2015下半年春秋檢工卡8d項(xiàng)目tgpe

1、TGPE-A242400-01-2SPRING AIRLINES MED第 1 頁(yè)，共 7 頁(yè)標(biāo)題工作者檢驗(yàn)者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.NOTE: You can do this test with the Blue electric pump or wiground hydraulic cart.注：此工作可通過(guò)藍(lán)電動(dòng)泵或地面車(chē)進(jìn)行。Job Set-up工作準(zhǔn)備Aircraft Maenance Configuration飛機(jī)構(gòu)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：確保飛行舵面行程區(qū)域內(nèi)無(wú)。飛行面的移動(dòng)會(huì)導(dǎo)致受傷和/或設(shè)備損壞。Energize the aircrafectrical circuits (Ref. AMM TASK 24-41-00-861-002).給飛機(jī)通電(參考 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).執(zhí)行電子儀表系統(tǒng) (EIS) 起動(dòng)程序(僅對(duì)上 ECAM 顯示組件和下 ECAM 顯示組件)(參考 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 藍(lán)電動(dòng)泵 或地面車(chē)給藍(lán)系統(tǒng)增壓 ( 參考 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.確認(rèn)縫翼/襟翼?xiàng)U在 0 位置。Make suret the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER(98D27803500001) is inition on the flap/slat control lever.確認(rèn)襟翼縫翼?xiàng)U零位鎖定工具(98D27803500001)在襟翼/縫翼?xiàng)U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 頁(yè)，共 7 頁(yè)標(biāo)題工作者檢驗(yàn)者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.將警告牌放置到位提示其它不要襟翼/縫翼?xiàng)U。(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，松開(kāi) LEAK MEASUREMENT VALVES/B 按鈕電門(mén)(OFF 燈亮)。Get acs to the Avionics Compartment接近電子艙P(yáng)ut an acs platform 2M (6 FT) at the acs doors 812 and 822 of the avionics compartment.將接近放在電子艙接近門(mén) 812 和 822 處。Open the acs doors 812 and 822 of the avionics compartment.打開(kāi)電子

7、艙接近門(mén) 812 和 822。Make suret this(these) circuit breaker(s) is(are) closed:確保下列電路跳開(kāi)關(guān)已閉合：Procedure步驟Operational Test of the Emergency Generation System應(yīng)急發(fā)電系統(tǒng)PANEL面板DESIGNATION名稱(chēng)FIN功能號(hào)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 頁(yè)，共 7 頁(yè)標(biāo)題工作者檢驗(yàn)者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.ACTION措施RESULT結(jié)果1. On the panel 21VU, on the EMER ELEC PWR section:在面板 21VU

9、的“應(yīng)急電源”部分上：-lift the safety guard,掀開(kāi)保險(xiǎn)蓋，-push and hold the EMER GEN TEST pushbutton switch.按壓并保持 EMER GEN TEST 按鈕電門(mén)。On the lower ECAM display unit:在下 ECAM 顯示組件：the ELEC page comes o view automatically,“ELEC” (電源) 頁(yè)面自動(dòng)出現(xiàn)，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 匯流條以及 DC1 和 DC ESS 匯流條之間的綠線。the EMER GEN and ESS TR indications are shown in white. The related parameters are shown in green,EMER GEN 和 ESS TR 顯示為白色，相應(yīng)參數(shù)顯示為綠色。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 匯流條之間，EMER GEN 和 ESS TR 之間以及 ESSTR 和 DS 流條之間的綠線出現(xiàn)。the SHED indication comes o view, below the AS and DS busbar indications.SHED 指示出現(xiàn)在 AS 和 DS匯流條指示下方。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 頁(yè)，共 7 頁(yè)標(biāo)題工作者檢驗(yàn)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： 如果主變壓整流器沒(méi)有連上：相應(yīng)參數(shù)顯示為琥珀色且主 TR 與 DC 主匯流條間的綠線不顯示。在 CSM/G (恒速馬達(dá)/發(fā)電機(jī)) 測(cè)試期間(當(dāng)恒速馬達(dá)/發(fā)電機(jī)運(yùn)轉(zhuǎn)時(shí))，按壓 103VU 面板上的按鈕電門(mén)(15PU) 以復(fù)位主變壓整流器。2. On the panel 21VU:在面板 21VU 上：-release the EMER GEN TEST pushbutton switch.松開(kāi)應(yīng)急發(fā)電測(cè)試按鈕電門(mén) EMER GEN TEST。On the panel 21VU:在面板 21VU 上：- checkt the safety guard is back in its pl

14、ace.檢查保護(hù)蓋是否已回到原位。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) 藍(lán)電動(dòng)泵自動(dòng)停止（如果用藍(lán)電動(dòng)泵進(jìn)試）。(2) 如果沒(méi)有，在 50VU 面板上的HYD部分，按壓然后松開(kāi) BLUE PUMP/OVRD按壓電門(mén)。確保 ON 燈熄滅。藍(lán)系統(tǒng)電動(dòng)泵必須停止。做應(yīng)急發(fā)電系統(tǒng)排故(參考 TSMTGPE-A242400-01-2SPRING AIRLINES MED第 5 頁(yè)，共 7 頁(yè)標(biāo)題工作者檢驗(yàn)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按壓 ELEC 鍵調(diào)出 ELEC 頁(yè)。On the lower ECAM display unit:在下 ECAM 顯示組件上：- the normal configuration comeso view: the emergency AC generator stops and the AC1s AS busbars 顯現(xiàn)正常構(gòu)型：應(yīng)急交流發(fā)電機(jī)

17、停止，AC1給 AS 匯流條供電。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 繼續(xù)給 D S 匯流條供電，如果出現(xiàn)這種情況，在交流電源中心 123VU 面板打開(kāi)再閉合跳開(kāi)關(guān) 1XC，并確認(rèn) ESS TR 不再給 D S

18、匯流條供電。4. On the ECAM control panel:在 ECAM 控制面板上：-push the STS key to get the SUS page.按壓 STS 鍵以進(jìn)入 SUS 頁(yè)面。On the SUS page of the lower ECAM display unit:在下 ECAM 顯示組件上的 SUS 頁(yè)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 項(xiàng)下顯示 AIR BLEED 指示，需要重置兩個(gè) FWC。這樣，在下次飛行的T FLIGHT REPORT 中將不會(huì)保留有此指示。Do the stept follows.TGPE-A242400-01-2SPRING AIRLINES MED第 6 頁(yè)，共 7 頁(yè)標(biāo)題工作者檢驗(yàn)者TitleOPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEMMech.Insp.進(jìn)行下面的步驟。5. On the pan

20、el 49VU:-open and close the circuit breaker 3WW.在 49VU 面板上：-斷開(kāi)再閉合電路跳開(kāi)關(guān) 3WW。On the panel 121 VU:-Open and close the circuit breaker 2WW.在 121 VU 面板上：-斷開(kāi)再閉合電路跳開(kāi)關(guān) 2WW。On the SUS page:在 SUS 頁(yè)面上：- the AIR BLEED indication goes out of view.AIR BEED 指示。3.Close-up結(jié)束A. Put the aircraft back to its initial co

21、nfiguration.將飛機(jī)恢復(fù)到初始構(gòu)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).如果測(cè)試持續(xù)超過(guò) 30 秒，在面板 22VU 上，按鈕電門(mén) EXTRACT 上的 FAULT 燈亮。在這種情況下，松開(kāi)然后按壓按鈕電門(mén) EXTRACT(FAULT 燈滅)。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，按壓 LEAK MEASUREMENT VALVE S/B (滲漏計(jì)量活門(mén)