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UNIT - (REF 31-61-00, FIG. 101) 
C EFIS/EICAS INTERFACE, M7352
 L EFIS/EICAS INTERFACE, M7353 
R EFIS/EICAS INTERFACE, M7351 
UNIT - (REF 27-51-00, FIG. 101)
 C FLAP CONTROL, M7880
 L FLAP CONTROL, M7881
 R FLAP CONTROL, M7879
UNIT - (REF 34-21-00, FIG. 101) 
C INERTIAL REFERENCE, B7163
 L INERTIAL REFERENCE, B7161
 R INERTIAL REFERENCE, B7162 

Autopilot/Flight Director System - Component Index
Figure 101 (Sheet 2)

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A

747-400 FAULT ISOLATION/MAINT MANUAL
P7 PANEL
AFCS MODE CONTROL
PANEL, B7080
SEE A
CAPTAIN'S THRUST CONTROL LEVERS WHEEL
SEE C
SEE B  FLIGHT COMPARTMENT
AFCS MODE CONTROL PANEL, B7080
A
CAPTAIN'S, FIRST OFFICER'S AUTOPILOT
DISENGAGE SWITCH, S282,S283
NOTE: THE AUTOPILOT DISENGAGE SWITCH AFCS GO-AROUNDON THE FIRST OFFICER'S CONTROL SWITCHES, S1,S2,S3WHEEL IS LOCATED ON THE RIGHT S4,S5,S6OUTBOARD HANDLE.
THRUST LEVERS CAPTAIN'S CONTROL WHEEL
C B
Autopilot/Flight Director System - Component Location Figure 102 (Sheet 1)
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A
747-400 FAULT ISOLATION/MAINT MANUAL
FLIGHT CONTROL

LEFT,CENTER,RIGHT, FLIGHT CONTROL COMPUTER (FCC), B7077,B7078,B7079

Autopilot/Flight Director System - Component Location
Figure 102 (Sheet 2)

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747-400
FAULT ISOLATION/MAINT MANUAL

OUTPUT TO
SPOILERS

LATERAL
AUTOPILOT SERVO, B7085 SEE G  VALVE ENGAGE SOLENOID CONNECTOR ELECTRICAL 
B7084,B7086 LEFT,RIGHT, CENTRAL LATERAL CONTROL PACKAGES, SEE F  SERVOVALVE ELECTROHYDRAULIC 
VALVE ARM SOLENOID 
LATERAL AUTOPILOT SERVO  VALVE SOLENOID ENGAGE 
HYDRAULIC SERVOVALVE ELECTRO- AUTOPILOT LVDT 
CRANK OUTPUT  VALVE ARM SOLENOID FILTER  B7084,B7086 CONTROL PACKAGE (CLCP), LEFT,RIGHT, CENTRAL LATERAL OUTPUT TO AILERONS 
AUTOPILOT LVDT  F 
OUTPUT LVDT  NOTE:____  THE LEFT CENTRAL LATERAL CONTROL PACKAGE IS SHOWN. THE RIGHT CLCP IS THE SAME. 
LATERAL AUTOPILOT SERVO (LAS), B7085 
G 

Autopilot/Flight Director System - Component Location
Figure 102 (Sheet 3)

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747-400
FAULT ISOLATION/MAINT MANUAL

LEFT, CENTER, RIGHT ROLLOUT POWER CONTROL PACKAGES, B7087, B7088, B7089
SEE H
AUTOPILOT LVDT
HYDRAULIC 
PRESSURE 
ROLLOUT 
ARM  POWER 
SOLENOID  CONTROL 
VALVE  PACKAGE 
(RPCP)
ELECTRO-
HYDRAULIC 
SERVOVALVE 
(EHSV)  OUTPUT 
CRANK 
HYDRAULIC 
RETURN 
FILTER 

ELECTRICAL CONNECTOR
ENGAGE SOLENOID OUTPUT VALVE LVDT
LEFT, CENTER, RIGHT
ROLLOUT POWER CONTROL PACKAGE (RPCP),
B7087, B7088, B7089

H
Autopilot/Flight Director System - Component Location Figure 102 (Sheet 4)
E24395
　
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