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单击此处编辑母版标题样式,单击此处编辑母版文本样式,第二级,第三级,第四级,第五级,深航机务培训中心,仅供培训使用,深航机务培训中心,FLB,中英文填写,FLB,中英文填写,制作人,：郑得如,审核人：杨 硕,课件版权归深航机务培训中心所有,Problems,？,Yes,！,句式,动词,+,名词,: remove XXX labels.,动词,update,lost,XXX of XXX,从属关系,专业术语,auto pressurization system,L/I main,wheel,句式总结,summary,一、检查发现,/,机组报告,XXX,故障,(,不正常状态,),1,、航后检查发现起飞灯不亮,AF FIND AND CHECK TAKE OFF LIGHT INOP,Answer,：,A,F CHECK FOUND THAT THE TAKEOFF LIGHT WAS NOT ON.,2,、航后机组反映前客舱配平空气活门故障。,Answer,：,AF THE CREW REPORTED/ REFLECTED THAT THE TRIM AIR VALVE OF THE FWD CABIN FAILED.,航前检查：,preflight/ PF check,过站检查：,transit/ TA check,航后检查：,after flight/AF check,发现：,f,oun,d that,（一般用过去时态）,机组报告：,t,he crew reported/reflected thatXXX,故障：,XXX,failed/,wa,s inop/had fault,s,.,Useful Expressions,3,、航后检查发现右内主轮磨损超出标准。,AF CHECKED AND FOUND RIGHT INSIDE MAIN WHEEL WORN OUT OF LIMIT.,Answer,：,AF CHECK FOUND THAT THE RIGHT INBOARD/ INSIDE,（,R/I,）,MAIN WHEEL WAS WORN OUT OF LIMITS.,4,、过站检查发现右前轮磨损超标。,Answer,：,TRANSIT/TA CHECK FOUND THAT THE RIGHT NOSE WHEEL WAS WORN OUT OF LIMITS.,5,、航后检查发现右外主轮扎伤超出标准。,AF FOUND R/O MLG WHEEL,WORN,OUT OF LIMIT.,Answer,：,AF CHECK FOUND THAT THE R/O,MAIN WHEEL,WAS CUT/PUNCTURED OUT,OF LIMITS.,磨损：,be worn (wear,过去分词,),扎破：,be punctured,割伤：,be cut,超出标准：,out of limits,左前轮：,left nose wheel,左外侧主轮：,L/O (left outboard/outside) main wheel,右内侧主轮：,R/I (right inboard/inside) main wheel,轮胎的故障描述,二、参考,/,按,.,更换（件）,，检查,/,测试正常,1,、航后参考,AMM32-45-21,更换左前轮，检查正常，轮压,204PSI,温度,28,度,A,F REF AMM32-45-21 REPLEACED LEFT FWD WHEEL, CHECK OK. PRESSURE IS 204 PSI, TEMP IS 28 DEGREE.,Answer,：,AF REF. AMM 32-45-21, REPLACED THE,LEFT NOSE WHEEL, CHECK OK. THE TIRE PRESSURE WAS 204 PSI, TEMPERATURE WAS 28 DEGREES.,2,、航后检查发现,23DEF,行李架锁扣损坏,更换锁扣，检查正常。,AF CHECK FOUND 23DEF BUGGAGE LATCH BROKEN.,AF REPLACE LATCH,CHECK OK.,Answer,：,AF CHECK FOUND THAT 23DEF,LUGGAGE RACK/STOWAGE BIN,LATCH,WAS DAMAGED/ BROKEN. REPLACED THE LATCH, CHECK OK.,3,、参照,AMM29-11-11,更换右发动机液压驱动泵，测试无渗漏。,Answer,：,REF. AMM 29-11-11, REPLACED THE RIGHT ENGINE HYDRAULIC DRIVEN PUMP , PERFORMED A TEST AND NO LEAKAGE./TESTED AND NO LEAKAGE.,参考,/,按,.,更换（件）,，检查,/,测试正常,Refer to/,Ref. .,，,replaced .Check / Test OK.,Useful Expressions,三、检查发现,故障，按,号,/,类别保留，,同意放行,1,、过站检查发现后客舱热空气配平活门失效，因时间原因，依据,MEL21-63-02B,保留后客舱热空气配平活门，放行飞机。,TA CHECK AFT TRIM VALVE INOP, FOR SD,REF MEL21-63-02B KEEP THE VALVE,DISPATCH THE A/C.,Answer,：,TA CHECK FOUND THAT THE AFT CABIN HOT,AIR TRIM VALVE FAILED/WAS INOP.,FOR SD, REF.,MEL 21-63-02B,DEFERRED,THE HOT AIR TRIM VALVE,AND RELEASED THE AIRCRAFT.,2,、航后,FLB,反映左侧跑道转弯灯不工作，航材原因，参考,MEL33-40-05A,办保留,C,类，贴不工作标签。,AF FLB report L RWY turnoff light INOP, for SL reason, ref MEL33-40-05A，make DD，C item, tape INOP,Answer,：,AF FLB REPORTED THAT THE L RWY TURNOFF,LIGHT WAS INOP.,FOR SL, REFER TO MEL33-40-05A,DEFERRED THE FAULT AS CATEGORY C,AFFIXED/,TAGGED/PLACED A INOP PLACARD,.,3,、过站依据,TSM23-28-01-810-803,，判断天线有故障,因时间原因办理卫星通讯系统保留,.,Answer,：,TRANSIT/TA REFER TO TSM23-28-01-810-803, CONFIRMED THAT ANTENNA HAD FAULTS. FOR SD, DEFERRED THE SATCOM SYSTEM.,故障保留单,DD,：,deferred defect card,故障单,FC,：,fault card,办保留：,defer the fault establish/make a deferred card,办,X,类保留：,defer the fault as category X,办,XX,类保留单：,make a category XX deferred card,办保留,放行飞机：,dispatch/release the aircraft,航材原因：,For SL/Because of no spares,时间原因：,For SD/For time reason,贴不工作标签：,affix/tag/place a INOP placard,办保留,4,、第三观察员座椅左侧扶手在座椅收回后，无法固定在收上位置，因航材无件临时固定在收上位，座椅可以使用。,T,he third observer seat left armrest can not retract automaticlly after stow the seat, fixed it in retraction because of no spare.,THE LEFT ARMREST OF THIRD OBSERVER SEAT,COULD NOT BE FIXED IN STOWED POSITION,WHEN,RETRACTED THE SEAT. FOR SL,FIXED THE ARMREST,IN STOWED POSITION,TEMPORARILY,AND THE SEAT,CAN BE USED.,5,、过站驾驶舱门锁电门无法弹回自动位。时间原因，参考,MEL52-17,，保留自动锁系统，执行,M,项，有,O,项，放行飞机。,TA THE FLT DOOR SWITCH CAN NOT BACK TO AUTO POSITION,。,FOR TIME LIMIT,，,REF MEL52-17,，,DEFER THE DEFECT OF THE COOKPIT DOOR AUTOLOCK SYSTEM,，,EXECUTE THE M ITEM,，,HAVE O ITEM,，,DISPATCH THE AIRPLANE,Answer,：,TA THE COCKPIT DOOR LOCKING SWITCH,COULD NOT,BACK TO AUTO POSITION,. FOR SD, REF.,MEL52-17, DEFERRED THE AUTO LOCKING SYSTEM,EXECUTED THE M ITEM, HAD O ITEM, DISPATCHED THE,AIRCRAFT.,弹回自动位：,back to auto position,在收上位：,in stowed position,在正常位：,in position,复位：,reset,保持：,stay,固定：,be fixed,Useful Expressions,1,、航后根据,AMM73-21-10,更换右发,HMU,，测试故障代码,73-10342,消失，撤保留单,DE619865,.,Answer,：,AF REFER TO AMM73-21-10 REPLACED THE RIGHT ENGINE HMU, PERFORMED A TEST AND THE FAULT CODE 73-10342 DISAPPEARED, WITHDREW/,RESCINDED/CLOSED THE DEFERRED CARD, DE619865.,四、按,XX,更换,XX,，测试正常，撤消,/,关闭保留,2,、航后依据,A,MM23-,20-00,，更换前服务话筒，并完成功能测试,结果正常，,撤消保留单,DE789983,。,Answer,：,AF REFER TO AMM23-20-00 REPLACED THE FWD ATTENDANT HANDSET, ACCOMPLISHED/ COMPLETED A FUNCTIONAL TEST AND THE RESULT WAS OK,RESCINDED/CLOSED THE DEFERRED CARD, DE789983.,故障代码：,fault code,撤保留单：,rescind/close/withdraw the deferred card,功能测试：,functional test,完成：,accomplish/complete,执行、操作：,execute/perform/do,Useful Expressions,五、为判断,故障，对,进行串件,1,、,B,6566,飞机航后有“,PHC 6DA1”,的故障信息。为判断故障，依据,AMM30-31-34,，将,B,6566 PHC1,与,B,6570 PHC3,对串，测试正常，串件挂签号：,A0000781,。,TO B6566 PFR HAS PHC 6DA1FAULT MESSAGE. AF FOR JUDGE FAULT,REF AMM30-31-34 B6566 PHC1 EXCHANGE WITH B6570 PHC3,TEST OK ,TAG NO: A0000781.,Answer,：,AF A/C B6566 HAD A FAULT MESSAGE “PHC,6DA1”. TO CONFIRM THE FAULT/FOR FAULT,CONFIRMATION, REF. AMM 30-31-34,EXCHANGED,THE PHC1 OF B6566 WITH PHC3 OF B6570, TEST OK.,TAG NO,: A0000781.,2,、为判断,B-2652,自动刹车故障，根据,AMMXX-XX-XX,将,P2-2,面板与,B-2650,的,P2-2,面板对串，并完成系统功能测试，结果正常。,Answer,：,TO CONFIRM THE FAULT OF A/C B-2652 AUTO BRAKE SYSTEM,REFER TO AMM XX-XX-XX, EXCHANGED THE P2-2 PANEL WITH THAT OF A/C B-2650,. EXECUTED,A SYSTEM FUNCTIONAL TEST,AND,THE RESULT WAS OK.,3,、参考,AMM23-12-00,测试,VHF 3,工作正常。参考,AMM46-21-00,测试,ATIMS,正常。为判断故障，本机,VHF2,与,VHF3,对串，检查测试正常。,Answer,：,REF. AMM23-12-00, TESTED VHF 3 AND IT WORKED OK. REF. AMM46-21-00, TESTED ATIMS AND IT WAS NORMAL. FOR FAULT CONFIRMATION, INTERCHANGED VHF2 WITH VHF3. CHECK AND TEST OK.,为判断故障：,to confirm the fault for fault confirmation,串件（同机）,interchangewith,串件（不同机间）,exchange/swapwith ,挂签号：,tag NO./number,判断故障,1,、航后测试,EEC,，有代码：,73-31371,。航后依据,FIM73-11 TASK 801,测量,S1,，,S2,，,S3,，,S4,电阻值正常，,J9,，,J10,导通性和绝缘性正常，清洁插头，做,EEC,测试无代码。,AF TEST EEC , HAVE CODE:73-31371.AF REF FIM73-11 TASK 801 MEASURE RESISTANCE OF S1,，,S2,，,S3,，,S4 NORMALAND CHECK J9,，,J10 NORMAL,。,CLEAN THE RECEPTACLES,，,DO EEC TEST NORMAL,。,Answer,：,AF TESTED EEC, HAD CODE:73-31371. AF REF.,FIM73-11TASK 801,MEASURED THE RESISTANCE,OF S1,S2, S3, S4, THE RESULTS WERE NORMAL. THE,CONTINUITY,AND,INSULATION,OF J9 AND J10 WERE OK.,CLEANED THE CONNECTOR, TESTED EEC AND HAD NO,CODE.,六、测量,XX,与,XX,之间的电阻,/,电压,2,、航前检查发现副驾侧侧杆无线电选择器（,PTT,）不工作，航后依据,ASM23-51-03,，按压副驾侧,PTT,电门，,1RN,钉,12J,，,12K,（,AA),间阻值为,1.5,欧姆，松开,PTT,电门，电阻大于,20M,欧姆，根据,AMM23-51-34,，更换,AMU,。测试正常。,PF CHECK AND FOUND F/O PTT,。,AF REF ASM23-51-03,PUSH F/O PTT SWITCH,THE RESISANCE BETWEEN 12J AND12K(10N AA)IS 1.5, .,RELEASE THE PTT SWITCH ,THE RESISTANCE MORE THAN 20M,REF AMM23-51-34,REPLACE AMU,TEST,Answer,：,AF CHECK FOUND F/O PTT WAS INOP. AF REF.,ASM23-51-03, PRESSED THE PTT SWITCH,THE,RESISTANCE BETWEEN 1RN PIN 12J AND 12K,WAS 1.5,OHMS. RELEASED THE PTT SWITCH, THE RESISTANCE,WAS,MORE THAN,20 OHMS. REF.AMM23-51-34, REPLACED,AMU. TEST OK.,3,、航后检查发现,1,号,DME,天线前缘有刻痕。航后依据,AMM34-51-11,更换,1,号,DME,天线，测量天线与机身电阻为,1.200,毫欧，在标准范围内（标准为小于,5,毫欧），测试正常,.,AF CHECK AND FOUND THE DME1 ANTENNA LEADIN EDGE HAVE NOTCHING.REF AMM34-51-11REPLACED THE NO.1 ANTENNA,MEASURE THE BONDING RESISTANCE BETWEEN THE ANTENNA AND FUSELAGE IS 1.2m,，,IN STANDARD,(STANDARD ISNOT HIGER THAN 5MILLIOHMS),TEST OK.,Answer,：,AF CHECK FOUND LEADING EDGE OF DME1,ANTENNA HAD SCOTCH/NOTCHING. AF REF. AMM34-51,-11 REPLACED DME1 ANTENNA. MEASURED THE,RESISTANCE BETWEEN ANTENNA AND FUSELAGE. THE,RESULT WAS 1.2m,AND,WITHIN THE LIMITS,（,THE,STANDARD IS LESS THAN 5 m,）, TEST OK.,4,、航后检查发现真空泵线路,32,MG,到,36,MG,之间,A2,到,L1,断路，,L1,点无电压,AF CHECK THE VACUUM A2 TO L1 OF 32MG TO 36MG OPEN，L1 POINT NO VOLTAGE,Answer,：,AF,CHECK FOUND THE VACUUM PUMP,WIRING BETWEEN,A2,TO,L1,OF 32,MG TO 36MG,WAS,OPEN,CIRCUIT/HAD NO CONTINUITY,. L1 HAD,NO VOLTAGE,.,5,、航后,PFR,有故障信息,VACU GEN SUPPLY（383100），,依据,TSM38-31-00-810-840,测量跳开关,33,MG,至接线块,7205,VT,电压,正常，线路正常,，接线块,7205,VT,到继电器,36,MG L1,接头电阻无穷大，电压,45,V，,时间原因，保留故障。,AF PFR FAULT MESSAGE“VACU GEN SUPPLY”，REF TSM38-31-00-810-840 CHECK C/B 33MG TO7205VT WIRE OK，7205VT TO 36MG L1 OPEN，FOR SD，DEFER IT,Answer,：,AF PFR HAD FAULT MESSAGE “VACU GEN SUPPLY”.,REF. TSM38-31-810-840 MEASURED THE,VOLTAGE,BETWEEN,C/B,33MG AND TERMINAL BLOCK 7205VT, IT WAS OK.,CHECKED THE WIRING AND IT WAS OK,. THE RESISTANCE,BETWEEN TERMINAL BLOCK 7205VT AND RELAY 36MG L1,WAS,INFINITE, THE VOLTAGE WAS 45V. FOR SD, DEFERRED,THE FAULT.,万用表,multimeter,兆欧表,megger,电压,voltage,电阻,resistance,插头,connector,插座,receptacle/socket,线路,wiring,线束,bundle/wire harness,继电器,relay,跳开关,circuit breaker (C/B),导通性,continuity,绝缘性,insulation,插钉,pin,测量,measure,Useful Expressions,A,和,B,之间的电阻为,XX,：,The resistance between A and B was XX.A,和,B,之间的电阻大于,/,小于,XX,：,The resistance between A and B was more than/ less than XX. A,和,B,之间电阻无穷大：,The resistance between A and B was infinite.,测量电阻,检查,/,修理,A,和,B,之间的线路：,Check/Repair the wiring between A and B.A,和,B,之间线路正常：,The wiring between A and B was OK.A,到,B,断路：,The wiring between A and B was open circuit/ had no continuity.,短路：,short circuit,测量线路,总结,检查发现,/,机组报告,XXX,故障,(,不正常状态,),参考,/,按,.,更换（件）,，检查,/,测试正常,检查发现,故障，按,号,/,类别保留，同意放行,按,XX,更换,XX,，测试正常，撤消,/,关闭保留,为判断,故障，对,进行串件,测量,XX,与,XX,之间的电阻,/,电压,深 航 维 修 你 来 传 承,Groove Crack,Rib Undercut,Tread Damage,Puncture,Bulge,Blister,Tread/Sidewall Separation,Open Tread Splice,Tread Rudder Reversion,Chevron Cut,Peeled Rib,Thrown Tread,Tread Flaking and Chipping,Tread Chunking,1,、航后检查发现前客舱配平空气活门在,ECAM,上指示为“,XX”.,依据,TSM21-63-00-810-803，AMM21-63-51，,更换前客舱配平空气活门,(12HK).,做温度控制测试正常，引气测试无渗漏，检查正常。,AF check and found FWD cabin trim air valve on ECAM indicate xx, ref TSM 21-63-00-810-803，AMM 21-63-51，replaced Fwd cabin trim air valve, temp control test OK, bleed test no leakage, check OK.,AF check found that the trim air valve of FWD cabin,indicated “XX” on ECAM. Ref. TSM 21-63-00-810-803,and AMM 21-63-51, replaced the valve(12HK).,Performed a temperature control test and test OK, did,a bleed air test and no leakage. Check OK.,2,、前货舱门作动筒,2,处搭接带断裂，参照,AMM20-28-00,更换搭接带，参照,AMM20-28-00-869-002,检查电阻,TWO LEADING-BONDINGS WERE DANGERDE OF FWD CARGO DOOR,。,Ref AMM20-28-00REPLACE THE lead-bonding,。,REF AMM20-28-00-869-002 Make sure that the ohmic resistance is correct,。,TWO BONDING LEADS OF FWD CARGO DOOR,ACTUATOR WERE BROKEN/DAMAGED. REFER TO,AMM20-28-00, REPLACED THE BONDING LEAD, REF.,AMM20-28-00-869-002 MEASURED THE RESISTANE.,六、测量,XX,与,XX,之间的电阻,1,、航后,EEC,自测有代码,73-30351,。航后依据,FIM73-25TASK804,测量电阻正常，清洁插头，作动筒测试正常。,AF EEC TEST HAVE MESSAGE: 73-30351. AF REF. FIM73-25TASK804 EXAMINE THE RESISTANCE NORM,CLEAR CONNECTOR SACT TEST OK,。,AF EEC BITE TEST HAD CODE 73-30351. AF REFER,TO FIM73-25 TASK804, MEASURED THE RESISTANCE,AND THE RESUTL WAS OK. CLEANED THE PLUG,PERFORMED A TEST OF ACTUATOR AND THE RESULT,WAS OK.,Plug-,改为,connector,电插头,CONNETOR,分为两类,PLUG(,插头,),和,CECEPTACLE(,插座,).,插座靠近电源端，有安装支座，一般线号为,D*J,，插头靠近接地端，无安装支座，一般线号为,D*P,。,
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