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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 BODY LANDING GEAR LOWER TORSION LINK - MAINTENANCE PRACTICES
____________________________________________________________
 1. General
_______
 A. This procedure contains three tasks:
 (1)  
The removal of the lower torsion link on the body landing gear.

 (2)  
The installation of the lower torsion link on the body landing gear.

 (3)  
The inspection for wear of the lower torsion link on the body landing gear.

 TASK 32-13-14-002-001
 2. Body Landing Gear Lower Torsion Link Removal (Fig./201)
____________________________________________
 A. Standard Tools and Equipment
 (1)  
Webbing - Nylon, 1-inch minimum width

 B.
References

 (1)  
AMM 09-11-00/201, Towing

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

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

 (4)  
AMM 32-45-01/401, Main Gear Tire and Wheel

 (5)  
AIPC 32-13-14 Fig. 1

 (6)  
AIPC 32-13-67 Fig. 1

 (7)  
AIPC 32-45-01 Fig. 2,

 (8)  
AIPC 32-45-03 Fig. 2

 (9)  
AIPC 32-45-04 Fig. 1

 C.
Access

 (1)  
Location Zone
 755 Body Landing Gear, LH
 765 Body Landing Gear, RH

 D.
Prepare for the Removal

 S 492-036
 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) Install the ground locks in all landing gear (AMM 09-11-00/201).
 S 842-027
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK 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 OR DAMAGE TO EQUIPMENT.
 (2)  Do this task: "Installation of the Door Locks on the Wing Landing Gear" (AMM 32-00-30/201).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

SHOCK STRUT
ELECTRICAL CONDUIT SEE A
FWD
TORSION LINK
Body Gear Torsion Link Electrical Installation
Figure 201 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
 (3)  S 842-029Do this task: "Installation of the Door Locks on the Body Landing Gear" (AMM 32-00-30/201).
 (4)  S 862-004Decrease the pressure on the hydraulic system No. 1 (AMM 29-11-00/201).
 (5)  S 492-005Hold the actuators to remove all load on the torsion link.
 (6)  S 032-006Remove the electrical conduit from the torsion link (Fig. 201). (a) Remove the bolts (2) and the nuts (3) to remove the pull box (1) from the torsion link. (b) Keep the conduit fairlead (7) and the conduit attached to the bracket.
 NOTE:____ The bracket with the fairlead attached is removed during the removal of the hydraulic installation.
 (c)  Remove the bolts (5) and the washers (4) to remove the apex fairlead assembly.
 (7)  S 032-007Remove the hydraulic tubing and the brackets from the torsion link (Fig. 202). (a) Remove the hydraulic clamp and the trapeze (8) from the spindle (Section A-A, Fig. 202). 1) Remove the nut (5), the washer (1, 2 and 3), the shaft (9) and the bolt (6) from the spindle. 2) Remove the hydraulic clamp and the trapeze.
　
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