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MODULE - (FIM 27-10-00/101) 
FLIGHT CONTROLS HYDRAULIC POWER, M191 
MODULE - (FIM 27-40-00/101) 
L STABILIZER TRIM/RUDDER RATIO, M3136 
R STABILIZER TRIM/RUDDER RATIO, M3137 
MODULE - AILERON/RUDDER TRIM CONTROL, M7312  1  1  FLT COMPT, P8  27-21-09 
MODULE - LOWER RUDDER POWER CONTROL PACKAGE 3  1  324DL,324DR, VERTICAL FIN  27-21-17 
MODULE - UPPER RUDDER POWER CONTROL PACKAGE  3  1  324UL,324UR, VERTICAL FIN  27-21-17 
QUADRANT - AFT  3  1  VERTICAL FIN, FRONT SPAR TO REAR  27-21-08 
SPAR 
RATIO CHANGER - LOWER RUDDER, M258  4  1 324DL,324DR, VERTICAL FIN  27-21-12 
RATIO CHANGER - UPPER RUDDER, M560  4  1  324UL,324UR, VERTICAL FIN  27-21-12 
RUDDER - LOWER  2  1  325 AREA AFT OF VERTICAL FIN  27-21-01 
RUDDER - UPPER  2  1  326 AREA AFT OF VERTICAL FIN  27-21-01 
SERVO - (FIM 22-21-00/101) 
YAW DAMPER 
SERVO - RUDDER RATIO CHANGER, LOWER  4  1  27-28-12 
SERVO - RUDDER RATIO CHANGER, UPPER 4  1  27-28-12 
SWITCH - RUDDER TRIM CONTROL, S3  1  1  FLT COMPT, P8 AILERON/RUDDER  * 
TRIM CONTROL MODULE, M7312 
TRANSMITTER - LOWER RUDDER POSITION, T491  4  1  324FL,324FR, VERTICAL FIN  27-21-01 
TRANSMITTER - UPPER RUDDER POSITION, T490  4  1  324FL,324FR, VERTICAL FIN  27-21-01 
UNIT - (FIM 31-61-00/101) 
C EFIS/EICAS INTERFACE, M7352
 L EFIS/EICAS INTERFACE, M7353
 R EFIS/EICAS INTERFACE, M7351
VALVE - RUDDER & ELEVATOR HYDRAULIC SYSTEM 1 5  1  312A, STABILIZER JACKSCREW  27-23-01 
SHUTOFF, V142 
VALVE - RUDDER & ELEVATOR HYDRAULIC SYSTEM 2  5  1  312A, STABILIZER JACKSCREW  27-23-01 
SHUTOFF, V143
VALVE - RUDDER & ELEVATOR HYDRAULIC SYSTEM 3  5  1  312A, STABILIZER JACKSCREW  27-23-01 
SHUTOFF, V147
VALVE - RUDDER & ELEVATOR HYDRAULIC SYSTEM 4  5  1  312A, STABILIZER JACKSCREW  27-23-01 
SHUTOFF, V150 

* SEE THE WDM EQUIPMENT LIST
Rudder - Component Index
Figure 101 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
FAULT ISOLATION/MAINT MANUAL

RUDDER TRIM 
RUDDER PEDAL  P7 PANEL  POSITION INDICATOR RUDDER TRIM CONTROL KNOB (S3) 
ASSEMBLIES  P6 PANEL  (N308) 
SEE  B  AILERON/RUDDER TRIM  10  RUDDER TRIM 5 0  5  10 
CONTROL PANEL, M7312 
SEE  A  NOSE LEFT  UNITS  NOSE RIGHT 
AILERON 
P180 PANEL  NOSE  NOSE 
LEFT  RIGHT 
R 
LEFT  RIGHT  U D 
WING  WING  D 
DOWN  DOWN  E 
R 

AILERON/RUDDER TRIM CONTROL PANEL, M7312
A RUDDER RATIO MODULES, M3136, M3137 (REF) L, R STABILIZER TRIM/
PUSHRODS FROM FIRST OFFICER'S RUDDER PEDALS
RUDDER PEDAL ADJUSTMENT CRANK
RUDDER PEDAL
POSITION
TRANSDUCER
CAPTAIN'S CAPTAIN'S
CONTROL RUDDER
COLUMN PEDALS
RUDDER FORWARD QUADRANT
FIRST OFFICER'S RUDDER PEDALS
B
PASS CABIN FWD CEILING ACCESS PANEL 212
CAPTAIN'S RUDDER PEDALS
B
Rudder - Component Location Figure 102 (Sheet 1)
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 ALL  ú ú 01 Page 103 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
ACCESS PANEL ACCESS 324UL

AFT SURFACE POSITION
DIGITIZER CARD FILE, M8011

Rudder - Component Location
Figure 102 (Sheet 2)

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