27-09-00
 ALL  ú ú 01 Page 203 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
AILERONS
COMPONENT  SHT 102 FIG.  QTY  ACCESS/AREA  REFERENCE 
ACTUATOR - AILERON TRIM, M254  3  1  LEFT WING GEAR WHEEL WELL  27-11-06 
ACTUATOR - INBOARD POWER CONTROL PACKAGE  4  2  573AB,673AB,573BB,673BB  27-11-12 
ACTUATOR - LEFT OUTBOARD AILERON LOCKOUT, X452 4  1  591CB, LEFT WING  27-11-14 
ACTUATOR - OUTBOARD POWER CONTROL PACKAGE  4  2  591CB,691CB,591CB,691DB  27-11-13 
X453 ACTUATOR - RIGHT OUTBOARD AILERON LOCKOUT,  4  1  691CB, RIGHT WING  27-11-14 
AILERON - INBOARD 4  2  WING TRAILING EDGE  27-11-01 
AILERON - OUTBOARD  4  2  WING TRAILING EDGE  27-11-02 
ASSEMBLY - AILERON DRUM  1  2  211,212, FWD PASS CABIN CEILING  27-11-04 
CARD - AILERON/SPOILER SURFACE POSITION DIGITIZER (SPD), YMLA17 1  1  ELEC SYS CARD FILE, M7603 (REF) LEFT OF NOSE GEAR WHEEL WELL,  27-18-02
CIRCUIT BREAKERS SPLR/ALRN SENSOR, C384 SPLR/ALRN IND, C10062 OUTBOARD AILERON LOCKOUT, C1186 AILERON TRIM, C75  1  16  6J20 6J21 7D18 7D17 FLT COMPT, P6,P7  * * * *
LIMITER - AILERON CONTROL LOAD  2  1  212, FWD PASS CABIN CEILING  27-11-05 
LIMITER - AILERON FORCE  2  1  LEFT WING GEAR WHEEL WELL  27-11-26 
MECHANISM - AILERON TRIM AND FEEL  3  1  LEFT WING GEAR WHEEL WELL  27-11-06 
MECHANISM - OUTBOARD AILERON LOCKOUT  4  2  591CB,691CB, WING  27-11-14 
MODULE - (REF 27-40-00, FIG. 101) R STABILIZER TRIM/RUDDER RATIO, M3137 MODULE - FLIGHT CONTROLS HYDRAULIC POWER, M191 MODULE - (REF 27-20-00, FIG. 101) AILERON/RUDDER TRIM CONTROL, M7312 L STABILIZER TRIM/RUDDER RATIO, M3136  1  1  FLT COMPT, P461  * 
PACKAGE - RIGHT AUTOPILOT - CENTERAL LATERAL CONTROL 3  1  LEFT WING GEAR WHEEL WELL  27-11-08 
AUTOPILOT - CENTERAL LATERAL CONTROL PACKAGE - LEFT 3  1  RIGHT WING GEAR WHEEL WELL  27-11-08 

* SEE THE WDM EQUIPMENT LIST
Ailerons - Component Index
Figure 101 (Sheet 1)

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 27-10-00
 ALL  ú
 ú  01  Page 101
 ú  Jun 10/91 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
COMPONENT  SHT 102 FIG.  QTY  ACCESS/AREA  REFERENCE 
QUADRANT - CLC INPUT  2  1  RIGHT WING GEAR WHEEL WELL  27-11-09 
QUADRANT - INBOARD AILERON  4  1  573AB,673AB,573BB,673BB, WING  27-11-11 
QUADRANT - LEFT AILERON PROGRAMMER  3  1  LEFT WING GEAR WHEEL WELL  27-11-10 
QUADRANT - OUTBOARD AILERON  4  1  591CB,691CB,591DB,691DB, WING  27-11-14 
QUADRANT - RIGHT AILERON PROGRAMMER  3  1  RIGHT WING GEAR WHEEL WELL  27-11-10 
QUADRANT - TRIM AND FEEL MECHANISM  3  1  LEFT WING GEAR WHEEL WELL  27-11-06 
ROD - LEFT CLC CONTROL  3  1  LEFT WING GEAR WHEEL WELL  27-11-26 
SERVO - (REF 22-10-00, FIG. 101) SWITCHES -LATERAL AUTOPILOT, B7085 ROD - RIGHT CLC CONTROL  3  1  RIGHT WING GEAR WHEEL WELL  27-11-26 
AILERON TRIM ARMING SWITCH, S1 1  1  TRIM CONTROL PANEL M7312 FLT COMPT, P8, AILERON/RUDDER * 
AILERON TRIM CONTROL SWITCH, S2  1 1  TRIM CONTROL PANEL M7312 FLT COMPT, P8, AILERON/RUDDER * 
TRANSMITTER - LEFT INBOARD AILERON POSITION, T1670  6  1  573BB, LEFT WING  27-18-01 
TRANSMITTER - LEFT OUTBOARD AILERON POSITION, T489  6  1  591BB, LEFT WING  27-18-01 
TRANSMITTER - RIGHT INBOARD AILERON POSITION, T1671 6  1  673BB, RIGHT WING  27-18-01 
TRANSMITTER - RIGHT OUTBOARD AILERON UNIT - (REF 31-61-00, FIG. 101) R EFIS/EICAS INTERFACE, M7351 L EFIS/EICAS INTERFACE, M7353 C EFIS/EICAS INTERFACE, M7352 POSITION, T488 6  1  691CB, RIGHT WING  27-18-01 
VALVE - AILERON & SPOILER HYDRAULIC SYSTEM 1 SHUTOFF, V140 5  1  591BB, LEFT WING  27-13-01 
　
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