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BOLT  OD  1.373  1.374  1.372  X  1 
311  BUSHING  ID  1.375  1.376  1.377  0.005  X 
BOLT  OD  1.373  1.374  1.372  X  1 
310 BUSHING  ID  1.437  1.438  1.439  0.005  X 
BOLT OD  1.435  1.436  1.434  X  1 
410  BUSHING  ID  1.375  1.376  1.377  0.005  X 
BOLT  OD  1.373  1.374  1.372  X  1
 411  BUSHING  ID  1.250  1.251  1.252  0.005  X 
BOLT  OD  1.248  1.249  1.247  X  1 
510  BUSHING  ID  1.375  1.376  1.377  0.005  X 
BOLT  OD  1.373  1.374  1.372  X  1 
5 11  BUSHING  ID  1.250  1.251  1.252  0.005  X 
BOLT  OD  1.248  1.249  1.247  X  1 
6  BUSHING  ID  0.7515  0.7525  0.754  0.005  X 
BOLT  OD  0.749  0.750  0.748  X  1 
7 BUSHING  ID  0.7515  0.7525  0.754  0.005  X 
BOLT  OD  0.749  0.750  0.748  X  1
 8 BUSHING  3  2.880  2.895  2.900  0.040  X 
BUSHING  4  2.864  2.874  2.854  X 
9 BUSHING  4  1.691  1.701  1.706  0.030  X 
BUSHING  5  1.681  1.686  1.676  X 

Main Landing Gear Reaction Link Wear Limits
Figure 601 (Sheet 3)

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 32-11-71
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
NO. INDEX  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  WORN PART REPLACE  PART WORN REPAIR  INSTR. REPAIR 
DIAMETER  DIM. WEAR MAX  ANCE CLEAR-DIAM MAX 
MIN  MAX 
10  TOTAL AXIAL CLEARANCE  6  0.006  0.057  8  0.085  9 
7  0.006  0.051  8  0.085  9 
BEARING (RACE) ID  ---- ---- 12  0.005
BEARING (BALL)  OD  ---- ---- 12 
10 11  BEARING (BALL)  ID  1.3745  1.3750  12  12 
BOLT  OD  1.3730  1.3740  1.372 
BEARING (RACE)  ID  ---- ---- 12  0.005  X 
BEARING (BALL)  OD  ---- ---- 12  X 
11 11  BEARING (BALL)  ID  1.2495  1.2500  12  12  X 
BOLT  OD  1.2480  1.2490  1.247  X 

REFER TO OVERHAUL MANUAL FOR REPAIR INFORMATION
FOR REACTION LINK/UPLOCK BOLT AND UPPER DOWNLOCK LINK BOLT, INSTALL BOLT HEAD AFT ON
LEFT HAND ASSEMBLIES, AND BOLT HEAD FORWARD ON RIGHT HAND ASSEMBLIES
DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN UPPER SIDE STRUT ASSEMBLY
DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN REACTION LINK ASSEMBLY
DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN REACTION LINK UNIVERSAL ASSEMBLY
TOTAL AXIAL CLEARANCE FOR JOINT WITH 65-46138-6,-10,-16 UPPER DOWNLOCK LINKS
TOTAL AXIAL CLEARANCE FOR JOINT WITH 65-46138-20 UPPER DOWNLOCK LINKS
MINIMUM BUSHING FLANGE THICKNESS 0.053
REPLACE WORN BUSHINGS
737-400 AIRPLANES
737-300/-500 AIRPLANES
THE TOTAL DIAMETRICAL CLEARANCE BETWEEN THE BEARING RACE, BEARING BALL, AND BOLT MUST
NOT BE GREATER THAN THE SPECIFIED MAX. DIA. CLEARANCE
Main Landing Gear Reaction Link Wear Limits
Figure 601 (Sheet 4)

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 32-11-71
 ALL  ú ú 01 Page 604 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E32899
A
737-300/400/500MAINTENANCE MANUAL
 MAIN LANDING GEAR DAMPER - REMOVAL/INSTALLATION
_______________________________________________
 1.  General
 A.  This procedure contains a tasks to remove and install the damper assembly of the main landing gear.
　
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