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747-400 MAINTENANCE MANUAL
 (e)  Disconnect the cables from the quadrant.
 TASK 32-31-04-404-008
 4. Wing Landing Gear Selector Valve Quadrant Installation
______________________________________________________
 A. Consumable Materials
 (1)  
C00308 Compound - Corrosion Preventive - MIL-C-11796, Class 3

 (2)  
C00712 Primer - MIL-P-8585, Color Y

 B.
References

 (1)  
09-11-00/201, Towing

 (2)  
25-22-01/401, Main Passenger Cabin Ceiling Panels

 (3)  
29-11-00/201, Main Hydraulic Supply System

 (4)  
32-00-30/201, Landing Gear Door Locks

 (5)  
32-31-00/501, Landing Gear Control

 (6)  
IPC 32-31-63 Fig. 1

 C.
Access

 (1)  
Location Zone
 138 Body Landing Gear Wheel Well, Right

 D.
Procedure

 S 494-021
 WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1)  Make sure you install the ground locks in all landing gear (Ref 09-11-00/201).
 S 494-010
 WARNING:_______ YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO INSTALL
 THE DOOR LOCKS ON THE LANDING GEAR DOORS.  THE DOORS CAN CLOSE
 QUICKLY IF YOU DO NOT INSTALL THE DOOR LOCKS CORRECTLY.  THIS

 CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  Do this task: "Installation of the Door Locks on the Doors for the Wing Landing Gear" (Ref 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 S 494-019
 (3)  Do this task: "Installation of the Door Locks on the Doors for the
 Body Landing Gear" (Ref 32-00-30/201).
 S 864-011
 (4)  Make sure there is no pressure to hydraulic system No. 4
 (Ref 29-11-00/201).
 S 424-013
 (5)  Install the selector valve quadrant (Fig. 401 and 404):
 (a) Connect the cables to the quadrant.
 (b) Install the cotter pins.
 (c) Apply corrosion preventive compound to the bolt hole for the
 quadrant attach bolt.
 (d) Install the quadrant into the quadrant bracket.
 (e) Install the quadrant attach bolt.
 (f) Connect the control rod assembly to the quadrant clevis:
 1) Apply the wet primer to all areas of the hole and
 immediately install the bolt, washer, and bushing.
 2) If the bolt does not have a hole in the shank for a cotter
 pin, install a self-locking nut.
 a) Tighten the self-locking nut to the approved torque
 value.
 3) If the bolt has a hole in the shank for a cotter pin, do
 the steps that follow:
 a) Install a nut that has castellations.
 b) Tighten the nut to a torque range of 20 to 40
 pound-inches.
 c) If it is necessary, increase the torque to 60
 pound-inches maximum to align the castellation with the
 hole in the bolt.
 d) Install the cotter pin.
 S 834-014
 (6)  Adjust the control system for the landing gear (Ref 32-31-00/501).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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747-400 MAINTENANCE MANUAL
　
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