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A
747-400 MAINTENANCE MANUAL
 WING GEAR WALKING BEAM - INSPECTION/CHECK
_________________________________________
 1.  General_______
 A.  The walking beam inspection measures the fit of the attach assemblies for the walking beam and the shock strut connection.
 B.  You must disconnect the walking beam from the shock strut to do the inspection.
 TASK 32-11-15-206-001
 2.  Walking Beam Examination For Worn Areas (Fig. 601)_______________________________________
 A.  References
 (1)  
32-11-15/401, Wing Gear Walking Beam

 (2)  
IPC 32-11-15 Fig. 2

 B.  
Access

 (1)  
Location Zone
 735 Wing Landing Gear, LH
 745 Wing Landing Gear, RH

 C.  
Procedure

 S 226-002
 (1)  
Disconnect the walking beam from the shock strut (Ref 32-11-15/401).

 S 226-003

 (2)  
Make a check of the worn limits of the attach points of the walking beam.

 (a)  
Measure the parts if it is necessary and compare the measured dimensions to the limit dimensions.

 (b)  
If the part is not in the tolerance, repair or replace it if it is necessary.

 (3)
Install the walking beam on the shock strut (Ref 32-11-15/401).

 S 436-004
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747-400 MAINTENANCE MANUAL
SEE A
1
FWD
A
A
A
1.
BUSHING/BOLT

2.
BUSHING/BOLT

3.
OVER BUSHING WALKING BEAM CLEVIS

FLANGES
4. BETWEEN
1 FOR WALKING BEAM-TO-HANGER
BUSHING
BOLT
BOLT INSPECTION/CHECK.
FLANGESREFER TO 32-11-16.
A-A
Wing Landing Gear Walking Beam Wear Limits Figure 601 (Sheet 1)
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747-400
MAINTENANCE MANUAL

INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE PART WORN  REPAIR WORN PART  REPAIR INSTR. 
DIAMETER  MITTED PER-WEAR DIM. 1  DIAM CLEAR-MAX ANCE
MIN  MAX 
1 2  BUSHING  ID  2.5000  2.5010  2.5042  0.0062  X 
BOLT  OD  2.4980  2.4990  2.4948  X  3 
2 2  BUSHING  ID  2.5000  2.5015  2.5055  0.0065  X 
BOLT 4  OD  2.4980  2.4990  2.4950  X  3 
3 2  5  3.688  3.694  3.716  0.044  X 
6  3.672  3.677  3.650  X 
4  7  1.437  1.450  1.471  X 

LIMITS SHOWN MAY BE EXCEEDED PROVIDED MAXIMUM CLEARANCE IS NOT EXCEEDED WALKING BEAM 65B01441 WORN PART IS REPAIRABLE. REFER TO OVERHAUL MANUAL FOR REPAIR INFORMATION BUSHING IN EAR OF SHOCK STRUT OUTER CYLINDER DISTANCE BETWEEN SHOULDER AND HEAD OF BOLT PLUS POSSIBLE 1/6 TURNBACK OF NUT WIDTH OVER FLANGES OF BUSHINGS WIDTH BETWEEN FLANGES OF BUSHINGS
Wing Landing Gear Walking Beam Wear Limits
Figure 601 (Sheet 2)

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 32-11-15
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 WALKING BEAM-TO-HANGER BOLT ASSEMBLY - MAINTENANCE PRACTICES
____________________________________________________________
　
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