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1、TGPE-M2910-SPRING AIRLINES 113 DETAILEDTGPE-M2910-SPRING AIRLINES 113 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND WARNING:OBEYTHEHYDRAULICSAFETY警告遵安全程WARNING:DONOTTOUCHTHEHYDRAULICSYSTEMCOMPONENTSFORASHORTTIMEAFTERTHEENGINE IS SHUTDOWN. THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN
2、 CAUSE CAUTION:DONOTLETHYDRAULICFLUIDFALLONTHEENGINE.UNWANTEDHYDRAULICFLUIDMUST BEREMOVEDIMMEDIA YWI CLEANL FREECLOTH.THEFLUIDCANCAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.警戒: 不要让 油从发 滴落。多余的 油必须马上用干净的不起毛的布清除。液压油会对保护层和一些 造成损伤。JobSet-up/Aircraftenance飞构Make suret the Green hydraulic syst
3、em is deprerized and put itenance configuration. (Ref. AMM TASK 29-00-00-864-001) .确定构型(参考AMMTASK29-00-00-864-Make suret the Yellow hydraulic system is deprerized and put itenance configuration. (Ref. AMM TASK 29-00-00-864-001)确定构型(参考AMMTASK29-00-00-864-rizethereservoirsoftheGreenandYellowhydraulics
4、ystems.(Ref. AMM TASK 29-14-00-614-001)给系统油箱释压(参考AMMTASK29-14-00-614-Put warning noti) inition tos not to prerizetheGreen hydraulic system:hecockpitonthehydraulicsection40VUoftheonthegroundservicepaneloftheGreenhydraulic系部分40VUPutwarning)itionsnottorizetheTGPE-M2910-SPRING AIRLINES 213 DETAILEDTGPE-
5、M2910-SPRING AIRLINES 213 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND hydraulichecockpitonthehydraulicsection40VUoftheonthegroundservicepaneloftheYellowhydraulic系部分40VUOntheedestal,ontheENGpanelputwarning)itionsnottostarttheMake suret the engine 1 (2) shutdown occurred not lessn5minutesbe
6、fore you do this procedure.在执行工作前,确定1号和2号已经停车5分钟以Ontheoverheadenancepanelmake surettheONlegendoftheENG/FADECGNDPWR/1(2)pushbutton switch is off.在头顶面板50VUENG/FADECGNDPWR/1 2ONPutwarning)itionsnottoenergizetheFADEC1激活FADEC1Open,safetyandtagthis(these)circuitHYDRAULIC/Y HYD/PUMP ENG2/MONGHYDRAULIC/YHYD
7、/PUMPHYDRAULIC/GHYD/PUMPHYDRAULIC/GHYD/PUMPYYHYD/ELEC/ELECGetTGPE-M2910-SPRING AIRLINES 313 DETAILED INSPECTION OF TGPE-M2910-SPRING AIRLINES 313 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND Opentheleftandrightfancowldoorsonleftandrightengine(Ref.AMMTASK 打开左发和右发的左右风扇整流罩(AMMTASK71-13-00-010
8、-Putthesplatformitionatthe在PutacontainerbelowtheenginetocollectunwantedProcedureNOTE:PERFORMEFOLLOWINGINSPECTIONONBOTH注在左右都要执行以下检Locatethehydraulicsuctionhose/tubeonleftsideoftheenginefan找到NOTE:During clinstallation ensurethose/tubeassemblyisproperlyaligned to prevent preload by tightening the bolts
9、 lightly during the initial installation. After ensuringtthereisnopreload,torquetheboltstotheir proper valuehis sequence (3, 4,2).注: 当安装Remove the bolt, the washer and the classemb stachthehydraulic suction hose /tube at the upper mid bracket.Remove the bolt, the nut, the two washers and the cltacht
10、he hydraulic suction hose/tube to the lower mid bracket. Remove the bolt, the washer, and the cltachthehydraulic suction hose/tube to the lower bracket.Inspecttheassemb sforanydamageor检左发 检查结果 采取措施:TGPE-M2910-SPRING AIRLINES 413 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND TGPE-M2910-SPRIN
11、G AIRLINES 413 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND 右发 检查结果 采取措施:Iftheassemb sshowanysignsofwearordamage,replacetheworn如Inspect the hydraulic suction hose/tube assembly at the clitions for chafing or damage. Refer to table # 1 for damage wear limits (umallowed damage depth is 10% o
12、f the wall thickness).左发 检查结果: 采取措施: 右发 检查结果 采取措施:FordamageassessmentofhosesectionarearefertoAMM,Chapter29-11-49 对于供油管损伤的评估,参考AMM29-11-If the damage is moren the allowable limits, replace the hydraulic prehose/tube assembly per AMM, Chapter 29-11-49.AMM29-11-49Install the classembly, the bolt and th
13、e washertach the hydraulic suctionhose/tubeassemblytotheuppermidbracket.Tightenthebolttoatorque of 30-35 lb-in. (3.4 - 3.9 N.m).(3.4-3.9左发 工具 右发工力矩值Install the classembly, the bolt, and the two washerstachthehydraulic suction hose/tube to the lower mid bracket. Tighten the bolt to a torque of 30-35
14、lb-in. (3.4 - 3.9 N.m).组件,螺钉和2个垫片安装到供油管上。力矩值:30-lb-in.(3.4-3.9左发工力矩值TGPE-M2910-SPRING AIRLINES 513 DETAILED INSPECTION OF HYDRAULICTGPE-M2910-SPRING AIRLINES 513 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND 右发工力矩值NOTE: Checktthecorrect(thin)washerNAS1149C0363Risinstalledatthis location. (L
15、ower Mid Bracket Suction Hose Tube)注: 检查安装在下中部支架上的垫片是正确(11)Install the classembly, the bolt and the washertach the hydraulic suctionhose/tubetothelowerbracket.Tightenthebolttoatorqueof30-35lb-in. (3.4 3.9 N.m). -3.9左发 工具 右发工力矩值Locate the hydraulic prereswitchhose/tubeassemblyonleftsideoftheengine fa
16、n case.找到管组NOTE: During clinstallation ensureto prevent preload by tightening the bolts lightly during the initial installation. After ensuringtthereisnopreload,torquetheboltstotheir propervaluehe following sequence: vertical clip注: 当安装Remove the bolt, the washer and the cltach the hydraulic preswit
17、ch hose/tube to the upper mid bracket on vertical side.Remove the nut, the washer (far side),the bolt, the washer and classembly(2 tach the hydraulic prere switch hose/tube to the upper mid bracket on horizontal side.垫片组件(2个位置Inspect the classemb s for any damage or wear at the clinglocation. (See F
18、igure 1 for classy arrangement).TGPE-M2910-SPRING AIRLINES 613 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND TGPE-M2910-SPRING AIRLINES 613 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND 检左发 检查结果: 采取措施: 右发 检查结果 采取措施:Iftheassemb sshowanysignsofwearordamage,replacetheworn如Inspect the
19、hydraulic hose/tube at the cllocationsforchafingorwear.No wear or damage is allowed.检左发 检查结果: 采取措施: 右发 检查结果 采取措施:FordamageassessmentofhosesectionarearefertoAMM,Chapter29-11-49 对管损伤的评估,参考AMM29-11-If the damage is moren the allowable limits, replace the hydraulic preswitch hose/tube assembly per AMM,
20、Chapter 29-11-49.如果损伤超过允许的值,根据AMM29-11-49更Install the cl, the bolt, and the washertach the hydraulic preswitchhose/tubetotheuppermidbracketonverticalside.Tightenthebolttoa torque of 30-35 lb-in. (3.4 - 3.9 N.m).30-35lb-in.(3.4-3.9左发 工具 右发工力矩值Install the classembly(2locations)thebolt,thewasher,thewas
21、her(farside) and the nuttach the hydraulic prere switch hose/tube to the upper mid bracket on horizontal side. Tighten the bolt to a torque of 30-35 lb-in. (3.4 - 3.9 管上。力矩值:30-35lb-in.(3.4-3.9TGPE-M2910-SPRING AIRLINES 713 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBETGPE-M2910-SPRING AIRLINES 713 DET
22、AILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND 左发 工具 右发工力矩值Locate the hydraulic prerehose/tubeassemblyonleftsideoftheenginefan 找到NOTE: During clinstallation ensureto prevent preload by tightening the bolts lightly during the initial installation.After ensuringtthereisnopreload,torquetheboltstot
23、heirpropervaluein this sequence (1, 2, 3, 4, 5).注:当安时,确认管组件正确对齐以防止初始安装时拧螺母产生的预紧力。确定没预紧力后,按图示顺序用正确的力拧到正确的数Remove the bolt, the washer and the classemb stachthehydraulic re hose/tube to the upper bracket.Remove the bolt, the washer and the classemb stachthehydraulic re hose/tube to the upper mid brack
24、et and engine fan case bracket( if installed ).压垫片Remove the bolt, the washer and the classemb stachthehydraulic re hose / tube to the lower mid and lower bracket.Inspect the classemb sforanydamageorwear.(Seefigure1forcl assy arrangement).检左发 检查结果: 采取措施: 右发 检查结果 采取措施:Iftheassemb sshowanysignsofwearo
25、rdamage,replacetheworn如TGPE-M2910-SPRING AIRLINES 813 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND TGPE-M2910-SPRING AIRLINES 813 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND Inspect the hydraulic hose/tube at the cllocationsforchafingorwear.Referto table #1 for damage wear limit
26、s (theum allowed damage depth is 10% of the wall thickness).左发 检查结果: 采取措施: 右发 检查结果 采取措施:FordamageassessmentofhosesectionarearefertoAMM,Chapter29-11-49 对 If the damage is moren the allowable limits, replace the hydraulic prehose/tube assembly per AMM, Chapter 29-11-49.如果损伤超过允许的值,根据AMM29-11-49更压力Insta
27、ll the cl assemb s, the bolt and the washertachthehydraulic pre rehose/tubeattheupperbracket.Tightenthebolttoatorqueof20-25 lb-in. (2.3 - 2.8 N.m). (2.3-2.8左发 工具 右发工力矩值Install the classemb s, the bolt and the washertachthehydraulic re hose/tube to the upper mid bracket and engine fan case bracket( i
28、f installed). Tighten the bolt to a torque of 30-35 lb-in. (3.4 - 3.9 N.m).压力管上。力矩值:30-35lb-in.(3.4-3.9左发 工具 右发工力矩值Install the classemb s, the bolt and the washertachthehydraulic re hose/tube at the lower mid and lower bracket. Tighten the bolt to a torque of 30-35 lb-in. (3.4 - 3.9 N.m).TGPE-M2910-
29、SPRING AIRLINES 913 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBSTGPE-M2910-SPRING AIRLINES 913 DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND 值:30-35 lb-in. (3.4 - 3.9 N.m)左发 工具 右发工力矩值Locatethehydraulictopcasedrainhose/tubeassemblyonleftsideoftheengine fan case.找到NOTE: During clinstall
30、ation ensureto prevent preload by tightening the bolts lightly during the initial installation. After ensuringproper value.注: 当安装Remove the bolt, the washer and the classemb s (3 locations)the hydraulic top case drain hose / tube.(3个位置Inspect the classemb sforanydamageorwear.(SeeFigure1forcl assy ar
31、rangement).检左发 检查结果: 采取措施: 右发 检查结果 采取措施:Iftheassemb sshowanysignsofwearordamage,replacetheworn如Inspect the hydraulic hose/tube at the cllocationsforchafingorwear.Referto table # 1 for damage wear limits (theum allowed damage depth is 10% of the wall thickness).检左发 检查结果 采取措施:TGPE-M2910-SPRING AIRLINE
32、S 1013DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND TGPE-M2910-SPRING AIRLINES 1013DETAILED INSPECTION OF HYDRAULIC HOSE/TUBE ASSEMBS AND 右发 检查结果 采取措施:FordamageassessmentofhosesectionarearefertoAMM,Chapter29-11-49 对管损伤的评估,参考AMM29-11-If the damage is morentheallowablelimits,replacethehydraulictopca
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