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 ALL  ú ú 01 Page 404 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (c) (d) (e)  Tighten the cable retaining nut.On the first officer's cable, install the 13-inch nylon tube on the rudder pedal adjustment cable.Install all the cable clamps. 1) Make sure the cable radius is more than 5.0 inch for all the curves in the cable.
 NOTE:____ If the radius is less than 5.0 inch, the cable will not operate correctly.
 (3)  S 714-010Turn the adjustment crank to move the rudder pedals fully forward and then aft. (a) Make sure the cable operates smoothly and freely.
 (4)  S 224-011Do a check of the rudder pedal travel (Ref 27-21-00/501).
 (5)  S 414-012Install the overhead access panels in the forward part of the lower nose compartment.
 (6)  S 414-013Close the access door 1103 (Ref 12-31-11/201).

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 27-21-41
 ALL  ú ú 01 Page 405 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 RUDDER FORWARD QUADRANT - REMOVAL/INSTALLATION
______________________________________________
 1.  General_______
 A.  This procedure contains the removal and installation tasks for the rudder forward quadrant, applicable to the Captain's and the First Officer's quadrants.
 TASK 27-21-51-024-001
 2.  Rudder Forward Quadrant Removal_______________________________
 A.  Special Tools and Equipment
 (1)  
Rigging Pins Kit - F70207-107

 (2)  
Rig Pin Kit F70207, Assy P/N (-11), Rig Pin (R-5), Rudder Feel and Centering Unit

 B.  
References

 (1)  
12-31-11/201, Body Section 41 Access Doors and Panels

 (2)  
27-21-00/201, Rudder and Rudder Trim Control System

 C.  
Access

 (1)  
Location Zones
 101 Control Cabin - Left
 102 Control Cabin - Right

 (2)  
Access Panel
 1103 Left Forward Access Door

 D.  
Prepare for the Removal

 S 864-003
 (1)  
Remove all hydraulic power from the rudder system (AMM 27-21-00/201).

 S 494-004

 (2)  
Install rig pin R-5 in the output crank of the feel and centering unit (Fig. 402).

 E.  
Remove the Rudder Forward Quadrant (Fig. 401)

 (1)
Remove the forward overhead access panels at the nose wheel well.

 (2)
Open the lower nose compartment door, 1103, (AMM 12-31-11/201).

 S 014-005
 S 014-057
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 27-21-51
 ALL  ú ú 02 Page 401 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 034-006
 WARNING:_______ BEFORE YOU DISCONNECT THE BUSROD, LOOSEN OR DISCONNECT THE
 RUDDER CABLES FROM THE QUADRANTS.  RELEASE THE TENSION EQUALLY
 IN THE TWO CABLES.  IF YOU DO NOT RELEASE THE TENSION, INJURY

 TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (3)  
Loosen the two rudder cables.

 S 034-007

 (4)  
Disconnect the applicable cables from the quadrant that you will remove.

 S 034-008

 (5)  
Disconnect the busrod and the pushrods from the forward quadrant.

 S 034-009

 (6)  
Remove the bearing plate from the bottom of the right jackshaft assembly.

 S 034-010

 (7)  
If you will remove the left quadrant, remove the rudder pedal steering arm from the bottom of the jackshaft assembly.

 S 034-011

 (8)  
Remove the aft adjustment shaft clamps for the two rudder pedals.

 S 034-012

 (9)  
Remove the bolts that hold the adjustment shaft support bracket to the structure and the jackshaft support channel.

 S 034-013
　
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