WOHA33_2294136_37_AT-292400-710-804

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WOHA332294_37_136DIC 培训方式2294136通用类/GenericTitleOperational Check of RAT Automatic Deployment (with ENGINE OPERATION SIMULATOR Tool) Detailed Visual Inspection of the Ram Air Turbine once extendedMcd&Rev/厂家工卡&修订日期标题操作检查冲压涡轮的自动放出（使用发动机操作模拟器工具）并详细目视检查冲压涡轮AMM 29-24-00-710-804-012016-10-01A/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BLNRAT-292400-710-804HR004007机身/AirframeMINP08:00MP Item/MP号Baseline/依据MP REV/ MP版本号Station/维修站Threshold/首检Interval/重复检HA33-292400-01-1MPD292400-01-1,MRB29.20.00/03,MRB29.20.00/05Issue 2 Revision 5HKG730 CA730 CAAccess Panels/接近盖板Zones/区域Written/编写Approved/批准633HB2102016-12-302017-01-04TOOLS/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198F29103004000ENGINE OPERATION SIMULATORTO1ALL(必需/Necessary)2D23304000PIN-GROUNDLOCK, NLGTO1ALL(必需/Necessary)3CML19-011SCOTCH BRITE PADSTO1ALL(必需/Necessary)或百洁布498F29103001001TEST SET - HYDRAULIC FLUID LEVELTO1ALL(必需/Necessary)5TT-I-735异丙醇-Non Aqueous Cleaner-Isopropyl AlcoholTO1ALL(必需/Necessary)CML11-010TOOLS 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198D27803000000LOCKING TOOL - FLAP/SLAT CONTROL LEVERTO1ALL(视情/As Necessary)2CML19-003CLEANING ABSORTO1ALL(视情/As Necessary)398F29208217000PIN SAFETY,RATTO1ALL(视情/As Necessary)4PGRAT1-1TEST EQUIPMENT - RAM AIR TURBINETO1ALL(视情/As Necessary)AGE10600C; HRT01598F29208412000DEVICE-R/I RATTO1ALL(视情/As Necessary)698F29208544000HOSE SUPPORT - GMT, RATTO1ALL(视情/As Necessary)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1AMS5687LOCKWIREAS1ALL(视情/As Necessary)CML19-0102MS24665-300PIN COTTERAS3ALL(视情/As Necessary)3M83248-1-908(7AB2)PACKINGAS2ALL(视情/As Necessary)4MIL-T-81533solventCH1ALL(视情/As Necessary)CML11-0045MS24665-155PINAS1ALL(视情/As Necessary)6MS24665-88PINAS2ALL(视情/As Necessary)7MIL-S-8802ADHESIVECH1ALL(视情/As Necessary)CML09-0018MIL-C-16173GREASECH1ALL(视情/As Necessary)CML05-005D9MIL-PRF-23827GREASECH1ALL(视情/As Necessary)CML04-00410VV-P-236VASELINECH1ALL(视情/As Necessary)CML04-01211NYCOTE7-11primer(18.33C-26.67C)CH1ALL(视情/As Necessary)CML07-00112CML03-003GREASECH1ALL(视情/As Necessary)13CML16-006SILICONE(base:F580-2080+hard:F275-160+thin:F850-1241)CH1ALL(视情/As Necessary)14CML05-002Non Hardening Jointing Putty - Medium Temp. AreaCH1ALL(视情/As Necessary)15CML06-011SOLID FILM LUBRICANTCH1ALL(视情/As Necessary)CMl06-002161702934ARAT-RAM AIR TURBINE（禁订禁用）AS1ALL(视情/As Necessary)17CML09-014CORROSION INHIBITIVE COATINGCH1ALL(视情/As Necessary)18M83248-1-021packingAS2ALL(视情/As Necessary)19CML04-002GRAPHITED MINERAL GREASECH1ALL(视情/As Necessary)20766542AGEARBOXAS1ALL(视情/As Necessary)21732040WASHERAS1ALL(视情/As Necessary)22LN29557KA16-75SHIM-LAMINATEDAS1ALL(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,D.101131* HKE Approval No: AI /218/1215, JMM 133 * Other: * Signature:_ Authorization No.:_ Date:_AT-292400-710-804 HR004007 W/O:2294 AC:BLNR页码，3 / 57工卡Job card:HA33-292400-01-1TITLEOperational Check of RAT Automatic Deployment (with ENGINE OPERATION SIMULATOR Tool) Detailed Visual Inspection of the Ram Air Turbine once extendedPerfInsp标题操作检查冲压涡轮的自动放出（使用发动机操作模拟器工具）并详细目视检查冲压涡轮工作者检查者Operational Check of RAT Automatic Deployment (with ENGINE OPERATION SIMULATOR Tool) Detailed Visual Inspection of the Ram Air Turbine once extended操作检查冲压涡轮的自动放出（使用发动机操作模拟器工具）并详细目视检查冲压涡轮WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR:- THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 警 告：确认执行工作前，在以下位置已放置安全装置和警告牌： - 飞行控制 - 飞行控制舵面 - 起落架及其随动门 - 运动部件 部件运动会造成人员伤亡。WARNING: DO NOT WEAR A HEADSET OR TOUCH CABLES/LINES CONNECTED TO THE AIRCRAFT WHEN THERE IS A RISK OF LIGHTNING. LIGHTNING IS DANGEROUS.警 告：当可能发生闪电时，切勿戴耳机或碰触与飞机相连的电缆/电线。闪电是危险的。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 THE PHC (1, 2 AND 3) CIRCUIT BREAKERS. IF YOU DO NOT OBEY THIS SEQUENCE: - THE PROBES WILL BECOME TOO HOT. - THIS CAN CAUSE DAMAGE TO EQUIPMENT AND INJURY TO MAINTENANCE PERSONNEL. 警 告：先拔出AOA (1, 2 和 3), TAT (1, 2), PITOT (1, 2 和 3), 和 STAT (1, 2 和 3)的皮托管加热跳开关，然后再拔出PHC (1, 2 和 3)跳开关。如果不按照顺序操作：- 皮托管会变得很热。- 可能导致人员受伤和设备损坏。WARNING: DO NOT TOUCH THE PROBES DURING OR IMMEDIATELY AFTER THIS PROCEDURE. THE PROBES ARE HOT AND CAN BURN YOU. 警 告：工作中或者工作结束不要立即触碰皮托管。过热的皮托管会灼伤皮肤。WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURERS INSTRUCTIONS AND YOUR LOCAL REGULATIONS.警 告：使用化工品是要小心。遵守材料厂家说明和当地规章。CAUTION: REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE TEST.注 意：执行测试之前，将皮托管套取下。CAUTION: MAKE SURE THAT YOU DO A RESET OF CIRCUIT BREAKER 5JR. IF YOU DO NOT DO THE RESET, THERE WILL BE NO GREEN HYDRAULIC PRESSURE AT ENGINE START OR TAKEOFF. 注 意：确认已重置断路开关5JR。如果不进行重置，在发动机启动或关车时将不会有绿系统液压压力。1. Job Set-up /工作准备 A. Safety Precautions /安全措施 M (1) Put the safety barriers in position. /将安全护栏放置在位。(2) Put the WARNING NOTICE(S) in position to tell persons that the RAT is in operation. 设置警告标牌，提示人员RAT正在被操作。B. Get Access /打开接近 M (1) Open the MLG doors (Ref. AMM TASK 32-12-00-010-801) . 打开MLG门(参考 AMM TASK 32-12-00-010-801)。(2) Put the access platform in position below the RAT. 在RAT下部将接近平台放置在位。(3) Open the access panel 633HB . /打开接近面板633HB。C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): T 接近电子舱，拔出以下跳开关、设置安全夹并挂警告标牌：PANELDESIGNATIONFINLOCATION 715VUANTI ICE WSHLD R1DG2R57721VUICE DET 12DD1B07 721VUANTI ICE TAT 112DA1B06721VUANTI ICE AOA 3 31DA3C05 721VUANTI ICE WIDOWS L4DG1D03 721VUANTI ICE PITOT 34DA1L07 721VUANTI ICE STAT 311DA3W10 721VUANTI ICE STAT 111DA1W09 722VUANTI ICE WINDOWS R4DG2D43 722VUANTI ICE TAT 212DA2E43 722VUANTI ICE AOA 21DA2F48722VUICE DET 2 2DD2F47 722VUANTI ICE PITOT 24DA2F43 722VUANTI ICE STAT 211DA2X41 740VUANTI ICE WSHLD L1DG1T74742VUESS ANTI ICE PITOT 316DAH69742VUESS ANTI ICE AOA315DAH68 742VUANTI ICE PITOT1OR33DAQ72742VUANTI ICE AOA 1 OR 331DA1Q68CAUTION: IN THE LIST OF CIRCUIT BREAKERS THAT FOLLOWS, MAKE SURE THAT YOU OPEN THESE CIRCUIT BREAKERS LAST: 2DA1, 2DA2, 2DA3, 5DG1, 5DG2. THIS WILL PREVENT UNWANTED OPERATION OF THE PROBE AND WINDOW HEATING SYSTEMS.注 意：确保以下跳开关打开：2DA1, 2DA2, 2DA3, 5DG1, 5DG2.这样可以防止探测器和窗加热系统的不正确动作 721VUPHC 32DA3N07 721VUPHC 12DA1P12 722VUPHC 22DA2X40 722VUWHC 25DG2X39 742VUWHC 15DG1G64D. Aircraft Maintenance Configuration / 飞机维护构型 T (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-801) . 接通飞机电源(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) . 执行EIS启动程序(仅EWD DU, SD DU) (参考 AMM TASK 31-60-00-860-801)。(3) Make sure that the engines 1 and 2 are not in operation. 确认1号和2号发动机未工作。(4) Make sure that the Green hydraulic system is depressurized (Ref. AMM TASK 29-00-00-864-804) . 确认绿液压系统已释压(参考 AMM TASK 29-00-00-864-804)。 (5) On the HYD panel 245VU, release the YELLOW/ELEC PUMP (4JJ) and GREEN/ELEC PUMP (4JV) pushbutton switches (the OFF legends come on). 在HYD面板245VU上，松开YELLOW/ELEC PUMP (4JJ)和GREEN/ELEC PUMP (4JV)按钮电门（OFF灯亮）。(6) For the Procedure 1, remove the PIN - SAFETY, RAT (98F29208457000) from the RAT if installed (Ref. AMM TASK 29-24-00-081-801) . 对于方法1，从RAT上拆除RAT安全销(98F29208457000) (如果安装)(参考 AMM TASK 29-24-00-081-801)。 (7) For the Procedure 2, /对于方法2 (a) Install the PIN - SAFETY, RAT (98F29208457000)at the RAT (Ref. AMM TASK 29-24-00-481-801) . 在RAT上，安装RAT安全销(98F29208457000)(参考AMM TASK 29-24-00-481-801)。 (b) Disconnect the electrical connector 11JR-B from the RAT. 从RAT脱开电插头11JR-B。E. On the ECAM control panel, push the C/B key (on the SD the C/B page comes into T view). Make sure that the SD does not show this(these) circuit breaker(s) : 在ECAM控制面板上，按压C/B键（在SD上，出现C/B页面）。确认SD未显示以下跳开关：PANELDESIGNATIONFINLOCATION 721VUHSMU B + PART G6JGU10 722VUHSM Y + PART G7JGX46 742VUHP FUEL SOV ENG 11KC1C68 742VURAT STOW CTL1JRD77 742VUHYD RAT EXT SOL 25JRD76 742VUHP UEL SOV ENG 21KC2D70 742VUAC EMER DET RLY25XEE77 742VUCSM/G AUTO START17XEJ78 742VURAT MAN ON2JRK74 742VUCSM/G OFF CTL24XEN62 742VUCSM/G MAN START22XEN61WARNING: DO NOT TOUCH THE PROBES DURING OR IMMEDIATELY AFTER THIS PROCEDURE. THE PROBES ARE HOT AND CAN BURN YOU. 警 告：工作中或者工作结束不要立即触碰皮托管。过热的皮托管会灼伤皮肤。CAUTION: REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE TEST. 注 意：执行测试之前，将皮托管套取下。2. Procedure /步骤 (Ref. Fig. Engine Operation Simulator - Engine 2 SHEET 1) (Ref. Fig. Engine Operation Simulator - Engine 1 SHEET 1)(参考图Fig. Engine Operation Simulator - Engine 2 SHEET 1) (参考图Fig. Engine Operation Simulator - Engine 1 SHEET 1)WARNING: MAKE SURE THAT THE RAT TRAVEL RANGE IS CLEAR BEFORE YOU EXTEND/RETRACT THE RAT. MOVEMENT OF THE RAT CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE. 警 告：在收放RAT前，确认RAT行程内无障碍。RAT做动会导致人员受伤和设备损伤。*ON A/C CRK 101-300，302-350/ 适用于CRK手册有效号为 101-300，302-350的飞机*ON A/C HKC ALL/适用于HKC手册所有飞机*ON A/C CHH ALL/适用于CHH手册所有飞机Subtask29-24-00-710-064-EA. Operational Test of the RAT Automatic Deployment Function after a Total Engine Flameout T DIC 操作测试RAT在全部发动机熄火情况下的自动放出功能(Ref. Fig. Engine Operation Simulator - Engine 2 SHEET 1)(参考图Fig. Engine Operation Simulator - Engine 2 SHEET 1)NOTE: The two procedures that follow permit you to do a check of the RAT automatic deployment function without RAT extension.- Procedure 1:The RAT extends by the first automatic deployment test. For the subsequent deployment tests you can hear a click when the deployment solenoid operates. - Procedure 2: For the first and the second deployment test, the RAT stays retracted and you measure the voltage at the electrical connector 11JR-B. For the third deployment test, you connect the electrical connector 11JR-Bto the RAT and the RAT extends during the test. 注 释：无需RAT放出，可以运用2种方法检查RAT自动放出功能。-方法1，RAT在首次自动放出测试时放出。对于后续放出测试，当放出电磁活门工作时，会听到滴答声。-方法2，RAT在前两次放出测试时保持收上，并测量电插头11JR-B的电压。进行第三次放出测试时，将电插头11JR-B连接到RAT，在测试中，RAT会放出。NOTE: Use one Multipurpose Control & Display Unit (MCDU) for the ADR RAM AIR TURBINE TEST (referred as Air Data Reference (ADR) MCDU) and a second MCDU for the LGCIU1/landing gear simulation (referred as Landing Gear Control and Interface Unit (LGCIU) MCDU). 注 释：一个MCDU用于ADR RAM AIR TURBINE TEST（简称(ADR) MCDU），第二个用于起落架模拟/ LGCIU(简称(LGCIU) MCDU)。ACTION/操作RESULT/结果1. On the ELEC panel 235VU:-push and release the BAT1, BAT2 and APU BAT P/BSWs.在ELEC面板235VU上：-按压并松开BAT1, BAT2和APU BAT按钮电门。On the ELEC panel 235VU:-the OFF legends of the BAT1, BAT2 and APU BAT P/BSWs come on.在ELEC面板235VU上：-BAT1, BAT2和APU BAT按钮电门OFF灯点亮。2. On the ELEC panel 235VU:-push and release the EXT A P/BSW在ELEC面板235VU上：-按压并松开EXT A按钮电门。On the ELEC panel 235VU, on the EXT A P/BSW-the ON legend goes off,-the AVAIL legend comes on.在ELEC面板235VU上，EXT A按钮电门：-ON灯熄灭- AVAIL灯点亮。3. On the SIMULATOR-ENGINE OPERATION (98F29103004000) :-Make sure that the switches are in the DE-ENERGIZED position.在发动机操作模拟器(98F29103004000)上：-确认电门都处于DE-ENERGIZED位。4. On the electronic rack 800VU:-Get access to the plugs on the R lateral connector plate 802VU.在电子架800VU上：-接近R水平插板802VU上的插头。A. To simulate the ENG 2 in operation, do as follows:-On the connector plate 802VU, disconnect the plug 2506VC-A and then connect the connectors of the SIMULATOR-ENGINE OPERATION (98F29103004000) identified 2506VC and 2506VC-A,-connect the alligator clip identified ENG 2 to the ground.A. 模拟2号发动机运转，执行以下步骤：-在插板802VU上，脱开插头2506VC-A并连接发动机操作模拟器(98F29103004000)商定义为2506VC和2506VC-A的电插头-定义为2号发动机的鳄鱼夹接地。5. On the ELEC panel 235VU:-Push the EXT A P/BSW.在ELEC面板235VU上：-按压EXT A按钮电门。On the ELEC panel 235VU, on the EXT A P/BSW:-The AVAIL legend goes off,-The ON legend comes on.在ELEC面板235VU上，EXT A按钮电门：-AVAIL灯熄灭-ON灯点亮。6. On the ELEC panel 235VU:-Push the BAT1, BAT2 and APU BAT P/BSWs.在ELEC面板235VU上：-按压BAT1, BAT2和APU BAT按钮电门。On the ELEC panel 235VU:-the OFF legends of the BAT1, BAT2 and APU BAT P/BSW go off.在ELEC面板235VU上：-BAT1, BAT2和APU BAT按钮电门OFF灯熄灭。7. On the SIMULATOR-ENGINE OPERATION (98F29103004000) :-Set the ENGINE 2 switches (24KS2-35KS2) to the ENERGIZED position.在发动机操作模拟器(98F29103004000)上：- 将ENGINE 2 电门(24KS2-35KS2) 设置到ENERGIZED位。On the 800VU:-You hear a closing click when the relays are energized.在800VU上：-当继电器通电时，会听到结束的喀哒声。On the HYD panel 245VU:-The FAULT legends of the GREEN/ENG 2 and YELLOW/ENG 2 P/BSWs come on.在HYD面板245VU上：- GREEN/ENG 2 和 YELLOW/ENG 2按钮电门上的FAULT灯点亮。8. On the ECAM control panel:-push the HYD key.在ECAM控制面板上：-按压HYD键。On the SD:-the HYD page comes into view,-the RAT triangle symbol is white.在SD上：-出现HYD页面- RAT三角标志为白色。9. On the (ADR) MCDU, start the simulation of the A/C speed with the ADR 1 RAM AIR TURBINE TEST (Ref. TASK 34-13-00-710-804).在(ADR) MCDU上，使用ADR 1 RAM AIR TURBINE TEST启动A/C速度模拟（参考34-13-00-710-804）。NOTE: You must not use the MCDU MENU key to stop the ADR RAM AIR TURBINE TEST.注释： 禁止使用MCDU MENU键终止ADR RAM AIR TURBINE TEST。NOTE: If the ADR RAM AIR TURBINE TEST does not complete: - Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-803) , wait for a minimum of 20s and then do the ADIRU start procedure (Ref. AMM TASK 34-10-00-860-801) . 注释：如果ADR 冲压空气涡轮测试未完成：-执行ADIRS停止程序(参考 AMM TASK 34-10-00-860-803)，等待至少20s然后执行ADIRU启动程序(参考 AMM TASK 34-10-00-860-801).10. On the (LGCIU) MCDU, start the simulation of the flight condition with the LGCIU1/landing gear simulation menu (Ref. TASK 32-69-00-860-801) Use the NOSE+LH+RH menu and then push the adjacent FLIGHT and UPLOCKED keys.在(LGCIU) MCDU上，使用LGCIU1/起落架模拟菜单启动飞行状态模拟（参考32-69-00-860-801）。使用NOSE+LH+RH菜单，再按压FLIGHT和UPLOCKED对应行选键。On HYD panel 245VU:- The FAULT legends of the GREEN/ENG 1 and BLUE/ENG 1 P/BSWs come on.在245VU面板液压部分- GREEN/ENG 1 和 BLUE/ENG 1 P/BSWs上的FAULT灯点亮11. Make sure that on the panel 742VU, the subsequent circuit breakers are closed:确认面板742VU上，以下跳开关已关闭：-HYD RAT EXT SOL 2 (5JR location D76),-CSM/G MAN START (22XE location N61).12. On the SIMULATOR-ENGINE OPERATION (98F29103004000) :-Set the ENGINE 2 switches (24KS2-35KS2) to the DE-ENERGIZED position to simulate a total engine shutdown operation.在发动机操作模拟器(98F29103004000)上：- 将ENGINE 2 电门(24KS2-35KS2) 设置到DE-ENERGIZED位以模拟整个发动机关断操作。For the Procedure 1:对于方法1：At the RAT:-The RAT extends.在RAT处：-RAT放出。On the SD:-The RAT triangle symbol changes from white to amber.在SD上：-RAT三角标志由白色变琥珀色。On the EWD:-The RAT FAULT warning comes on.在EWD上：-RAT FAULT警告出现。For the Procedure 2:对于方法2：At the electrical connector 11JR-B:-Between the pins A and B, there is 28VDC.在电插头11JR-B上：-销钉A与B之间为28VDC。NOTE: The 28VDC is only applied for 15 seconds. 注释：2