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1、TSM手册介绍该介绍以空客A300排故手册为例。1. 概述飞机排故手册（TSM）是用于飞机系统的故障隔离。它为工作者提供了一种快速 准确判断飞机在空中或地面时出现的故障的系统或部件。在排故手册里没有提供详细的修正工作和修理，对于飞机的标准施工可参考飞 机维护手册20章，对于飞机电气线路和部件的标准施工可参考ESPM20章。飞机排故手册（TSM）是按照ATA 100规范编制的。2. 手册的使用飞机排故手册（TSM）是按照ATA 100规范划分系统，系统是按照功能进行划分。进入的方法如下：-对于22, 27, 31和34章（带有故障隔离图的章节）目录1故障隔离对于其它系统目录1故障现象1故障隔离我
2、们使用一个例子来讲解手册的使用。1 故障现象和故障隔离页的使用例如：A Pack Temperature Control Problem情况：-R ECAM DISPLAY UNIT (AIR BLEED page selected)-Pack 1(2) MODE SEL P/BSW released (out)“MAN” legend ON-With MAN CTL SW in HOT or COLD POSN do turb inlet and pack disch. TEMP return to normal?TABLE OF CONTENTS(TOC)ALL CHAPTERS WITH
3、FAULT SYMPTOMS ANDFAULT ISOLATION(SINGLE PAGE)CHAPTERS Z乙 27z 31AND 34WITH SCHEMATICS(OVERSIZE PAGE)FAULT SYMPTOMSFAULT ISOLATION(SCHEMATICS)COMPONENTLOCATION FAULT SYMPTOMS ANDRESULTS ON AIRCRAFT ACTIONS TO BE TAKENFAULT ISOLATIONCOMPONENT BITE TESTLOCATION REMOVAL/INSTALLATION (REF. AMM) REMOVAL/I
4、NSTALLATION (REF. AMM) WIRING (REF. A)一 WIRING (REF. AWM) X-REF. TO OTHER TSM CHAPTERS首先，进入21章空调目录页（参考图2）。在目录页里可以找到标题PackTemperature Control。在目录页的 ATA章节参考（ATA REF）栏里，Pack Temperature Control 对应于21-61，这是一个故障现象页（参考图3）。在这页上，正常的操作被一条水平线指向“NORMAL”。故障现象提示如下:! WITH PACK 1(2) MODE SEL !；P/BSW RELEASED (OUT)
5、!| (MAN* LEGEND ON), DO TURB ! ；INLET AND PACK DISCHI；TEMPERATURES RETURNTO；NORMAL (MAN CTLSUINHOT!OR COLD POSN) ?；八 YE$L 21 61 00;7厂 FIG. 102ljp 2161 DO!IFIG. 103根据故障现象作出的回答“YES”或“NO”，指导工作者的故障隔离的方法在页 的左边。(参考图4, 5)相应的故障隔离程序将被完成。(1) 故障现象故障现象(FS)程序是确定一个故障的中间步骤。每一个FS页对应于给定 系统中的几种故障类型的回顾。例如：Pack Tempera
6、ture Control-Fault Symptoms.一个FS页包含有水平和垂直线，在FS页的顶部包含了需要考虑的相关系 统设备的注释。(电门/开关位置，选钮电门，指示灯的情况，来自于ECAM 显示组件的数据，等等)。每一行根据技术上的详细情况，通常都带有一 个询问，根据回答的情况“YES”或“ NO”，工作者执行下一步排故程序或 直接进入相应故障隔离的交叉参考图。有时，“YES”或“NO”可以被描述情况的文字替代。例如：/ OUT注：-故障现象(FS)页正常是显示在一页。但有时根据故障隔离顺序的编号， 故障现象页可能被分为两页。-在一页里，各种线指示了根据故障现象需要参考的其他页，对于两个
7、相 近的页，先决条件在每页的上部被重复显示。正常的操作也被框出来。-一些章节的故障现象直接交叉参考到故障隔离页，这些带有星号的页块 关联相应的故障隔离的ATA参考图号。(参考图6, 7)(2) 先决条件在FS页的上部，先决条件指出了排故开始时的飞机构型以及必须要闭合的 跳开关。例如：EXTERNAL ELECTRICAL POWER (AMM 24-41-00, P. BLOCK 301).N/A IF REFUELING ON A/C BATTERIESC/Bs IN: 321/P56 thru 321/P61(3) 故障隔离故障现象的交叉参考引导到故障隔离页。例如：23-31-00 Fig
8、. 109.每页的顶部都包含有要求的先决条件，按照数字页块的形式进行编排，并 按照排故的逻辑顺序进行定位。FS文字内容的开始对应于故障现象栏。需要执行的工作和引起故障的原因在页的左侧部分，在页的右侧是需要执 行的工作(例如更换等)。拆卸/安装程序参考AMM,线路修理参考参考AWM和ESPM。在没有特殊要 求时，线路检查包括连续性和绝缘性检查。TITLEATA REFLATERAL PANEL - MFA READ TEST21-00FLOW CONTROL ANO INDICATING21*11FLIGHT COMPARTMENT ANO ELECTRONICS RACKS AIR CISTR
9、IBUTION. ELECTRONICS RACKS AIR EXTRACTION21-20CABIN pressure control and monitoring (MAIHTENANCE TESTS)21-30-00CABJN oepressuhization valve21-31CAfiltt PRESSURE COHTROL AND MONITORING21-31EMERGENCY RAM AIR INLET21-53AFU AMD PACK TEMPERATURE DEMAND CONTROLLER (BITE PROCEDURE)21-60-00PACK TEMPERATURE
10、CONTROLj1-61 LTRIM AIR CONTROL AND OVERHEAT MONITORIHG21-62FLIGHT COMPAfiTMENT ANO CABIN TEMPERATURE CONTROL21-63CARGO COMPARTMENT TEMP CONTROL (BULK CARGO COMPT)21-64CARGO COMPARTMENT TEMP CONTROL (FUD CARGO CWT)21-64i/X-REF TO FAULTAIR CONCITIONING - CONTENTSLS21GD0DOAO1QQ2-OOI EFFECTIVITYFrinied
11、in France图2R ESM OISPSY UNIT (AIR BLEED PAGE SELECTED)WITH PACK 1(2) i WITH PACK 1(2) HQDE SEL P/BSW :MODE SEL P/BSW PRESSED (IN)m ! PRESSED (INJ, IS PACK 1(Z) f IS PACK 1(2) TUR0 INLET TEMP； DISCH TEMPERATURE TOO HIGH(7EM- i TOO LOU ? PERATURE INDI- !CATION FLASHING!GREEN ABOVEi95*0 ?；:WITH PACK UZ
12、) iriODE SEL P/BSW:RELEASED (OiJT)z；CMAN LEGEND !on).:g TUR日 INLETANO PACK DISCH:TEMPERATURES!RETURN TO NORMAL !E (MAN CTL W !hqt OR COLD -P0SN)?WITH MAX COOL ； X-REF TO P/BSW PRESSED f FAULT CINJZ IS MAX COOL f ISOLATION SELECTION EFFEC-Stive (pack 1USCH TEMPERATURELOWERED FROM + 12*C TO -m 枷典:PACK
13、 DISCH TEMPERATURE STILL HIGH IN SPITE OF PACK TURBINE BYPASS VALVE POSITION ARROW INDICATING C.心典让:PACK TURBINE INLET TEMPERATURE EQUAL TO PACK DISCH TEMPERATURE.坠 NOTE : PACK TURBINE INLET TEMPERATURE HIGHER THAN PACK DISCH TEMPERATUREZA1 N哄 :PACK TURBINE INLET TEMPERATURE LOWER THAN PACK DISCH TE
14、MPERATURE,PACK TEMPERATURE CONTROL - FAULT SYMPTOMSLS2U100lA0ia0l-01EFFECT1VITY*21-61Printed m France图3PRECAUTIONS FOR ELECTfilCALAND FUEL 翌STEMS.TO TSM 24-57-00ATA REF, 1t*IIFRESELE匚TQR! 2S 42 00IACTUALQTYIII八 NORM. OR BATT； . / RELEASED；/F /；PRESSED ； ；(TEST) i i I | POSITION ； i * i ii；RELEASED |
15、/FUEL STATE 卜八FUEL STATE ! NORMALV /aBLANKBLOCK 5*ALL TANKS 洲W 日LANK | BLANK j BLOCK 7* L. OUTER/ L. INNER AND fLCTR/TT TANKS SHOH BLANK,八BLANKj日展比 3*| FUEL STATE ! .BLOCK 4*R- OUTER AND R. I敞ER ；*TANKS SHW 乳Ki J FUEL STATE | BLOCK 6*ONE OR MORE TANKS (iSHOW BLANKDASH IN LEAST SIGNIFI- CANT DIGIT FO
16、R ONE TANK； 如 旦9邛 INNER TANKS 、| FUEl3tATE J L FIG. 101 ； BLOCK 7L 盘】101DASH IN L*5* DIGIT FOR】BLOCK8CTR TANK UITH CTR AHO:jTT OR TT SELECTEDIFUEL 5TA* J!次5以9*TANK INDICATED QUANTITY；;DIFFERS HO抑 KNOWN QTV Lj FUEL STATEOR BLANK_kFIG. 101 ! BLOCK 6/2Sheet 2J iPREREQUISITES :EXTERNAL ELECTRICAL POWER
17、(flMM 2471-叩，P. BLOCK 301) |t 0白曜HME SAfEtyCN/A IF REFUELING ON A/C BATTERIES) IN : 321/P56 THRU 32VP61FDR REFUELING OK BATTEHY CONTROL C/B5, REFERREFUEL PANEL DOOR OPEH :REFUEL PANELPWR $UFPLX 臾 ! TEST 制 ；5 TA住K IMDKAT0RPOSTU i:/3ZZX &ASH IN LEAST SIGNIFICANT DIGIT FOR 5TI DISPLAYS/PRESELECTOR 1-RE
18、PORT MY FAULT SYMPTOM OR PATTERN NOT SHOWN ASOVE 42 00i ACTUAL1 QTY.尘 DEPEN&ING UPON FUEL QTY SWITCH POSITION CENTRE TANX DISPLAY WILL INDICATE CTR【CENTER T0, CTR AND T.T. (CENTER AND TRIM TK) OR T.T, (TRIM TK) QUANTITY.* THESE BLOCKS ARE LOCATED IN 28 42 DC, FIG. 102.F-O.I. REFUEL PANEL SYSTEM MONI
19、TOR/BITE TEST - FAULT SYMPTOMS (Sheet 1/2) LS2842001A04004EFFECT! VITY28-42Panted in FrameFigure 1D6PREREQUISITES :WARNING : OBSERVE SAFETY PRECAUTIONS FOR ELECTRICAL MD FUEL SYSTEMS.EXTERNAL ELECTRICAL POWER (AMM 24-41-OD, P. BLOCK 301) N7A IF REFUELING ON A/C BATTERIES) C/0$ IN : 3VP56 THRU 321/P6
20、1FOR REFUELING ON BATTERY CONTROL C/BSr REFER TO TSN 24-57-00REFUEL PANEL DOOR OPEN., ATA REF.；REf.UEL PANEL；PNR SUPPLY 胡 ； TEST 丝 ；5 TANK INDICATOR ； PRESELECTOR | 2S 42 OQPOSTN ；:/3:ACTUAL QTY ； -IJ-t/NORM OR BATT；.八RELEASED f .八FUEL STATE； AF4JEL STATE ! NORMALVV : : 7、 F 一 :Ii L i!/ Sheet 1:! Tf
21、tNK INDICATED QUANTITYJ ；i! I DIFFE典 ERM KNOWN E.：心 I : .FIG. 103!；i BLOCK 1EI*PRESSEDIALL*8*5 (AFTER； 2 SECrS);(TEST)ii礼L AFTER!伯 SEL$)，一NORMALi /!tI*t日LA忡K OR E$ HISSING Q INCOMPLETE j 卜81_。食 1*日LANK (DOES NOT 心心】ALL H) BLOCK 2+A州 FWTNJ DIM LED DISPLAY I OCK S*BATT : RELEASED : J WUEL STATE斥EL STA
22、TE 、NORMAL| /R. OUT Eft AI4D R, INNER ；!；:I TANK SHW BLANK:FUEL STATE fBLMK 6* iif iii i;r-REPORT ANY FAULT SYMPTOM OR PATTERN HOT SHOUN ABOVE 2B 42 00ZU PRESELECTOR WILL DISPLAY TOTAL OF ALL TANK QUANTITIES.* THESE BLOCKS ARE LOCATED IN 28 42 00, FIG* 的矿F.Q.l. REFUEL PANEL SYSTEM MONITOR/BITE TEST
23、- FAULT SYMPTOMS(Sheet 2/2)L52&42001A04504EFFECT1VITY20-42Prnld inB. ATA22, 27, 31和34章的例子（故障隔离图）在ATA22, 27, 31和34章，进入图表页也是通过目录，直接引导到故障隔离页。（参 考图8）。例如：在飞机上的现象1.1.1.1.1.1 NO FD BARON PFD首先，进入目录页，AUTO FLIGHT, CHAPTER 22 （参考图8） 在目录页可以找到下面标题：-FLIGHT DIRECTOR BARS DISPLAY ON PFD -在目录页的ATA REF栏里可以查到故障隔离页22-
24、10-03。对于这个章节，故障隔离被给出在两页。-页1给出了功能简图。-页 2 以表格形式给出 了 “SYMPTOMS AND RESULTS ON AIRCRAFT” 和 “ACTIONS TO BE TAKEN”（参考图 9，10）。如果电路不是太复杂，简图和列表将被显示在一页。TITLEATA REFauto flightAUTOMATIC FLIGHT SYSTEM - OUTPUT SUSES MEASUREMENT POINTS22-00-00AUTOMATIC FLIGHT SYSTEM - BITE PROCEDURE22-DO-OOAfS - STANDARD TROUBLE
25、 SHOOTING PROCEDURE22-00-01AFS - ELECTRICAL POWER SUPPLY - D1STR13UTI0N22-00-02AFS - ELECTRICAL POWER SUPPLY - CUT OFF/RESTORATION22DD-O3AFS - LANDING GEAR DATA PROCESSING2-00-04AFS - SLAT & FLAP DATA PROCESSING22-QD-05AFS - FLIGHT CONTROL UNIT OPERATION2200-06AUTOPILOTAfVFD -阡LIGHT COMPARTMENT CONF
26、IGURATION AFTER FCCDETECTED FAILURE22-10-00AP/FD - GENERAL OVERVIEW OF FCCS DIALOGUES & AP/FO OPERATION22-10-01FLIGHT OIRECTOR 1(2) ENGAGEMENT AND WARNINGS22-10-0FLIGHT DIRECTORS BARS DISPLAY ON PFD22-1D-03 kAUTOPILOT 13) ACTUATORS AND PObJER LOOP22-10-04AUTOPILOT 1(2) ENGAGEMENT IN CWS22-10-05 /AUT
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