* SEE WDM EQUIPMENT LIST 
Brake Control System - Component Index 
Figure 101 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 32-42-00
 ALL  ú ú 02 Page 102 ú Oct 18/99 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A 
747-400 FAULT ISOLATION/MAINT MANUAL 
COMPONENT  102 SHT FIG.  QTY  ACCESS/AREA  AMM REFERENCE  
TRANSDUCER - WHEEL SPEED  11 16 HUBCAP, MAIN WHL AXLE  32-42-04  
M46  1 L WING GEAR, R REAR WHL  32-42-04  
M47  1 L WING GEAR, R FRONT WHL  32-42-04  
M48  1 L WING GEAR, L FRONT WHL 32-42-04  
M49  1 L WING GEAR, L REAR WHL 32-42-04  
M50  1 L BODY GEAR, R REAR WHL  32-42-04  
M51  1  L BODY GEAR, R FRONT WHL  32-42-04  
M52  1 L BODY GEAR, L FRONT WHL  32-42-04  
M53  1 L BODY GEAR, L REAR WHL  32-42-04  
M54  1 R BODY GEAR, R REAR WHL  32-42-04  
M55  1 R FRONT WHL, R BODY GEAR  32-42-04  
M56  1 R BODY GEAR, L FRONT WHL  32-42-04  
M57  1  R BODY GEAR, L REAR WHL  32-42-04  
M58  1 R WING GEAR, R REAR WHL  32-42-04  
M59  1 R WING GEAR, R FRONT WHL  32-42-04  
M60  1  R WING GEAR, L FRONT WHL  32-42-04  
M61  R WING GEAR, L REAR WHL  32-42-04  
UNIT - BRAKE SYSTEM CONTROL, M80  2  1 125B, CENTER EQUIP CTR, E9  32-42-01  
VALVE - ANTISKID (ALTERNATE), V35, V36, V37,  4  8 ALT ANTISKID MODULES  32-42-02  
V38, V129, V130, V131, V132  
VALVE - ANTISKID (NORMAL), V24, V25, V26,  3 16 NORMAL ANTISKID MODULES  32-42-02  
V41, V42, V43, V44, V51, V65, V69, V73, V77, 
 V126, V127, V128 
VALVE - ANTISKID SHUTOFF  3  4 NORMAL ANTISKID MODULES  32-42-02  
VALVE - AUTOBRAKE PRESSURE CONTROL  7  1 AUTOBRAKE PRESS CONT VALVE  32-42-11  
MODULE 
VALVE - AUTOBRAKE SHUTTLE  8  2 AUTOBRAKE SHUTTLE VALVE ASSEMBLY  32-42-12  
VALVE - CHECK (ALTERNATE ANTISKID)  4  4 ALT ANTISKID MODULES  32-42-02  
VALVE - CHECK (NORMAL ANTISKID)  3  4 NORMAL ANTISKID MODULES  32-42-02  
VALVE - SERVO CONTROL, YCJV02  7  1 AUTOBRAKE PRESS CONT MODULE  32-42-11  
VALVE - SOLENOID, YCJV01  7  1 AUTOBRAKE PRESS CONT MODULE  32-42-11 
Brake Control System - Component Index 
Figure 101 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 32-42-00
 ALL  ú ú 01 Page 103 ú Oct 18/99 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 起落架 LANDING GEAR 7(5)