E.
Remove the Drag Strut Spindle (Fig. 201)

 S 032-005
 (1)
Remove the spindle lockbolt (6) and loosen the spindle nut (1).

 S 032-006

 (2)  
Remove the upper drag strut which includes the hydraulic swivel, the hydraulic lines of the swivel bracket and the spindle bolt (Ref 32-13-04/401).

 S 032-007

 (3)  
Use the special torque wrench adapter to remove the spindle nut (1) and the splined washer (5).

 S 022-008

 (4)  
Remove the spindle (4) and the spindle washer (3) from the structure.

 NOTE: The spindle weighs approximately 30 pounds.
____
 TASK 32-13-05-402-009
 3.  Body Gear Drag Strut Spindle Installation_________________________________________
 A. Special Tools and Equipment
 (1)  
F70312-26 - Torque wrench adapter for drag strut spindle

 B.
Consumable Materials

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

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-05
 ALL  ú ú 01 Page 202 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

SEE A
FWD
2.  NUT
LUBE RETAINER
1.  SPINDLE
NUT

O-RINGS
SPINDLE BOLT
6.  LOCKBOLT
5.  SPLINED
WASHER HYDRAULIC SWIVEL
4.  SPINDLE
3.  SPINDLE
WASHER

SWIVEL BRACKET STRUCTURE
DRAG STRUT
FWD
A
Body Gear Drag Strut Spindle Installation Figure 201
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-05
 ALL  ú ú 01 Page 203 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

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

 C.
References

 (1)  
AMM 09-11-00/201, Towing

 (2)  
AMM 32-00-30/201, Landing Gear Door Locks

 (3)  
AMM 32-13-04/401, Body Gear Upper Drag Strut

 (4)  
AIPC 32-13-01 Fig. 1

 (5)  
AIPC 32-13-05 Fig. 1

 (6)  
AIPC 32-13-10 Fig. 1

 D.
Prepare for Installation (Fig. 201)

 S 222-011
 (1)  Do a check on the spindle (4) and the structural attachment points for permitted wear limits.
 NOTE: The wear limits for the attach points are found on Fig. 202
____
 or referred to in other sections.

 S 642-012
 (2)  
Lubricate the spindle (4) shank, the washer (3) and (5) surfaces, the nut (1) and the spindle threads with grease immediately before installation.

 E.
Install the Drag Strut Spindle (Fig. 201)

 S 422-013
 (1)  
Insert the spindle washer (3) on the spindle (4), insert the spindle in the structure and install the splined washer (5) and the nut (1).

 S 432-014

 (2)  
Install the upper drag strut, the hydraulic swivel bracket, the hydraulic lines and the spindle bolt (AMM 32-13-04/401).

 NOTE: After you install the upper drag strut, tighten the spindle
____ nut (1) (before you do a check on the hydraulic connections for leaks or the jury strut for correct alignment). These checks are necessary in AMM 32-13-04/401.
 S 432-015
 (3)  Use the special torque wrench adapter to tighten the spindle nut (1) 3600 to 4800 pound-inches maximum.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-05
 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 432-022
 (4)  
Loosen the nut and then tighten it to get the 0.001 to 0.003-inch gap.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 起落架 LANDING GEAR 3(3)