S 215-279

 (6)  
Make sure the rudder is no more than 0.10 inch (2.54 mm) away from the rudder neutral datum position.

 S 865-280

 (7)  
Remove the power from the right hydraulic system
 (AMM 29-11-00/201).

 S 865-281

 (8)  
Supply pressure to the center hydraulic system
 (AMM 29-11-00/201).

 S 215-282

 (9)  
Make sure the rudder is no more than 0.10 inch (2.54 mm) away from the rudder neutral datum position.

 R.
Put the Airplane Back to Its Usual Condition

 S 865-302
 (1)  
Remove the DO-NOT-CLOSE tag and close this circuit breaker on the P11 panel:

 (a)  
11D18 or 11G10, RUD RATIO

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 27-21-00
 ALL  ú ú 06 Page 580L ú Jan 28/02
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757
MAINTENANCE MANUAL

 S 865-303
 (2)  Remove the DO-NOT-OPERATE tags and move the AUTOPILOT/FLIGHT DIRECTOR switches on the P55 panel to ON.
 S 215-007 CAUTION: IF THE RRCM TEST SWITCH IS NOT MOVED TO "NORMAL", THE AMBER
_______ "RUDDER RATIO" LIGHT WILL COME ON. IF THIS LIGHT IS ON, THE AIRPLANE CANNOT BE DISPATCHED.
 (3)  Make sure the RRCM test switches are in their NORMAL positions.
 S 095-013 WARNING: STAY AWAY FROM THE NOSE WHEELS WHEN THE LOCKPIN IS REMOVED.
_______ THE WHEELS CAN TURN TO THE CENTER POSITION QUICKLY, AND CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (4)  
Make sure the nose wheels are in their center position and remove the towing lever lockpin from the nose gear (Fig. 503).

 S 865-304

 (5)  
Remove the power from the left, right, and center hydraulic systems (AMM 29-11-00/201).

 S 095-305

 (6)  
Remove rig pins. S 415-306

 (7)  
Close access doors and panels. S 865-307

 (8)  
Remove electrical power if it is not necessary (AMM 24-22-00/201).

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MAINTENANCE MANUAL

 RUDDER PEDALS - REMOVAL/INSTALLATION
____________________________________
 1.  General
_______
 A.  This procedure contains 2 tasks. The first task contains the data that is necessary to remove the rudder pedal assemblies. The second task contains the data that is necessary to install them.
 TASK 27-21-02-024-003
 2.  Remove Rudder Pedal Assembly
____________________________
 A.  Equipment
 (1)  
Nose Gear Towing Lever Lockpin - A09003-1

 B.  
References

 (1)  
06-41-00/201, Fuselage Access Doors and Panels

 (2)  
24-22-00/201, Electrical Power - Control

 C.  
Access

 (1)  
Location Zones
 211 Control Cabin (Left)
 212 Control Cabin (Right)

 (2)  
Access Panels 113AL Flight/Landing Gear/Engine Control Components

 D.  
Prepare for Removal

 S 864-004
 (1)  
Supply electrical power (Ref 24-22-00).

 S 864-005

 (2)  
Move the FLT CONTROL SHUTOFF switches L, C, and R on the right side panel, P61, to OFF. Attach DO-NOT-OPERATE tags and make sure that the amber switch-position legend lights come ON.

 S 864-006

 (3)  
Open these circuit breakers on the overhead panel, P11, and attach DO-NOT-CLOSE tags:

 (a)  
11H17, FLT CONT SHUTOFF TAIL LEFT

 (b)  
11H18, FLT CONT SHUTOFF TAIL CTR

 (c)  
11H28, FLT CONT SHUTOFF TAIL RIGHT

 (4)  
Remove the side panels from the rudder pedal cover.

 S 014-008

 (5)  
Open access panel 113AL for the rudder pedal assembly, the forward quadrant, and the steering interconnect mechanism (Ref 06-41-00).
　
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