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2  SPINDLE  ID  0.9250  0.9270  0.9380  0.0200  X  1 
PLUG  OD  0.9180  0.9240  0.9070  X 
3  HEAD/SHOULDER  3.2600  3.2750  3.2960  0.0600  X  1 
STRUT BUSHINGS  3.2360  3.2600  3.2150  X  2 
4  BUSHING  ID  2.5000  2.5015  2.5075  0.0087  X  2 
BOLT  OD  2.4980  2.4990  2.4950  X  1 
5  BOLT  ID  1.6170  1.6200  1.6330  0.0250  X  1 
RETAINER  OD  1.6120  1.6140  1.5950  X  1 
6  BUSHING  ID  2.5000  2.5030  2.5060  0.0070  X  2 
BOLT  OD  2.4980  2.4990  2.4950  X  1 
7  STRUT BUSHINGS  5.7490  5.7540  5.7810  0.032  X  2 
SPINDLE BUSHINGS  5.7360  5.7490  5.7220  X  2 
8  HEAD/SHOULDER  8.3520  8.3670  8.3800  0.0080  X  1 
STRUT BUSHINGS  8.3000  8.3500  8.2870  X  2 

PART IS REPAIRABLE. REFER TO OVERHAUL MANUAL FOR REPAIR INFORMATION.
PROCURE REPLACEMENT BUSHING. INSTALL BUSHING PER 20-11-01 WITH INTERFERENCE FIT.
LIMITS MAY BE EXCEEDED PROVIDED MAXIMUM CLEARENCE IS NOT EXCEEDED.

Body Gear Upper Drag Strut Wear Limits
Figure 601 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-04
 ALL  ú ú 01 Page 603 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 BODY GEAR DRAG STRUT SPINDLE - MAINTENANCE PRACTICES
____________________________________________________
 1. General
_______
 A. This procedure has three tasks:
 (1)  
Remove the drag strut spindle of the body landng gear

 (2)  
Install the drag strut spindle of the body landing gear

 (3)  
Examine the drag strut spindle of the body landing gear for worn areas.

 TASK 32-13-05-002-001
 2. Body Gear Drag Strut Spindle Removal
____________________________________
 A. Special Tools and Equipment
 (1)  
F70312-26 - Torque wrench adapter for drag strut spindle

 B.
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

 C.
Access

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

 D.
Prepare for Removal

 S 492-024
 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 492-026
 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 Nose Landing Gear" (AMM 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-05
 ALL  ú ú 01 Page 201 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 492-028
 (3)  
Do this task: "Installation of the Door Locks on the Wing Landing Gear" (AMM 32-00-30/201).

 S 492-029

 (4)  
Do this task: "Installation of the Door Locks on the Body Landing Gear" (AMM 32-00-30/201).

 S 492-004
 WARNING:_______THE UPPER DRAG STRUT WEIGHS APPROXIMATELY 120 POUNDS. MAKE SURE THE STRUT IS HELD SUFFICIENTLY BEFORE YOU REMOVE THE DRAG STRUT OR THE SPINDLE. INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR IF THE UPPER DRAG STRUT FALLS.
　
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