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/工作指令號SEQ NO/序列號WOHA332632_35_288DIC 培訓方式2632288通用類/GenericTitleOperational Check of Ram Air Turbine Automatic Deployment Detailed Inspection of the Ram Air Turbine once extendedMcd&Rev/廠家工卡&修訂日期標題操作檢查沖壓渦輪的自動放出并詳細目視檢查沖壓渦輪AMM 29-24-00-710-804-012017-01-01A/C/飛機號Subtask No/工卡號JC Rev/工卡版本號Workarea/工作區(qū)域Skill/工種Man Hour/工時BLNVAT-292400-710-804HR004008機身/AirframeMINP08:00MP Item/MP號Baseline/依據(jù)MP REV/ MP版本號Station/維修站Threshold/首檢Interval/重復檢HA33-292400-01-1MPD292400-01-1,MRB29.20.00/03,MRB29.20.00/05Issue 2 Revision 5PVG730 CA730 CAAccess Panels/接近蓋板Zones/區(qū)域Written/編寫Approved/批準633HB2102017-03-202017-03-24TOOLS/工具TOOLS NECESSARY/必須工具ITEM項目P/N件號DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注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異丙醇-Non Aqueous Cleaner-Isopropyl AlcoholTO1ALL(必需/Necessary)CML11-010TOOLS IF NECESSARY/視情工具ITEM項目P/N件號DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注198D27803000000LOCKING TOOL - FLAP/SLAT CONTROL LEVERTO1ALL(視情/As Necessary)298F29208217000PIN SAFETY,RATTO1ALL(視情/As Necessary)3PGRAT1-1TEST EQUIPMENT - RAM AIR TURBINETO1ALL(視情/As Necessary)AGE10600C; HRT01498F29208412000DEVICE-R/I RATTO1ALL(視情/As Necessary)598F29208544000HOSE SUPPORT - GMT, RATTO1ALL(視情/As Necessary)PARTS AND MATERIAL/航材NOTE:OPERATOR MUST GET AND INSTALL THE PARTS THAT CORRESPOND TO THE RELATIVE WORKORDER NO.注釋：請工作者嚴格按照工作指令號領取預定的航材裝機PARTS AND MATERIAL NECESSARY/必須航材ITEM項目P/N件號DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注1CML19-011SCOTCH BRITE PADSCH1ALL(必需/Necessary)或百潔布PARTS AND MATERIALIF NECESSARY/視情航材ITEM項目P/N件號DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注1AMS5687LOCKWIREAS1ALL(視情/As Necessary)CML19-0102MS24665-300PIN COTTERAS3ALL(視情/As Necessary)3M83248-1-908(7AB2)PACKINGAS2ALL(視情/As Necessary)4MIL-T-81533solventCH1ALL(視情/As Necessary)CML11-0045MS24665-155PINAS1ALL(視情/As Necessary)6MS24665-88PINAS2ALL(視情/As Necessary)7MIL-S-8802ADHESIVECH1ALL(視情/As Necessary)CML09-0018MIL-C-16173GREASECH1ALL(視情/As Necessary)CML05-005D9MIL-PRF-23827GREASECH1ALL(視情/As Necessary)CML04-00410VV-P-236VASELINECH1ALL(視情/As Necessary)CML04-01211NYCOTE7-11primer(18.33C-26.67C)CH1ALL(視情/As Necessary)CML07-00112CML03-003GREASECH1ALL(視情/As Necessary)13CML16-006SILICONE(base:F580-2080+hard:F275-160+thin:F850-1241)CH1ALL(視情/As Necessary)14CML05-002Non Hardening Jointing Putty - Medium Temp. AreaCH1ALL(視情/As Necessary)15CML19-003CLEANING ABSORCH1ALL(視情/As Necessary)16CML06-011SOLID FILM LUBRICANTCH1ALL(視情/As Necessary)CMl06-002171702934A（禁訂）RAT-RAM AIR TURBINEAS1ALL(視情/As Necessary)18CML09-014CORROSION INHIBITIVE COATINGCH1ALL(視情/As Necessary)19M83248-1-021packingAS2ALL(視情/As Necessary)20CML04-002GRAPHITED MINERAL GREASECH1ALL(視情/As Necessary)21766542AGEARBOXAS1ALL(視情/As Necessary)22732040WASHERAS1ALL(視情/As Necessary)23LN29557KA16-75SHIM-LAMINATEDAS1ALL(視情/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頁碼，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標題操作檢查沖壓渦輪的自動放出并詳細目視檢查沖壓渦輪工作者檢查者Operational Check of Ram Air Turbine Automatic Deployment Detailed Inspection of the Ram Air Turbine once extended操作檢查沖壓渦輪的自動放出并詳細目視檢查沖壓渦輪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：確認執(zhí)行工作前，在以下位置已放置安全裝置和警告牌： - 飛行控制 - 飛行控制舵面 - 起落架及其隨動門 - 運動部件 部件運動會造成人員傷亡。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：當可能發(fā)生閃電時，切勿戴耳機或碰觸與飛機相連的電纜/電線。閃電是危險的。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)的皮托管加熱跳開關，然后再拔出PHC (1, 2 和 3)跳開關。如果不按照順序操作：- 皮托管會變得很熱。- 可能導致人員受傷和設備損壞。WARNING: DO NOT TOUCH THE PROBES DURING OR IMMEDIATELY AFTER THIS PROCEDURE. THE PROBES ARE HOT AND CAN BURN YOU. 警 告：工作中或者工作結(jié)束不要立即觸碰皮托管。過熱的皮托管會灼傷皮膚。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。遵守材料廠家說明和當?shù)匾?guī)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：沖壓渦輪測試前確保其涉及的范圍被清理干凈。沖壓渦輪測試時肯恩會擴大影響范圍并 導致人員傷亡。CAUTION: REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE TEST.注 意：執(zhí)行測試之前，將皮托管套取下。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：確認已重置斷路開關5JR。如果不進行重置，在發(fā)動機啟動或關車時將不會有綠系統(tǒng)液壓壓力。1. Job Set-up /工作準備 A. Safety Precautions /安全措施 M (1) Put the safety barriers in position. /將安全護欄放置在位。(2) Put the WARNING NOTICE(S) in position to tell persons that the RAT is in operation. 設置警告標牌，提示人員RAT正在被操作。B. Get Access /打開接近 M (1) Open the MLG doors (Ref. AMM TASK 32-12-00-010-801) . 打開MLG門(參考 AMM TASK 32-12-00-010-801)。(2) Put the access platform in position below the RAT. 在RAT下部將接近平臺放置在位。(3) Open the access panel 633HB . /打開接近面板633HB。C. Get access to the avionics compartment. Then open, safety and tag this(these) circuit breaker(s): T 接近電子艙，拔出以下跳開關、設置安全夾并掛警告標牌：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：確保以下跳開關打開：2DA1, 2DA2, 2DA3, 5DG1, 5DG2.這樣可以防止探測器和窗加熱系統(tǒng)的不正確動作 721VUPHC 32DA3N07 721VUPHC 12DA1P12 722VUPHC 22DA2X40 722VUWHC 25DG2X39 742VUWHC 15DG1G64D. Aircraft Maintenance Configuration / 飛機維護構(gòu)型 T (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-801) . 接通飛機電源(參考 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) . 執(zhí)行EIS啟動程序(僅EWD DU, SD DU) (參考 AMM TASK 31-60-00-860-801)。(3) Make sure that the engines 1 and 2 are not in operation. 確認1號和2號發(fā)動機未工作。(4) Make sure that the Green hydraulic system is depressurized (Ref. AMM TASK 29-00-00-864-804) . 確認綠液壓系統(tǒng)已釋壓(參考 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，松開YELLOW/ELEC PUMP (4JJ)和GREEN/ELEC PUMP (4JV)按鈕電門（OFF燈亮）。(6) For the Procedure 1, remove the PIN - SAFETY, RAT (98F29208457000) from the RAT if installed (Ref. AMM TASK 29-24-00-081-801) . 對于方法1，從RAT上拆除RAT安全銷(98F29208457000) (如果安裝)(參考 AMM TASK 29-24-00-081-801)。 (7) For the Procedure 2, /對于方法2 (a) Install the PIN - SAFETY, RAT (98F29208457000)at the RAT (Ref. AMM TASK 29-24-00-481-801) . 在RAT上，安裝RAT安全銷(98F29208457000)(參考AMM TASK 29-24-00-481-801)。 (b) Disconnect the electrical connector 11JR-B from the RAT. 從RAT脫開電插頭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，按壓C/B鍵（在SD上，出現(xiàn)C/B頁面）。確認SD未顯示以下跳開關：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：工作中或者工作結(jié)束不要立即觸碰皮托管。過熱的皮托管會灼傷皮膚。CAUTION: REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE TEST. 注 意：執(zhí)行測試之前，將皮托管套取下。2. Procedure /步驟 (Ref. Fig. Engine Operation Simulator - Engine 2 SHEET 1) (Ref. Fig. Engine Operation Simulator - Engine 1 SHEET 1)(參考圖Fig. Engine Operation Simulator - Engine 2 SHEET 1) (參考圖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，確認RAT行程內(nèi)無障礙。RAT做動會導致人員受傷和設備損傷。*ON A/C CRK 013-300，302-350/ 適用于CRK手冊有效號為 013-300，302-350的飛機*ON A/C HKC ALL/適用于HKC手冊所有飛機*ON A/C CHH ALL/適用于CHH手冊所有飛機Subtask29-24-00-710-064-EA. Operational Test of the RAT Automatic Deployment Function after a Total Engine Flameout T DIC 操作測試RAT在全部發(fā)動機熄火情況下的自動放出功能(Ref. Fig. Engine Operation Simulator - Engine 2 SHEET 1)(參考圖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 釋：無需RAT放出，可以運用2種方法檢查RAT自動放出功能。-方法1，RAT在首次自動放出測試時放出。對于后續(xù)放出測試，當放出電磁活門工作時，會聽到滴答聲。-方法2，RAT在前兩次放出測試時保持收上，并測量電插頭11JR-B的電壓。進行第三次放出測試時，將電插頭11JR-B連接到RAT，在測試中，RAT會放出。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 釋：一個MCDU用于ADR RAM AIR TURBINE TEST（簡稱(ADR) MCDU），第二個用于起落架模擬/ LGCIU(簡稱(LGCIU) MCDU)。ACTION/操作RESULT/結(jié)果1. On the ELEC panel 235VU:-push and release the BAT1, BAT2 and APU BAT P/BSWs.在ELEC面板235VU上：-按壓并松開BAT1, BAT2和APU BAT按鈕電門。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按鈕電門OFF燈點亮。2. On the ELEC panel 235VU:-push and release the EXT A P/BSW在ELEC面板235VU上：-按壓并松開EXT A按鈕電門。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按鈕電門：-ON燈熄滅- AVAIL燈點亮。3. On the SIMULATOR-ENGINE OPERATION (98F29103004000) :-Make sure that the switches are in the DE-ENERGIZED position.在發(fā)動機操作模擬器(98F29103004000)上：-確認電門都處于DE-ENERGIZED位。4. On the electronic rack 800VU:-Get access to the plugs on the R lateral connector plate 802VU.在電子架800VU上：-接近R水平插板802VU上的插頭。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. 模擬2號發(fā)動機運轉(zhuǎn)，執(zhí)行以下步驟：-在插板802VU上，脫開插頭2506VC-A并連接發(fā)動機操作模擬器(98F29103004000)商定義為2506VC和2506VC-A的電插頭-定義為2號發(fā)動機的鱷魚夾接地。5. On the ELEC panel 235VU:-Push the EXT A P/BSW.在ELEC面板235VU上：-按壓EXT A按鈕電門。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按鈕電門：-AVAIL燈熄滅-ON燈點亮。6. On the ELEC panel 235VU:-Push the BAT1, BAT2 and APU BAT P/BSWs.在ELEC面板235VU上：-按壓BAT1, BAT2和APU BAT按鈕電門。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按鈕電門OFF燈熄滅。7. On the SIMULATOR-ENGINE OPERATION (98F29103004000) :-Set the ENGINE 2 switches (24KS2-35KS2) to the ENERGIZED position.在發(fā)動機操作模擬器(98F29103004000)上：- 將ENGINE 2 電門(24KS2-35KS2) 設置到ENERGIZED位。On the 800VU:-You hear a closing click when the relays are energized.在800VU上：-當繼電器通電時，會聽到結(jié)束的喀噠聲。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按鈕電門上的FAULT燈點亮。8. On the ECAM control panel:-push the HYD key.在ECAM控制面板上：-按壓HYD鍵。On the SD:-the HYD page comes into view,-the RAT triangle symbol is white.在SD上：-出現(xiàn)HYD頁面- RAT三角標志為白色。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啟動A/C速度模擬（參考34-13-00-710-804）。NOTE: You must not use the MCDU MENU key to stop the ADR RAM AIR TURBINE TEST.注釋： 禁止使用MCDU MENU鍵終止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) . 注釋：如果ADR 沖壓空氣渦輪測試未完成：-執(zhí)行ADIRS停止程序(參考 AMM TASK 34-10-00-860-803)，等待至少20s然后執(zhí)行ADIRU啟動程序(參考 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/起落架模擬菜單啟動飛行狀態(tài)模擬（參考32-69-00-860-801）。使用NOSE+LH+RH菜單，再按壓FLIGHT和UPLOCKED對應行選鍵。On HYD panel 245VU:- The FAULT legends of the GREEN/ENG 1 and BLUE/ENG 1 P/BSWs come on.在245VU面板液壓部分- GREEN/ENG 1 和 BLUE/ENG 1 P/BSWs上的FAULT燈點亮11. Make sure that on the panel 742VU, the subsequent circuit breakers are closed:確認面板742VU上，以下跳開關已關閉：-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