ESS busbar. 在左侧头顶 板 211VU 面板：- LAND RECOVERY 电门上 ON 字。在 SD，ELEC AC 页面：- 绿色 LAND RCVRY显示在 AC ESS

50、汇流条左侧。4.Get access to the SYSTEM REPORT/ TEST L/G:EXT/RETR page(Ref. AMM TASK 45-10-00-860-821) . 获取 SYSTEM REPORT/TEST L/G:EXT/RETR 页面(参考 AMM TASK 45-10-00-860-821)。NOTE: MCDU3 and MCDU1 are not d during the test and you cannotuse them.注 释：在此测试中 MCDU3 和 MCDU1 不提供，不要使用他们。On the SD:- There is no chan

51、ge.在 SD 上：- 无变化。AT-242400-710-806 HR005013 2016-03-2910 / 34页码，工卡 Job card:HA33-242400-04-2TITLEOperational Test of the Emergency Generator Automatic ConnectionPerfInsp标题应急发电机自动连接操作测试工作者检查者5.On MCDU2, on LGCIU1 page, simulate the nose landing gear in flight:- Push the line key adjacent to FLIGHT and

52、 UPLOCKED indications(Ref. AMM TASK 32-69-00-860-801) .在 MCDU2 的 LGCIU1 页面，模拟在飞状态下的前起落架：-按下FLIGHT 和 UPLOCKED 的行健(参考 AMM TASK 32-69-00-860-801)。On the SD:- There is no change.在 SD 上：- 无变化。 T6.On circuit breaker panel 721VU:- Open circuit breaker 29XE.在 721VU 跳开关面板：- 拔出跳开关 29XE。On the SD:- There is no change.在 SD 上：- 无变化。NOTE: If the CSM/G