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A

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MAINTENANCE MANUAL

SEE  A  1  1 2 FLT CONTROL HYD POWER NORM 3  4 
TAIL OFF SHUT 
CLOSED a VALVE  VALVE aCLOSED  CLOSED a VALVE  aCLOSED VALVE 
1 
NORM 
OFF SHUT WING 
aCLOSED VALVE  CLOSED a VALVE  VALVE CLOSED a  CLOSED a VALVE 
FLIGHT COMPARTMENT 
POWER MODULE FLT CONTROL HYD 
A 

F/O ELEVATOR 
FORWARD 
QUADRANT 
SEE  D 
SEE  E 
CONTROL 
COLUMN  E2A 
SEE  B 
E2B 
TORQUE 
TUBE  CAPT ELEVATOR 
FORWARD QUADRANT  E1B 
SEE  C  E1A 

1 ON SOME AIRPLANES THE NORM POSITION IS DOWN AND THE SHUT OFF POSITION IS UP.
Elevator Control System Component Location Figure 2 (Sheet 1)
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MAINTENANCE MANUAL

FIRST OFFICER'S
CONTROL COLUMN
RIGHT STICK
SHAKER

CAPTAIN'S CONTROL COLUMN
TORQUE TUBE
LEFT STICK SHAKER
CONTROL COLUMM
CONTROL COLUMN
B
TORQUE TUBE
RIGGING PIN E-1
E2A
E1B
E2B
CAPT
F/O ELEVATOR
ELEVATOR
FORWARD
FORWARD
QUADRANT
QUADRANT
FWD TENSION REGULATOR
E1A
FWD

CAPT ELEVATOR FORWARD QUADRANT  F/O ELEVATOR FORWARD QUADRANT
C D
Elevator Control System Component Location
Figure 2 (Sheet 2)

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E2A
E2B
E1B
ELEVATOR
E1A

FEEL UNIT
ELEVATOR AUTOPILOT SERVO MODULE (3 PLACES)
ELEVATOR
FEEL COMPUTER

ELEVATOR AFT QUADRANTELEVATOR FEELFWD ACTUATOR
INBOARD ELEVATOR AFT TORQUE TUBE
POWER CONTROL
PACKAGE

RIGGING PIN E-2
SLAVE LINKAGE
LEFT INBOARD ELEVATOR
LEFT OUTBOARD ELEVATOR
OUTBOARD ELEVATOR
POWER CONTROL
PACKAGE

ELEVATOR CONTROLS
E
Elevator Control System Component Location Figure 2 (Sheet 3)
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MAINTENANCE MANUAL

SEE  A SEE  B  STRUCTURE INSPECTION (TYPICAL 7 PLACES) PANEL IN LOWER SKIN 
INBOARD HOIST POINTS 
HINGE FITTING (TYPICAL 4 PLACES) 
ACTUATOR ATTACHMENT AND REACTION HINGE FITTING INBOARD HOIST POINTS  INBOARD ELEVATOR (LH SHOWN; RH OPPOSITE) A OUTBOARD HOIST POINTS 

STRUCTURE INSPECTION PANEL IN LOWER SKIN (TYPICAL 11 PLACES)
ADJUSTABLE WEIGHTS (TYPICAL, OUTBOARD HOIST POINTS3 INBOARD ACTUATOR
BALANCE ATTACHMENT
WEIGHT AND REACTION
INSTALLATIONS)
HINGE
FITTING BALANCE WEIGHT
(6 PLACES)

OUTBOARD ELEVATOR HINGE FITTING
(LH SHOWN; RH OPPOSITE)
(TYPICAL 6 PLACES)
B
Elevators - Mechanism Components Figure 3
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