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 S 492-006
 WARNING: MAKE SURE THAT YOU HAVE DEVICES TO HOLD THE STRUTS BEFORE YOU
_______ REMOVE THE BOLTS. THE DRAG AND THE JURY STRUT ASSEMBLY WEIGH APPROXIMATELY 330 POUNDS. THE BUNGEE IS SPRING LOADED. IF YOU DO NOT DO SO, THE STRUT CAN CAUSE INJURY TO PERSONS AND DAMAGE TO PARTS.
 (3)  
Attach the bungee restraining tool to the bungee (AMM 32-33-16/401).

 E.
Procedure

 S 032-007
 (1)  
Disconnect the actuator strut (15) for the aft inboard door.

 (a)  
Remove the bolt (16), the spacers (17 and 22), the washer (23), the nut (24) and the cotter pin (25).

 S 032-008
 (2)  
Remove the pin assembly of the drag strut which has the bolt (1), the lubrication insert (3), and the O-rings (2).

 (a)  
Remove the nut (10), the washer (11) and the lockbolt (12).

 (b)  
Remove the nut (13) and the washer (14).

 (c)  
Install the thread protector.

 (d)  
Remove the drag strut bolt (1), the lubrication insert (3) and the O-rings (2) from the drag strut (9).

 S 032-009
 (3)  
Remove the pin assembly of the shock strut which has the bolt (19), the lubrication insert (21) and the O-rings (20).

 (a)  
Remove the self-locking nut (4), the washer (5) and the lockbolt (6).

 (b)  
Remove the nut (7), the washer (8) and the shock strut bolt (19) with the lubrication insert (21) and the o-rings (20).

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 32-13-07
 ALL  ú ú 01 Page 203 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 022-010
 (4)  Remove the universal (18) from the airplane.
 TASK 32-13-07-402-011
 3.  Body Gear Drag Strut Universal Installation (Fig.201)___________________________________________
 A. Special Tools and Equipment
 (1)  
2MIT65B08802-1 - Body Landing Gear Bungee Restraining Tool

 (2)  
3PRE65B00163-1 - Body Gear Shock Strut to Drag Strut Pin -Protective Equipment (Thread Protector)

 B.
Consumable Materials

 (1)  
D00633 Grease - BMS 3-33 (preferred)

 (2)  
D00013 Grease, MIL-G-23827 (optional)

 (3)  
B00316 Solvent, TT-N-95, Type I (preferred)

 (4)  
B00083 Solvent, TT-N-95, Type II (alternate)

 C.
References

 (1)  
AMM 07-11-01/201, Jacking Airplane

 (2)  
AMM 09-11-00/201, Towing

 (3)  
AMM 12-21-01/301, Landing Gear

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

 (5)  
AMM 32-14-00/501, Body Gear Doors

 (6)  
AMM 32-33-16/401, Body Gear Downlock Bungee

 (7)  
AIPC 32-13-02-02

 (8)  
AIPC 32-13-07-01

 D.
Access

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

 E.
Prepare for the Installation.

 S 222-012
 (1)  
Examine the drag strut bolt (1), the shock strut bolt (19) and the universal (18) for the permitted worn areas (as specified in the paragraph for the Body Gear Drag Strut Universal Examination for Worn Areas).

 S 112-013

 (2)  
Use the solvent to clean all the bolts, the washers, the nuts, the inserts, and the mating surfaces.

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 32-13-07
 ALL  ú ú 01 Page 204 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 432-014
 (3)  
Prepare the pin assemblies for the installation.

 (a)  
Examine the O-rings (2 and 20) for the worn areas or the damage.

 NOTE: Replace the O-ring if it is necessary.
____
 (b)  
Apply a thick layer of grease on the O-rings (2, 20), the lubrication inserts (3, 21) and the inner surface of the bolts (1, 19).
　
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