2015下半年春秋检工卡8d项目tgpe

1、TGPE-A242400-01-2SPRING AIRLINES MED第 1 页，共 7 页标题工作者检验者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.NOTE: You can do this test with the Blue electric pump or wiground hydraulic cart.注：此工作可通过蓝电动泵或地面车进行。Job Set-up工作准备Aircraft Maenance Configuration飞机构型WARNING: MAKE SURET THE TRAVEL R

2、ANGES OF THE FLIGHT CONTROLS ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TOS AND/OR DAMAGE.警告：确保飞行舵面行程区域内无。飞行面的移动会导致受伤和/或设备损坏。Energize the aircrafectrical circuits (Ref. AMM TASK 24-41-00-861-002).给飞机通电(参考 AMM TASK 24-41-00-861-002)。Do the EIS start procedure (Upper ECAM DU and lower ECA

3、M DU only)(Ref. AMM TASK 31-60-00-860-001).执行电子仪表系统 (EIS) 起动程序(仅对上 ECAM 显示组件和下 ECAM 显示组件)(参考 AMM TASK 31-60-00-860-001)。Pre rize the Blue hydraulic system with the bule electric pump (Ref. AMM TASK29-10-00-863-003) or wi ground er supply (Ref. AMM TASK 29-10-00-863-003).用 蓝电动泵 或地面车给蓝系统增压 ( 参考 AMM TA

4、SK29-10-00-863-003)。On the FLAPS control panel 114VU:在襟翼控制面板 114VU：Make suret the slat/flap control lever is on the 0ition.确认缝翼/襟翼杆在 0 位置。Make suret the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER(98D27803500001) is inition on the flap/slat control lever.确认襟翼缝翼杆零位锁定工具(98D27803500001)在襟翼/缝翼杆上。Put a warnin

5、g notice inition tols not to operate the flap/slat control lever.TGPE-A242400-01-2SPRING AIRLINES MED第 2 页，共 7 页标题工作者检验者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.将警告牌放置到位提示其它不要襟翼/缝翼杆。(5) On the HYD section of the panel 50VU, release the LEAK MEASUREMENT VALVES/B pushbutton switc

6、h (the OFF legend come on).在面板 50VU 的 HYD部分，松开 LEAK MEASUREMENT VALVES/B 按钮电门(OFF 灯亮)。Get acs to the Avionics Compartment接近电子舱Put an acs platform 2M (6 FT) at the acs doors 812 and 822 of the avionics compartment.将接近放在电子舱接近门 812 和 822 处。Open the acs doors 812 and 822 of the avionics compartment.打开电子

7、舱接近门 812 和 822。Make suret this(these) circuit breaker(s) is(are) closed:确保下列电路跳开关已闭合：Procedure步骤Operational Test of the Emergency Generation System应急发电系统PANEL面板DESIGNATION名称FIN功能号LOCATION位置49VUFWS/FWC1/SPLY3WWF01105VUELEC/CSM/G /EV AUTO/SPLY7XEC01106VUCSM/G /EV/MAN/SPLY6XEB04106VUESSTOR/CTL5PEC02106

8、VUESS TR/SPLY4PEC01121VUEIS/FWC2/SPLY2WWQ07122VUELEC/EMER GEN AUTO/29XEZ26122VUELEC/EMER GEN AUTO/111XEZ25TGPE-A242400-01-2SPRING AIRLINES MED第 3 页，共 7 页标题工作者检验者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.ACTION措施RESULT结果1. On the panel 21VU, on the EMER ELEC PWR section:在面板 21VU

9、的“应急电源”部分上：-lift the safety guard,掀开保险盖，-push and hold the EMER GEN TEST pushbutton switch.按压并保持 EMER GEN TEST 按钮电门。On the lower ECAM display unit:在下 ECAM 显示组件：the ELEC page comes o view automatically,“ELEC” (电源) 页面自动出现，the green lines bet n the AC1 and the A S busbar and the DC1 and the DC ESS busb

10、ar go out of view,AC1 和 AS 汇流条以及 DC1 和 DC ESS 汇流条之间的绿线。the EMER GEN and ESS TR indications are shown in white. The related parameters are shown in green,EMER GEN 和 ESS TR 显示为白色，相应参数显示为绿色。the green lines bet n the EMER GEN and the A S busbar, the EMER GEN and the ESS TR, the ESS TR and the DC ESS bus

11、bar come o view,在 EMER GEN 和 AS 汇流条之间，EMER GEN 和 ESS TR 之间以及 ESSTR 和 DS 流条之间的绿线出现。the SHED indication comes o view, below the AS and DS busbar indications.SHED 指示出现在 AS 和 DS汇流条指示下方。NOTE: If the essential TR is not in line:. its related parameters are shown in amber and. the green line betn theTGPE-A

12、242400-01-2SPRING AIRLINES MED第 4 页，共 7 页标题工作者检验者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.essential TR and the Dsential busbar is not shown.- During the CSM/G test (when the CSM/G is running), push the TR RESET pushbutton switch (15PU) on the panel 103VU to reset the essential

13、TR.注： 如果主变压整流器没有连上：相应参数显示为琥珀色且主 TR 与 DC 主汇流条间的绿线不显示。在 CSM/G (恒速马达/发电机) 测试期间(当恒速马达/发电机运转时)，按压 103VU 面板上的按钮电门(15PU) 以复位主变压整流器。2. On the panel 21VU:在面板 21VU 上：-release the EMER GEN TEST pushbutton switch.松开应急发电测试按钮电门 EMER GEN TEST。On the panel 21VU:在面板 21VU 上：- checkt the safety guard is back in its pl

14、ace.检查保护盖是否已回到原位。NOTE: (1) The Blue electric pump stops automatically(if you do the test with the Blue electric pump). (2)If not, on the HYD section of the panel 50VU, push and release the BLUE PUMP/OVRD push- button switch. Make suret the ON legend goes off. The Blue electric pump must stop. Do the

15、 trouble shooting of the emergency generation system (Ref. TSM TASK 24-24-00-810-806).注： (1) 蓝电动泵自动停止（如果用蓝电动泵进试）。(2) 如果没有，在 50VU 面板上的HYD部分，按压然后松开 BLUE PUMP/OVRD按压电门。确保 ON 灯熄灭。蓝系统电动泵必须停止。做应急发电系统排故(参考 TSMTGPE-A242400-01-2SPRING AIRLINES MED第 5 页，共 7 页标题工作者检验者TitleOPERATIONAL CHECK OF EMERGENCY GENERAT

16、ING SYSTEMMech.Insp.TASK 24-24-00-810-806)。3. On the ECAM control panel:在 ECAM 控制面板上：- push the ELEC key to get the ELEC page按压 ELEC 键调出 ELEC 页。On the lower ECAM display unit:在下 ECAM 显示组件上：- the normal configuration comeso view: the emergency AC generator stops and the AC1s AS busbars 显现正常构型：应急交流发电机

17、停止，AC1给 AS 汇流条供电。NOTE: It is sible t the ESS TR continues to supply the D S busbar. If this occurs, on the ACer center 123VU, open and close the circuit breaker 1XC and make suret the ESS TR no longers the DS busbar.注：有可能 ESS TR 继续给 D S 汇流条供电，如果出现这种情况，在交流电源中心 123VU 面板打开再闭合跳开关 1XC，并确认 ESS TR 不再给 D S

18、汇流条供电。4. On the ECAM control panel:在 ECAM 控制面板上：-push the STS key to get the SUS page.按压 STS 键以进入 SUS 页面。On the SUS page of the lower ECAM display unit:在下 ECAM 显示组件上的 SUS 页面：If the AIR BLEED sus maenance comeso view below theMAENANCE item, it is nesary to reset the two FWCs. Thus the FWCs will not k

19、eep a record of the indicationhe T FLIGHT REPORthe nextflight.如果在 MAENANCE 项下显示 AIR BLEED 指示，需要重置两个 FWC。这样，在下次飞行的T FLIGHT REPORT 中将不会保留有此指示。Do the stept follows.TGPE-A242400-01-2SPRING AIRLINES MED第 6 页，共 7 页标题工作者检验者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.进行下面的步骤。5. On the pan

20、el 49VU:-open and close the circuit breaker 3WW.在 49VU 面板上：-断开再闭合电路跳开关 3WW。On the panel 121 VU:-Open and close the circuit breaker 2WW.在 121 VU 面板上：-断开再闭合电路跳开关 2WW。On the SUS page:在 SUS 页面上：- the AIR BLEED indication goes out of view.AIR BEED 指示。3.Close-up结束A. Put the aircraft back to its initial co

21、nfiguration.将飞机恢复到初始构型.If the test continues for moren 30 seconds, on the panel 22VU, the FAULT legend of the EXTRACT pushbutton switch comes on.his case, release then push the EXTRACT pushbutton switch (the FAULT legend goes off).如果测试持续超过 30 秒，在面板 22VU 上，按钮电门 EXTRACT 上的 FAULT 灯亮。在这种情况下，松开然后按压按钮电门 EXTRACT(FAULT 灯灭)。On the HYD section of the panel 50VU, push the LEAK MEASUREMENT VALVES/B pushbutton switch (the OFF legend goes off).在 50VU HYD()面板上，按压 LEAK MEASUREMENT VALVE S/B (渗漏计量活门