WOHA33_2632288_35_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WOHA332632_35_288DIC 培训方式2632288通用类/GenericTitleOperational Check of Ram Air Turbine Automatic Deployment Detailed 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并详细目视检查冲压涡轮AMM 29-24-00-710-804-012017-01-01A/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BLNVAT-292400-710-804HR004008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 5PVG730 CA730 CAAccess Panels/接近盖板Zones/区域Written/编写Approved/批准633HB2102017-03-202017-03-24TOOLS/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)2460007174PIN - GROUNDLOCK, MLGTO2ALL(必需/Necessary)3D23304000PIN-GROUNDLOCK, NLGTO1ALL(必需/Necessary)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)298F29208217000PIN SAFETY,RATTO1ALL(视情/As Necessary)3PGRAT1-1TEST EQUIPMENT - RAM AIR TURBINETO1ALL(视情/As Necessary)AGE10600C; HRT01498F29208412000DEVICE-R/I RATTO1ALL(视情/As Necessary)598F29208544000HOSE 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1CML19-011SCOTCH BRITE PADSCH1ALL(必需/Necessary)或百洁布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)15CML19-003CLEANING ABSORCH1ALL(视情/As Necessary)16CML06-011SOLID FILM LUBRICANTCH1ALL(视情/As Necessary)CMl06-002171702934A（禁订）RAT-RAM AIR TURBINEAS1ALL(视情/As Necessary)18CML09-014CORROSION INHIBITIVE COATINGCH1ALL(视情/As Necessary)19M83248-1-021packingAS2ALL(视情/As Necessary)20CML04-002GRAPHITED MINERAL GREASECH1ALL(视情/As Necessary)21766542AGEARBOXAS1ALL(视情/As Necessary)22732040WASHERAS1ALL(视情/As Necessary)23LN29557KA16-75SHIM-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 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-292400-710-804 HR004008 W/O:2632 AC:BLNV页码，3 / 58工卡Job card:HA33-292400-01-1TITLEOperational Check of Ram Air Turbine Automatic Deployment Detailed Inspection of the Ram Air Turbine once extendedPerfInsp标题操作检查冲压涡轮的自动放出并详细目视检查冲压涡轮工作者检查者Operational Check of Ram Air Turbine Automatic Deployment Detailed Inspection of the Ram Air Turbine once extended操作检查冲压涡轮的自动放出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。WARNING: MAKE SURE THAT THE RAT TRAVEL RANGE IS CLEAR BEFORE YOU GET THE RAM AIR TURBINE TEST PAGE. THE RAT CAN EXTEND DURING THE RAM AIR TURBINE TEST AND CAUSE INJURY TO PERSONS AND/OR DAMAGE.警 告：冲压涡轮测试前确保其涉及的范围被清理干净。冲压涡轮测试时肯恩会扩大影响范围并 导致人员伤亡。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：ANELDESGNATIONFINLOCATION 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 013-300，302-350/ 适用于CRK手册有效号为 013-300，302-350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-E