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SEQ NO/序列號 TitleInspect the Leakage of Hydraulic SystemMcd&Rev/廠家工卡&修訂日期標題檢查飛機液壓系統(tǒng)滲漏A/C/飛機號/組別EO JC No./EO 工卡EO JC Rev/工卡版本Workarea/工作區(qū)域Skill/工種Man Hour/工時 EOA33-29-0011 R10機身/AirframeAIR

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

3、對多發(fā)滲漏部件進行 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.運行中收到液壓系統(tǒng)發(fā)生漏油報告較多，故下發(fā) EO 進行定期對多發(fā)滲漏部件進行 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：新飛機引進，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：新飛機引進，增加 B-L NL 和 B-LNW 適用性,修改了計劃信息。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：新飛機引進，增加 B-LNM 適用性,修改了計劃信息。Reason for R 04: revise applicability to add new aircrafts B-LNM and amend PLAN inf ormation.R05 改版原因：新飛機引進，增加 B-LNN 適用性,修改了計劃信 息。Reason for R05

6、: revise applicability to add new aircrafts B-LNN andamend PLAN information.R06 改版原因：新飛機引進，增加 B-LNO 適用性,修改了計劃信息。Reason for R06: revise applicability to add new aircrafts B-LNO andamend PLA N information.R07 改版原因：新飛機引進，增加 B-LNP 適用性,修改 了計劃信息。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：新飛機引進，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EOA33-29-0011 R10 2014-08-25頁碼，3 / 22198F32104013000SAFETY COLLAR-DOORMLGTO2ALLALLTOOLS 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、序號欄指需要定期執(zhí)行維修工作的部件。對于要求更換拆下返廠工作的部件，該欄指拆下件、序號信息。完成工作后裝上件號和序號欄請?zhí)顚懴嚓P裝機件信息；對于在位執(zhí)行工作的（如稱重、測試等），該欄指在位工作部件件、序號信息，完成工作后裝上件號和序號請用斜線畫去。PN/件號

14、SN/序號ATA/章節(jié)ZONE/區(qū)域FIN/代碼LOCATION/裝機位置EOA33-29-0011 R10 2014-08-25頁碼，4 / 22PN-IN裝上件號SN-IN裝上序號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標題檢查飛機液壓

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安裝好，這將確保起落架不會意外收起。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)工作會比

19、較危險。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)域工作時確保安全防護和警告標識已經準備

20、好：-飛控系統(tǒng)-飛控表面-起落架和相關的艙門-可移動的部件這些部件作動可能傷害到人A. Preparation/準備1. Make sure that the Aircraft Electrical Circuits are energized (Ref. AMM TASK 24-41-00-861-801) .確保飛機電源已接好（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、黃液壓系統(tǒng)已經釋壓并處于維護構型（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器安全防護裝置（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標題檢查飛機液壓系統(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 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 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標題檢查飛機液壓系統(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 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 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標題檢查飛機液壓系統(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 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，黃系統(tǒng)儲壓器(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 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 目視檢查藍系統(tǒng)剎車儲

41、壓器（FIN 5426GG , 5427GG ）及相關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 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標題檢查飛機液壓系統(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 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 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1. Make sure that the access panel 195CB, 195DB are installed確認接近蓋板 195CB、195DB 已經安裝。2. Put the aircraft back to its usual configration.恢復飛機到正常狀

46、態(tài)。EOA33-29-0011 R10 2014-08-25頁碼，10 / 22工卡 Job card:TITLEInspect the Leakage of Hydraulic SystemPerfInsp標題檢查飛機液壓系統(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標題檢查飛機液壓系統(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標題檢查飛機液壓系統(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標題檢查飛機液壓系統(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標題檢查飛機液壓系統(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標題檢查飛機液壓系統(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標題檢查飛機液壓系統(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