A320飛機(jī)所有接近電門(mén)簡(jiǎn)介無(wú)錫基地陸亦彬

1、.專(zhuān)業(yè)資料分享.WORD完美格式.A320飛機(jī)所有接近電門(mén)簡(jiǎn)介以B-6796為例37CV39CV左大翼38CV40CV flap-attachme nt failure detect ion sen sor37CV （ 581AT） 39CV （ 581AT ）襟翼內(nèi)連結(jié)構(gòu)上的襟翼連接失效探測(cè)傳感器右大翼上38CV （681AT ）40CV（681AT）NPC.2TS 10501 01eo90ATAMess&gsSourceClass*ON A/CALL27-51-15L FIZP DISC FROX SNSR (37CV)/LG CIU1 (5GA1)LGCIU 11 ON A/C ALL2

2、7-51-15L FLP DISC PROX SM SR37CVLGCIL111* ON A/C ALLZ27-51-15FLP LH PROXSNSR1 37CV MIS ADJUSTMENTSFCC12ON A/CALL黑27-51-15FLP LH PROX SNSR 1 37CV OR LGCltJ 1SFCC12ATAMessageSourceass UN A/C ALLS27-51-15R FLAP DISC PROX SNSR(38CVyLGClU I (5GA1)LGCIU 11 UN A/C ALL27-51-16R FLP DISC PROt； SNSR38CVLGCIU

3、11ON A/C ALL27-51-15FLP RHPftOX SNSR 1 38CV MISAJD JUSTMENTSFCC12_ ON A/C ALLX27-5M5FLP RHPROX SNSR 1 38CVORLQCIU1SFCC12ATAMessageSourceClas&* ON AC ALLX27-51-15L FLAP DISC PROX SNSR (39C0/LGau2(5GA2)LGCIU 21_ ON A?C ALLX27-51-15L FLP DISC PHOXSNSR 39CVLGCIU 21* ON A；C ALLX27-61-15FLP LM PROX SNSR2

4、39CVMISADJUSTM E MTsfcc?2J ON A；C ALLX27-51-15FLP LH PROX SNSR 2 39CVOR LGOU 2SFCC?2|ataMessageSourceassON A/C ALL27-51-15R FLAP D ISC FROX SNSR (4 OCVJ/LQ Cl U 2(5 GAZ)LGCIU 21* ON A/C ALL27*51-15R FLP DISC PROX SNSR TDCVLGCIU 21*ON A/CALL527-51-15FLP RH PROX SNSR 2 毗CV MISADJUSTMENTSFCC?2ON A/C AL

5、L27-51-15FLPRH PROX SNSR 2 DCVORLGCIU 2SFCC?2下面以37CV為例，其余類(lèi)似7-51-15 L FLAP DISC PROX SNSR (37CV)/LGCIU1 (GA1)LGCIU 1127-51-15L FLP DISC PR.OX SNSR 37CVLGCIU 11TASK 32-31-00-S10-62fl-ALeft Flap Disconnect Praximity SensorWARMILKS： MAKE SURE THAT THE GROUND SAFETT-LOCKS ARE IN POSITION ON THE LANDING G

6、EAR,訶職MING: PUT THE SAFETY DEVICES AMD THE WARMING NOTICES IN POSITION BEFORE YOU START A TASK OM OR HEAR:THE FLIGHT CONTROLSTHE FLIGHT CONTROL SURFACESTHE LANDING GEAR AND THE RELATED DOORS-COMPONENTS THAT MOVE.-LGCIU-1 ( 5GA1 I-LGCU-2 ( 5GA2 i SENSOR-L FLAP AUACHMErrT FAILURE DETECTION t 37CV I- S

7、ENSOR-L FLAP ATTACHMENT FAILURE DETECTION t 39CV )* aircran wiring2. J口野：5出山0 InformaiticiinA Referenced! InfurmananREFERENCEDESIGNATIONBef ASM 27-51-06Ref ASM 27-51-07AMM5/-61-15-DD0-C02MAM 27-51-1S40D-0D2Removsl of the Proxim rty-Sen?Of 5 crf thi Interconn-echng Strut Inslallah口n 口f the Proximity-

8、SenEors of Che Interconnecting StmtMAIA 32-31-71-000-001Removal of the LGCIUAP.1M 323 U1400-001hstallalion of the LGCIUAMM 3269-00740-001BITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is Operatic3 F 日ij 11二口門(mén)liirii ml.1 二門(mén)Subtask 32-31-00-740-068-AA.

9、 Test(1) Do a BITE test vvith the LGCIU (1 or 2 that is the source of the CFDS message AMM 32用(a) If the test gms a mMsagfl that includes DISC PROX SNSR do the fault isolation.NOTE If a fault occurs on lhe two proximrty senMrs of the same inteirconnecting stmt (the RH wing 38CV and 40 CV or the LH w

10、ng 37CV amd 39V|I a F/CTL FLAPS FAULT. ECAM WARNING is shown on top of the SFCS Maintenance Status when flaps are in confiiguraEion 1B 2 o01起落架控制和接組件(LGCIU)番用th所有32-31-01A條復(fù)期限安裝數(shù)量掛牌A21是(o)LGClU 2可且尖蝕懇罷飛廿個(gè)航段*但需；1) 所有的ELAG, SEC, SFCC. RA. FAG和ADIRSTiE常.H.2) 阿部空調(diào)工作正常*且3) 不泥使用FLEX起飛模式，H4) 電子設(shè)備在地面工作有時(shí)間限制

11、*號(hào)(o)鑫考操作程序323心入超落架控制和接口爼件(LGClU)SFCC127-51-15 FLP LH PROXSNSR1 37CV MISADJUSTMENTTASK 27-51-00-810-83 0-ASFCC 1 or 2 占hows a LH or RH Flap Attadimetit Proximity Sensor as a hh關(guān)djustAnont1 Pdible Cmuwm言-SENSOR.L FLAP AHACHMENT FA1 LURE DETECTION L37CV l- 5ENSOR-R FLAP ATTACHMENT FAILURL DLTt6ON t 3S

12、CV 1” SENSOR-L FLP ATTACHMENT FA1L URE DETECTION f 3乳甘 1- SENSOR-R FLAP ATTACHMEF-JT FAILURE DETECT1OPJ t JDCV )2 Job Swlup InTuEiRlicinA Referenced InfarmnlicinREFEREMCEDESIGNATION27-51-00-810-817-A27-51-00-B10-B21-ALeft Flap InEercannectingi-Strul: Attachment IFailure-Detectdon Sensor Fault Right

13、Flap Interconnecting-Strut Aitachmafil Failure-Detection Sensoir Fault32-31-00-81CI-B02-ALGClU FaultAMM 27-S1-00-710-002Operational Test ahh Flap Interconnecting Strut and the Flap-Attachment Failure-DetecE.ion SensorsAMM_27-5144-0DQ2Removal of the Proximity-Sensor of the Intfirconnecting StrutAMM 2

14、7-S144-4M-002Installation of the Proximity-Sensoir of t he Interc onnecting StrutAMM 31-32-00-3W-OMProcedure to Get Access lo the SYSTEM REPORT.TEST F?CTL Page3. FeuH Cum&rniEiicinSubtask 27-61-00-740-062-AA Test(1) Trouble sheet any LGOU faults L%f 1$皿衛(wèi)-31-00-朗00岔 before you continue this pfocedure

15、(2) Do ar operlional test of Iha failure deletion sensor for th? Hap attachment AKIhi 2丁-51-00-門(mén)0-0024 Fmult IsolmtioriSubtask 27-51-00-810-079-AA. Proc &d ura(1) If there i$ m proximity sensor mimmEju百iment failure(a) Refer to th 烏 MM 27-1圉-01)-00 and 占1Muse I he removal arrd inslallalion procedure

16、s tu do llie pfOximity sen5or adjuslmert(b Gat access to the SYSTEM REPORT/TEST AMM 茁 32 加朋0 Q竝(C Mke sure that the SYSTEM STATUS shows NO FAULTS(2) If the (dull continues(a) Amplaum the Eppl icblE pfwehs(j- SENSQR-L FLAP AJTACHMEMT FAILURE DTCTIOhl m :-SENSOR-R FUP ATTACHMENT FAILURE OETECHON i 36C

17、V 1- SENSOR-L FLOP ATTACHMENT FAILURE DETECTIOM 39CV )-SEMSOR-R FLAP ATTACHMENT FAILURE DETECTION U0CV 陽(yáng) M 2了-5144-000-002 and AM 閘 21屮加詢(xún)2(b) Reped the lest in Para 3 A (2) If the fault continues da the sppliabl& task for an invalid proximity sensor (Ref TSM 27-51-M-aiO-Bm Of (Ref. IBM 盯-51-00陽(yáng)0-821

18、1.(a Repeal the test in Para. 3.A.(2) and make sure that the SYSTEM STATUS shows MO FAULTS.5 CIq迪udSubtask 27-51-00-942-071-AA Remove tha ground support and mainienance equipment the special and standard tools and all other itemSubtask 27-5T-OO-06O-O72-AB Put the aircraft back to its initial configu

19、ration.SFCC127-51-15 FLP LH PR0XSNSR1 37CVOR LGCIU1TASK 27-51-00-810-817-ALeft Flap Interconn&cting-Strut Attachmenl Failur-D&laction Senior FauttNOTE: a huH occura on the lw& proximity a-emaors 37CV and 39V. s F/CTL FLAPS Fault EAW ns shown on |(he top of the SFCS msmlenanGe flatus wtien Flspa are

20、in cgnf 1.2 帖閘 27活肚00廠1(1002.(3) Ifthe tesl is OK(a) Rpta.ee the SLAT/FLAP COMTR COMP. (21CV) or SLAT/FLAP CONTR.COMP ( 22CV that was th& source oFthe iniEial CFDS meag(4 If the test is not OK (grves the same CFDS message 豳 the inrtiai CFDS m-essags):(a)盹陰盟 the applicable ipraximity sensor SENSORS F

21、LAP ATTACHMENT FAILURE DETECTION ( 37CV ) or SENSOR-L FLAP ATTACHMENT FAILURE DETECTION t 39CV ) AMM 22UD00皿 and AIM 2知15曲402(5) Ilf the fault c&ntiniues . do a 亡h &ck and repair nee的抽呼 aircraft wiring b&t&n-(he applicable proximily censor nd the related LGCIU. Ref AS忖 2了or Ref ASM 2了 W-the apphble

22、LGCIU and lhe related SFCC, BfiLASMJLfiUffi ar BaL ASM ZL51SL(a) Do the tost given in Para.(2).27-51-01SFCC襟翼通道堆用th JK#27-51-01A修復(fù)期限安裝數(shù)最旌行所需數(shù)晟掛牌C21是1SFCC 2襦輯迪逍可以先汝但要求:1) 解除工作且2) SFCC 1檢沓襟縫翼工作正常，衛(wèi)3) 毎次飛行前塗査SFCC1襟翼翼尖剎車(chē)(WTB)T作iE常，且4) l*r fiELAC, SECa LGCIU, RA, FAC 和 ADIRST作正軌 且5) 地面最小慢軍被認(rèn)為不工作.UELH 73-

23、2(05地廊雖水慢車(chē)聲龍何塞琴操作粹宇佔(zhàn)SHX律児通迫m)蓼 g AMM 27-51-00-040-001修豆期限安裝數(shù)帚放行所需歓試掛牌|C21是(o(m) SFCC 2淮譚通直可以天效也理求:1) 解除T-作，且2) 在SFCG1檢査樣継翼T作正常，且勒每次飛行前檢査SFCC 1雍翼軽賓剎車(chē)(WTB)工作正常，且4) ELACr SEC, LGC1U, RA, FAC 和 ADIRS工柞正常，且5) 不允押在CONF KF卜起屯.池何 奄錚掠作榕宇27-1-02A SFCC絃管砂趟(m)乜 了 AMM 27-51-00-040-005以上為飛控方面的14GA 15GA15GA左主起落架放下

24、鎖定接近電門(mén)（系統(tǒng)1）（ B-6796飛機(jī)上兩傳感器的標(biāo)簽貼錯(cuò)了！）14GA右主起落架放下鎖定接近電門(mén)（系統(tǒng)1）*ON A/CALL32-31 ?3RL/GDNLK PROX SNSR14 GALGCll 1-*0N A/C 002-002rfl-19, 051-099, 101-H9r 151-191 Z01-249, 251-299r 301-501 511-65 E5G-SOO|EMB SB 32-118? for A/C 002-002, 051-05232-31 ?3R L/G DNLK PROX SNSR 11RATGT POSLGCll 1-*ON A/CALL32-31 ?3R

25、 LG ONLK PROX S NSR (11GAM-G d U1 (5G A1)LGCll 1-* ON A/C ALL|SEt*32-31 73R LG DNLK PROX S NSR (11 GTCT POSLGCll 1-ATAMessageSourceassON A/CALL蠱32-31-73IL L/G DNLK PROX SNSR1 5 GALGOU11 ON A/C 002 00?. 004-09, 051-099 101-149, 151-199, 201-219, 251299, 301-509, 511-651 656-800|EMD SB 32-1 1 82 for A

26、/C 00? 002, 0132-31-?3L UG DNLK PROK SNSR15GA TGT POSLGOU11 ON A/CALL黑32-3173L LG DNLK PROX SNSRfl GAJ/LGCI U1(5GA1)LGCIU 11*ON A/CALLjSD *攔32-31-73L LG DNLK PROX SNSR (15GAJTGT POSLGCIU 11以14GA的第一條信息為例32-31-73 RIJG DNLK PROX SNSR14GALGCIU11TASK 32-31-00-810-822-ARLG Dowmlock Proximity Sensor FaultW

27、ARNING: MAKE SURE THAT THE GROUND SAFETY丄OCK5 ARE IN POSITION ON THE LANDING GEAR.VERMIN PUT THE SAFETY DEVICES AND THE WARMING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:-THE FLIGHT CONTROLS-THE FLIGHT CONTROL SURFACES-THE LANDING GEAR AND THE RELATED DOORS-COMPONENT S THAT MOVE.1 Rciss

28、iblE CmLises PROX SNSR-R LJG DNLK, SYS 1 ( WGA-PROX SNSR-R LJG DNLK, SYS 2 EGA- aircraft wiring-LGCIU-1 (5GA1 l-LGCIU-2 估GA2 12. Jdlj S業(yè)-lju Inform議ion3 Fwult Confirm at ionSubtask 32-31-00-74Q-0&2-AA Test：1 j Do a BITE test on the LGCIU 1 or LGCIU 2 AMM 32-69-00-耳口-。1. wtiich identified the R L G p

29、roximrty-sensorfauIt-if a R L/G DNLK PROX SNSR message is shown, do the fault isolation procedure in Para 4 A (2)i2) If a R L7G DNLK PROX SflSR message is shown on lhe Post Flight Report (PFR). do the fault is Dialion procedure in ParaNOT巳 The fault R UG DNLK PROX SNSR TGT POS cannot be identified b

30、y the BITE test. The BITE test can only confirm an open-circuit or short-circuit in lhe proKimity-sensor. or its related wing Target position faults car only be confirmed by continuous SITE during LG operation To confirnn a target position fault, it is necessary to do the proximrty-sens&r-ta(get ins

31、pection and the inductance check, given in the fault isolation procedureNOTE- For more information about LGCIU proximity sensor trouble shooting, referto SIL 32-Q674 Fault IwolmtionSubtask 32-31-00-010-0 73-AA Procedure：1 If the PFR shows 9 proximity-sens or target-position fault do the steps that f

32、ollow:(a) Do the inspection of the applicable pmximity-sensar PROX SNSR-R L/G DNLK. SYS 1 t 14GA) or PROX SNSR-R L7G DNLK. SYS 2 ( 16GAI. AMM J2-引(b Use an IMDUCTANCE METER 1KH2 to da a check nf the inductance of ths applicable praximity-sensor AMM 亞-31 了玄320哥関-1 If the fault continues, do the subse

33、quent stepi2) If Lhe BITE lest shows a proximity-sensor fault do lhe steps that follow.fa At the applicbl? proximity sen?Qi. release lh electrical uonnectJNlOTE If tha ELDEC proximity-senQr test unit is available go to page block 301 nd da lhe procdurs in Para 4(b) Use 3 f-IULTlfETER - STANDARD a Rd

34、 do a ch?ck of th? r&sistncE between the pinw A and B af lhe applicable prtJKimity，呂 mnE” Ref ASM 32-31-OS of Ref ASh1 32-J1-C4. The resistance must be.-11 to 13 ohms for a Fanite proximity sensor (PN 848401) -15 to 17 ohms for an a III mal proximity sensor (P/N 8-933-01)(c) Connect the pins A and B

35、 together:di Connect one test lead of the TESTER - INSULATION RESISTANCE to the pins AB and the other test lead lo the caseie) Supply a lest signal far 5 seconds and read lhe re&isiance value shown. Tte resistance value must be more than 400 Megohms.(f) From the re si stance checks in steps (b) and

36、(e).1 If the twc rsislance values are carrect da step (42 If one or mare jf the nesistance values is nut correct d口 the ubsaquenl step(3) Replace the applicable piBximity-sensor PROX SNSR-R L/G DNLK. SYS 1 14GAI or PROX SNSR-R L G DNLK. SYS 2 i 16GA 1 . Am 筑- 006口釘 and(a) If the fault comiinues da t

37、he subsequent step(4) Do a check and repair as necessa the aircraft wiring between the applicable proximity-sensor electncal connector and the related LGCIU ARINC tray 陽(yáng)f AM 3221P3 Dr RM ASM 32后1，04(fi) Do ths test m Para 3 A (1)田If the fault continues do the subsequent step阿 Replace the applicable

38、LGCIll-1 ( 5GA1 ) ar LGCIU-2 GA2 F AMM 號(hào)-3忖and 帥幗 32與1-4叩0加一 which identified the fault.(7) If MMEL condilicns apply to the PROX SNSR-R L-G DNLK. SYS 2 ( 16GA1ia) Do Lhe deactivation &F lhe proximily sensor AhILI6 CIom叩Subtask 323 V00-8 50 072 AA Put the aircraft bck to rts initial configuration16GA

39、 17GA 20GA 21GA 22GA 23GA回回SEE 32-1100 1 T 0回E250SEE 32-11SEE 32-1 1SEE 32-1 1-1 1-66SEE 32-1 116GA17GAE30SEE 32-1 1-1 1 -83245220 240SEE 32-11-11-52SEE 3 2-1 1-1 1-70LHSEE 3 2-11 J 1-75RK607 090 20GA ?1GAhl PC 321V1 22 C ai 0017GA左主起落架放下鎖定接近電門(mén)（系統(tǒng)2）16GA右主起落架放下鎖定接近電門(mén)（系統(tǒng)2）21GA左主起落架伸展接近電門(mén)（系統(tǒng)1）20GA右主起落架

40、伸展接近電門(mén)（系統(tǒng)1）23GA左主起落架伸展接近電門(mén)（系統(tǒng)2）22GA右主起落架伸展接近電門(mén)（系統(tǒng)2）ATAMessageSourceassn ON A/C ALL232-31-73R UG DNLK PROX SNSR 1 6GALGCIU 21 ON A/C D02-003. 004-049. ft51-0Sl 101-H9,201-M9. 251-2S9, 301-509. 511-654 656-B00|EMB SB 32-11fl2 for A/C 002-002, 0X32-31-73R 典 DNLK PROX SNSR 1 SGA TGT PO SLGCIU 21* ON A/C

41、 ALL232-31-73R LG ONLK PROX SNSRC1 BGALGC1U2(5GA2)LGCIU 21n ON A/C ALLJSD *32-31-73RLGD NLK PROX SNSRfl 6GA)TGT PCSLGCIU：1ATAMessageSourceClass-ON A；C ALLX32-31-73L UG DNLK. PROX SNSR 17GALGaU21* ON A/C 002-002, 00 09. 051-099, 1 01-1 49. 1 51-199. 201-249. 251 -299, 301-509, 611-651 65G-800|EMR SB

42、32-11 02 for A/C 002-002. 0?32-31-73L UG DNLK PROX SNSR 17GA TGT POSLGOU21J ON A；CALL32-31-73_ LG DNLKPROX SNSR (17GA)/LGaU2(5GA2!)LGQU 21J ON A/C ALL|SB *232-31-73L LG DNLKPROX SNSR (17GA)TGT POSLGCIU 21ATAMessageSourceClassj ON A/C ALL|SB *32-31-73RUG EXT PROX SNSR 20GALGCIU 11ON A/C 002-002. 001-

43、049. 051 D99” 101 H9, 151 199, 2D1-29, 251-?99, 301-501 511 654, 55G 800|EMB SB 32 1182 lor A/C 002 002, DA32-31-73RUG EXT PROK SNSR 20GA TGT POSLGCIU 11t ON A/C ALL|SB *32-31-73R LG EXT PROX SNSR (20GAVLGCIU1(5GA1)LGCIU 11*ON A/C ALLJSB *232-31-73R LG EXT PROX SNSR (2QGA)TGT POSLGCIU 11| ATAMessage

44、SourceClass* ON A/C ALL|SD *32-31-73L L/G EXT PROXSNSR21 GALGCIU 11ON A/C U02-002, 004-049, 051-099. 101-H9,151-193, 201-2-13. 251-m 301-501 511-654, 656-80D|EMB SB 32-1182 for A/C 002-002； 0A3231-73L LJG EXT PROXS 忖ER 21 GA TGT POSLGCIU 11* ON AJC ALL|SB *X32-31-73L LG EXT PROX SNSR 0GA“LGCIU1(5G的LGCIU 11n ON A/C ALL|SB *熬32-31-73L LG EXT PROX SNSR(21GA)TGT POSLGCIU 11JATAMessageSourceClass ON A/C ALL|SB *32-31-73RUG EXT PROKSNSR 22GALGCIU 21*ON A/C OOZ-002, 004-049, 051-099. 101-M9. 151-199, 201-2-13, 251-299, 3U1-509, 51 1-B54r 6