成果fin已完成檢eoa33290011r

1、EOA33-29-0011 R10 2014-08-25頁碼，1 / 22Airlines Limited03110-01香港航空 Airlines MEDAirlines LimitedWO NO/工作指令號(hào)SEQ NO/序列號(hào) TitleInspect the Leakage of Hydraulic SystemMcd&Rev/廠家工卡&修訂日期標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏A/C/飛機(jī)號(hào)/組別EO JC No./EO 工卡EO JC Rev/工卡版本W(wǎng)orkarea/工作區(qū)域Skill/工種Man Hour/工時(shí) EOA33-29-0011 R10機(jī)身/AirframeAIR

2、P04:00Baseline/依據(jù)Operator EO/營運(yùn)人 EOEO Rev/EO 版本W(wǎng)ork Type/工作類別Threshold/首檢Interval/重復(fù)檢AMM29-11-00/29-12-00/29-13-00EOA33-29-0011R107CA7CAWritten/編寫2014-08-25Reviewed/審核2014-08-25Approved/批準(zhǔn)2014-08-25Accomplished完工簽署Complete Date完工日期Station維修站REASON & DESCRIPTION/原因及描述運(yùn)行中收到液壓系統(tǒng)發(fā)生漏油報(bào)告較多，故下發(fā) EO 進(jìn)行定期

3、對(duì)多發(fā)滲漏部件進(jìn)行 定期檢查。Some Hydraulic system leakage reports were received duringoperating, so issue the EO for leakage inspection of Hydraulic system at regular intervals.運(yùn)行中收到液壓系統(tǒng)發(fā)生漏油報(bào)告較多，故下發(fā) EO 進(jìn)行定期對(duì)多發(fā)滲漏部件進(jìn)行 定期檢查。Some Hydraulic system leakage reports were received duringoperating, so issue the EO for lea

4、kage inspection of Hydraulic system at regular intervals.R01 改版原因：新飛機(jī)引進(jìn)，增加 B-LNK 適用性。Reason for R01: add B-LNK applicability due to new aircraftdelivered.R02 改版原因：反饋表格中加入英文注釋。Reason for R02: add english instruction in the feedback form.R03 改版原因：新飛機(jī)引進(jìn)，增加 B-L NL 和 B-LNW 適用性,修改了計(jì)劃信息。EOA33-29-0011 R10 2

5、014-08-25頁碼，2 / 22Reason for R03: revise applicability to add new aircrafts B-LNL and B-LNW and amend PLAN information.R 04 改版原因：新飛機(jī)引進(jìn)，增加 B-LNM 適用性,修改了計(jì)劃信息。Reason for R 04: revise applicability to add new aircrafts B-LNM and amend PLAN inf ormation.R05 改版原因：新飛機(jī)引進(jìn)，增加 B-LNN 適用性,修改了計(jì)劃信 息。Reason for R05

6、: revise applicability to add new aircrafts B-LNN andamend PLAN information.R06 改版原因：新飛機(jī)引進(jìn)，增加 B-LNO 適用性,修改了計(jì)劃信息。Reason for R06: revise applicability to add new aircrafts B-LNO andamend PLA N information.R07 改版原因：新飛機(jī)引進(jìn)，增加 B-LNP 適用性,修改 了計(jì)劃信息。Reason for R07: revise applicability to add new aircraft s B

7、-LNP and amend PLAN information.R08 改版原因：改版適用性， 刪除 B-LNN 適用性。Reason for R08: revise applicability tete airc raft B-LNN.R09 改版原因：新飛機(jī)引進(jìn)，增加 B-LNV 適用性。Reason f or R09: revise applicability to add new aircrafts B-LNV.R10 改 版原因：增加對(duì)于剎車總管的檢查，修改航材信息。Reason for R10: Add ch eck brake manifold，revise parts.TOOL

8、S/工具TOOLS NECESSARY/必須工具ITEM項(xiàng)目P/N件號(hào)DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注EOA33-29-0011 R10 2014-08-25頁碼，3 / 22198F32104013000SAFETY COLLAR-DOORMLGTO2ALLALLTOOLS IF NECESSARY/視情工具ITEM項(xiàng)目P/N件號(hào)DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注PARTS AND MATERIAL/航材NOTE:OPERATOR MUST GET A

9、ND INSTALL THE PARTS THAT CORRESPOND TO THE RELATIVE WORKORDER NO.注釋： 請(qǐng)工作者嚴(yán)格按照工作指令號(hào)領(lǐng)取預(yù)定的航材裝機(jī)PARTS AND MATERIAL NECESSARY/必須航材ITEM項(xiàng)目P/N件號(hào)DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注PARTS AND MATERIALIF NECESSARY/視情航材ITEM項(xiàng)目P/N件號(hào)DESCRIPTION名稱EQTP類型QTY數(shù)量APP適用性Conditions note互換信息及備注1NAS1611-015(7

10、3B4)PACKINGAS1ALL視情/OC2NAS1611-119PACKINGAS2ALL視情/OC3NAS1612-12(32A1)PACKINGAS4ALL視情/OC4NAS1612-16PACKINGAS4ALL視情/OC5NAS1612-8(32A1)PACKINGAS2ALL視情/OC6NAS1612-10(73B2)PACKINGAS1ALL視情/OC7NAS1612-4PACKINGAS2ALL視情/OC8NAS1612-6(7AB10)PACKINGAS2ALL視情/OC9088256-04644(AOG)ACCUMULATOR-BRAKEAS1ALL視情/OC10NSA8

11、213-16SEALAS6ALL視情/OC11NSA8671-16RING-BACKUPAS6ALL視情/OC12NSA8674-16RING-BACK UPAS6ALL視情/OC13CML19-010LOCKWIREAS1ALL視情/OC14CML16-003primerCH1ALL視情/OC15088259-04644ACCUMULATOR-POWERAS1ALL視情/OC16MS21924-8FITTINGAS1ALL視情/OC17918B0000-01PCU-POWER CONTROLUNIT,SLATAS1ALL視情/OC182-1577-9BRAKE-MULTIPLE DISKAS

12、1ALL視情/OC19FA04804AFILTER ASSYAS1ALL視情/OC20NAS1601-119PACKINGAS2ALL視情/OCPARTS INFORMATION/部件信息:NOTE: The component in PN,SN form is need to do periodic maintenance. For the return repair or retrofit，the form is PN,SN of the removed component. And the PN-IN,SN-IN would be written according to new par

13、ts after finish. For the non- returns(such as weight, test)， the form is PN,SN of the on-wing maintenance component. And fill the PN-IN,SN-IN with bias after finish.注釋：件號(hào)、序號(hào)欄指需要定期執(zhí)行維修工作的部件。對(duì)于要求更換拆下返廠工作的部件，該欄指拆下件、序號(hào)信息。完成工作后裝上件號(hào)和序號(hào)欄請(qǐng)?zhí)顚懴嚓P(guān)裝機(jī)件信息；對(duì)于在位執(zhí)行工作的（如稱重、測試等），該欄指在位工作部件件、序號(hào)信息，完成工作后裝上件號(hào)和序號(hào)請(qǐng)用斜線畫去。PN/件號(hào)

14、SN/序號(hào)ATA/章節(jié)ZONE/區(qū)域FIN/代碼LOCATION/裝機(jī)位置EOA33-29-0011 R10 2014-08-25頁碼，4 / 22PN-IN裝上件號(hào)SN-IN裝上序號(hào)REMOVAL REASON AND COMPONENT TASK REQUEST拆件原因及其部件工作要求TASK NOTE工作注釋IMPORTANT NOTE: In the event of any discrepancies between theinstruction and the English instruction, the English procedure should prevail. Re

15、cord Additional Work/Findings(If Applicable) Reference No. 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-145 and in respect to that

16、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 / 129

17、5 * 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 * Other:* Signature:Authorization No.:Date: EOA33-29-0011 R10 2014-08-25頁碼，5 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓

18、系統(tǒng)滲漏工作者檢查者WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE CORRECTLY INSTALLED ON THE LANDING GEAR. THIS PREVENTS UNWANTED MOVEMENT OF THE LANDING GEAR.警告：確保起落架安全銷已經(jīng)安裝好，這將確保起落架不會(huì)意外收起。WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES. WORK ON THE HYDRAULIC SYSTEMS CAN BE DANGEROUS.警告：遵守液壓安全程序，液壓系統(tǒng)工作會(huì)比

19、較危險(xiǎn)。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 INJURES.警告：在以下區(qū)域工作時(shí)確保安全防護(hù)和警告標(biāo)識(shí)已經(jīng)準(zhǔn)備

20、好：-飛控系統(tǒng)-飛控表面-起落架和相關(guān)的艙門-可移動(dòng)的部件這些部件作動(dòng)可能傷害到人A. Preparation/準(zhǔn)備1. Make sure that the Aircraft Electrical Circuits are energized (Ref. AMM TASK 24-41-00-861-801) .確保飛機(jī)電源已接好（參考 AMM TASK 24-41-00-861-801）2. Make sure that the Green, Blue and Yellow hydraulic system are depressurized and put it in the mainte

21、nance configuration. (Ref. AMM TASK 29-00-00-864-804) .確保綠、藍(lán)、黃液壓系統(tǒng)已經(jīng)釋壓并處于維護(hù)構(gòu)型（參考 AMM TASK 29-00-00-864-804）3. Make sure that the Main Landing Gear (MLG) door is open (Ref. AMM TASK 32-12-00-010-801) and Install the safety device on the actuator of the MLG door (Ref. AMM TASK 32-00-00-481-802)打開做主起落架

22、艙門（參考 AMM TASK 32-12-00-010-801）并安裝主起落架艙門作動(dòng)器安全防護(hù)裝置（參考 (Ref. AMM TASK 32-00-00-481-802)4. Make sure that the access panel 195CB, 195DB are removed拆除接近改版 195CB、195DB。B. Procedure/步驟1. Visual inspection Green HP Filter Manifold (FIN 5102JM) and attachments inclouding (Ref. FIG 1) :EOA33-29-0011 R10 201

23、4-08-25頁碼，6 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者- the union and connectors,- the check valve (FIN 5316JM101, 5316JM102)- the Fluid Sampling Valve (FIN 5123JM1)- the filter cup (FIN 5111JM101, 5111JM102) and so onIf you find sign of leakage, perform t

24、he process refer to applicable TASK AMM 29-11-45-400-801, 29-11-53-400-806, 29-11-53-400-805, 20-23-22-910-801,29-11-42-400-801.參考圖 1 目視檢查綠系統(tǒng)HP FILTER MANIFOLD (FIN 5102JM)區(qū)域，包括其附件:- 管接頭- 單向活門(FIN 5316JM101, 5316JM102)- 取樣閥(FIN 5123JM1)- 濾杯(FIN 5111JM101, 5111JM102)等發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM 29-11-45-400-80

25、1，29-11-53-400-806，29-11-53-400-805，20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。2. Visual inspection Green HP Manifold (FIN 5103JM ) and attachments inclouding (Ref. FIG 2):- the union and connectors- HP Relief Valve (FIN 5021JM1 )- Pressure-Transducer （FIN 6JS1 ）- Pressure-Switch （FIN 7JS1 ）- Leakage-Measurem

26、ent Solenoid-Valve （FIN 1JL1 ）- Flight-Control Hydraulic Pressure-Switch （FIN 19CE1 ） and so on.If you find sign of leakage, perform the process refer to applicable TASK AMM 29-11-53-400-808, 29-19-51-400-801, 29-31-15-400-801, 29-31-16-400-801,29-11-32-400-801,27-92-17-400-801, 20-23-22-910-801.參考圖

27、 2 目視檢查綠系統(tǒng)HP MANIFOLD (FIN 5103JM)區(qū)域，包括其附件：- 管接頭- 釋壓活門(FIN 5021JM1)- 壓力傳感器(FIN 6JS1)- 壓力電門(FIN 7JS1)- 滲漏計(jì)量活門（FIN 1JL1）- 飛控液壓壓力電門（FIN 19CE1）等，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM 29-11-53-400-808, 29-19-51-400-801, 29-31-15-400-801,29-31-16-400-801, 29-11-32-400-801, 27-92-17-400-801, 20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。3

28、. Visual inspection Blue HP Manifold (FIN 6103JM ) and attachments inclouding (Ref. FIG 3 ):- the union and connectors- HP Relief Valve (FIN 5021JM2)- Pressure-Transducer （FIN 6JS2）- Pressure-Switch （FIN 7JS2）EOA33-29-0011 R10 2014-08-25頁碼，7 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic Syst

29、emPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者- Leakage-Measurement Solenoid-Valve （FIN 1JL2）- HP Filter （FIN 5111JM2）- the check valve (FIN 5316JM201)- the Fluid Sampling Valve (FIN 5123JM2)- Flight-Control Hydraulic Pressure-Switch （FIN 19CE2） and so on.If you find sign of leakage, perform the process refer to appl

30、icable TASK AMM 29-12-53-400-805, 29-12-32-400-801, 29-31-15-400-802, 29-31-16-400-802,29-19-51-400-802, 29-12-45-400-801, 29-12-53-400-806, 27-92-17-400-802,20-23-22-910-801.參考圖 3 目視檢查藍(lán)系統(tǒng)HP MANIFOLD (FIN 6103JM )區(qū)域，包括其附件：- 管接頭- 釋壓活門(FIN 5021JM2)- 壓力傳感器(FIN 6JS2)- 壓力電門(FIN 7JS2)- 滲漏計(jì)量活門（FIN 1JL2）- 油

31、濾（FIN 5111JM2）- 單向活門(FIN 5316JM201)- 液壓油取樣閥(FIN 5123JM2)- 飛控液壓壓力電門（FIN 19CE2）等，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM 29-12-53-400-805, 29-12-32-400-801, 29-31-15-400-802,29-31-16-400-802, 29-19-51-400-802, 29-12-45-400-801, 29-12-53-400-806,27-92-17-400-802, 20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。4. Visual inspection Green B

32、rake Manifold (FIN 5105JM ) and attachments inclouding (Ref. FIG 12 ):- the union and connectors- Priority Valve (FIN 5121JM)- Filter ASSY （FIN 5200GG）- Brake Selector Valve （FIN 4GG）and so on.If you find sign of leakage, perform the process refer to applicable TASK AMM 29-12-53-400-805, 29-12-32-40

33、0-801, 29-31-15-400-802, 29-31-16-400-802,29-19-51-400-802, 29-12-45-400-801, 29-12-53-400-806, 27-92-17-400-802,29-11-53-400-807,20-23-22-910-801.參考圖 12 目視檢查綠系統(tǒng)剎車 MANIFOLD (FIN 5105JM)區(qū)域，包括其附件：- 管接頭- 優(yōu)先活門(FIN 5121JM)- 油濾(FIN 5200GG)- 剎車選擇活門(FIN 4GG)等，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM 29-12-53-400-805, 29-12-32-400

34、-801, 29-31-15-400-802,29-31-16-400-802, 29-19-51-400-802, 29-12-45-400-801, 29-12-53-400-806,27-92-17-400-802, 29-11-53-400-807,20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。EOA33-29-0011 R10 2014-08-25頁碼，8 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者5. Visual inspectio

35、n Yellow HP Manifold (FIN 7103JM ) and attachments inclouding (Ref. FIG 4):- the union and connectors- HP Relief Valve (FIN 5021JM3)- Pressure-Transducer （FIN 6JS3）- Pressure-Switch （FIN 7JS3）- Leakage-Measurement Solenoid-Valve （FIN 1JL3）- HP Filter （FIN 5111JM3）- the check valve (FIN 5316JM301)- t

36、he Fluid Sampling Valve (FIN 5123JM3)- Flight-Control Hydraulic Pressure-Switch （FIN 19CE3） and so on.If you find sign of leakage, perform the process refer to applicable TASK AMM 29-13-53-400-803, 29-13-32-400-801, 29-31-15-400-803, 29-31-16-400-803,29-19-51-400-803, 29-13-45-400-801, 29-13-53-400-

37、804, 27-92-17-400-803,20-23-22-910-801.參考圖 4 目視檢查黃系統(tǒng)HP MANIFOLD (FIN 7103JM)區(qū)域，包括其附件：- 管接頭- 釋壓活門(FIN 5021JM3 )- 壓力傳感器(FIN 6JS3 )- 壓力電門(FIN 7JS3 )- 滲漏計(jì)量活門（FIN 1JL3 ）- 油濾（FIN 5111JM3 ）- 單向活門(FIN 5316JM301 )- 液壓油取樣閥(FIN 5123JM3 )- 飛控液壓壓力電門（FIN 19CE3 ）等，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM 29-13-53-400-803, 29-13-32-400-8

38、01, 29-31-15-400-803,29-31-16-400-803, 29-19-51-400-803, 29-13-45-400-801, 29-13-53-400-804,27-92-17-400-803, 20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。6. Visual inspect Green Power Accumulator (FIN 5151JM1 ), Blue Power Accumulator (FIN 5151JM2 ) and Yellow Power Accumulator (FIN 5151JM3 ) hydraulic tube co

39、nnectors. If you find sign of leakage, perform the process refer to applicable TASK AMM 29-11-42-400-801, 29-12-42-400-801, 29-13-42-400-801, 20-23-22-910-801 (Ref. FIG 5, 6, 7).參考圖 5，6，7 目視檢查綠，藍(lán)，黃系統(tǒng)儲(chǔ)壓器(FIN 5151JM1, 5151JM2, 5151JM3 )液壓接頭是否有液壓滲漏痕跡，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM9-11-42-400-801, 29-12-42-400-801,2

40、9-13-42-400-801, 20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。7. Visual inspect Parking Alternate Brake Accumulator （ FIN 5426GG , 5427GG ） and hydraulic tube connectors. If you find sign of leakage, perform the process refer to applicable TASK AMM 32-44-11-400-801,20-23-22-910-801 (Ref. FIG 8).參考圖 8 目視檢查藍(lán)系統(tǒng)剎車儲(chǔ)

41、壓器（FIN 5426GG , 5427GG ）及相關(guān)液壓管路接頭是否有液壓滲漏痕跡，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM 32-44-11-400-801, 20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。EOA33-29-0011 R10 2014-08-25頁碼，9 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者8. Visual inspect Slat Power Control-Unit (FIN 5000CW ) hydraulic tub

42、e connectors. If you find sign of leakage, perform the process refer to applicable TASK AMM 27-84-51-400-801, 20-23-22-910-801 (Ref. FIG 9).參考圖 9 目視檢查縫翼 PCU(FIN 5000CW )及相關(guān)液壓管路接頭是否有液壓滲漏痕跡，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM 27-84-51-400-801, 20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。.9. Visual inspect MLG-Door Bypass Valve (F

43、IN 5228GA , 5229GA ). If you find sign of leakage, perform the process refer to applicable TASK AMM 32-31-13-400-802, 20-23-22-910-801 (Ref. FIG 10).參考圖 10 目視檢查左右主起落架艙門旁通活門(FIN 5228GA , 5229GA )及相關(guān)液壓管路接頭是否有液壓滲漏痕跡，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng) AMM 32-31-13-400-802, 20-23-22-910-801章節(jié)要求完成處理并檢查測試措施。10. Visual inspect

44、primary and alternate Wheel Brake(FIN 5240GG , 5241GG , 5242GG , 5243GG , 5244GG , 5245GG , 5246GG ,5247GG ) tube connectors and seats. If you find sign of leakage, perform the process refer to applicable TASK AMM 32-42-27-400-801, 20-23-22-910-801 (Ref. FIG 11).參考圖 11 檢查所有剎車轂(FIN 5240GG , 5241GG ,

45、5242GG , 5243GG , 5244GG , 5245GG , 5246GG ,5247GG )主、備用剎車管路接頭及底座是否有液壓滲漏痕跡，發(fā)現(xiàn)油液滲漏痕跡則按照相應(yīng)AMM32-42-27-400-801, 20-23-22-910-801 章節(jié)要求完成處理并檢查測試措施。C. Close up/恢復(fù)1. Make sure that the access panel 195CB, 195DB are installed確認(rèn)接近蓋板 195CB、195DB 已經(jīng)安裝。2. Put the aircraft back to its usual configration.恢復(fù)飛機(jī)到正常狀

46、態(tài)。EOA33-29-0011 R10 2014-08-25頁碼，10 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者Figure 1. HP Filter Manifold Green hydraulic systemEOA33-29-0011 R10 2014-08-25頁碼，11 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者Figure

47、2. HP Manifold Green hydraulic systemEOA33-29-0011 R10 2014-08-25頁碼，12 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者Figure 3. HP Manifold - Blue hydraulic systemEOA33-29-0011 R10 2014-08-25頁碼，13 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerf

48、Insp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者Figure 4. HP Manifold Yellow hydraulic systemEOA33-29-0011 R10 2014-08-25頁碼，14 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者Figure 5. Green Power Accumulator 5151JM1EOA33-29-0011 R10 2014-08-25頁碼，15 / 22工卡 Job card:TITLEInspect the Leaka

49、ge of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者Figure 6. Blue Power Accumulator 5151JM2EOA33-29-0011 R10 2014-08-25頁碼，16 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標(biāo)題檢查飛機(jī)液壓系統(tǒng)滲漏工作者檢查者Figure 7. Yellow Power Accumulator 5151JM3EOA33-29-0011 R10 2014-08-25頁碼，17 / 22工卡 Job card:TITLEInspect the