(f)  
Connect the door actuator rod to the door actuator beam with the bolt (5).

 (g)  
Tighten the nut to 600-1500 pound-inches.

 (h)  
Install the cotter pin.

 (i)  
If you cannot install the cotter pin or you can loosen the nut below the minimum torque after you install the cotter pin, do these steps: 1) Change the aft nut with the forward nut. 2) Install washers adjacent to the nuts.

 (j)  
Put the rod end of the actuator between the flanges of the actuator beam.

 (k)  
Install the nylon washers between the rod end and the flanges of the beam.

 CAUTION:_______HOLD THE BOLT WHEN YOU TIGHTEN IT. IF YOU PERMIT THE BOLT TO TURN, IT CAN CAUSE DAMAGE TO THE CLEVIS LOCKING DEVICE.

 (l)  
Install the bolt (4) with the square head in the milled recess.

 (m)  
Tighten the self-locking nut to 1400-1500 pound-inches.

 S 984-014
 (2)  
Manually lift the door.

 S 214-013

 (3)  
Make sure it does not hit or touch something.

 S 214-015

 (4)  
Make sure the linkage operates correctly.

 S 714-008

 (5)  
Make sure the adjustment for the wheel well doors for the wing landing gear is correct (Ref 32-12-00/501).

 S 094-009
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO REMOVE
_______ THE DOOR LOCKS FROM THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT REMOVE THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (6)  Do this task: "Wing Landing Gear Door Lock Removal" (Ref 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 094-012
 (7)  Do this task: "Body Landing Gear Door Lock Removal" (Ref 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-32-28
 ALL  ú ú 01 Page 405 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 WING LANDING GEAR DOOR SAFETY VALVE - REMOVAL/INSTALLATION
__________________________________________________________
 1.  General
_______
 A.  This procedure contains these two tasks:
 (1)  
The removal of the door safety valve for the wing landing gear

 (2)  
The installation of the door safety valve for the wing landing gear.

 B.  
To remove the door safety valve these operations are necessary:

 (1)  
Disconnect the hydraulic lines from the valve.

 (2)  
Disconnect the valve from the differential assembly.

 (3)  
Remove the clamping bolt and remove the valve.

 C.  
To install the safety valve these operations are necessary:

 (1)  
Install the hydraulic fittings in the valve.

 (2)  
Install the door safety valve.

 (3)  
Connect the hydraulic lines to the valve.

 D.  
The door safety valve is in the forward inboard corner of the wheel well of the wing landing gear. You can remove the safety valve independently or with the applicable differential.

 TASK 32-32-29-004-001
 2.  Wing Landing Gear Door Safety Valve Removal
___________________________________________
 A.  References
 (1)  
09-11-00/201, Towing

 (2)  
29-11-00/201, Main Hydraulic Supply System

 (3)  
32-00-30/201, Landing Gear Door Locks

 (4)  
IPC 32-36-08 Fig. 10

 B.  
Access

 (1)  
Location Zone
 135 Wing Landing Gear Wheel Well, LH
 136 Wing Landing Gear Wheel Well, RH

 C.  
Prepare for the Removal

 S 494-012
 WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
　
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