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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 424-016
 (8)  To remove air pockets, make a small hole with a pin and make it smooth with a roller.
 NOTE: Be careful not to cause creases with the roller.
____
 S 114-017
 WARNING: DO NOT GET SOLVENTS IN YOUR MOUTH, OR YOUR EYES, OR ON YOUR
_______ SKIN. DO NOT BREATHE THE FUMES FROM SOLVENTS. SOLVENTS ARE HAZARDOUS MATERIALS. SOLVENTS MAY BE FLAMMABLE OR HARMFUL TO THE ENVIRONMENT. REFER TO PRODUCT MATERIAL SAFETY DATA SHEETS (MSDS) AND LOCAL REQUIREMENTS FOR PROPER HANDLING PROCEDURES.
 (9)  
If you used BMS 5-14 adhesive, remove the unwanted adhesive with MEK , isopropyl alcohol, or ethyl alcohol .

 S 114-018

 (10)
 If you used BMS 5-55 adhesive, remove the unwanted adhesive with solvent (BMS 3-2, Type I) or aliphatic naphtha (TT-N-95).

 S 034-019

 (11)
 For markers with a protective paper facing, remove the paper facing.

 NOTE: Pull it at an 180 degrees direction to the marker.
____
 S 394-022
 (12) For protection of markers from BMS 3-11 Hydraulic Fluids, apply an edge sealer as follows:
 (a)  
Clean open surfaces as specified in this procedure.

 (b)  
Apply the edge sealer mixture with a brush.

 NOTE: Use a mixture of two-thirds 683-3-2 base to one-third
____ X-310A catalyst, by volume (AMM 51-21-61/701).
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 20-10-21
 ALL  ú ú 01 Page 407 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 LUBRICATION FITTINGS - REMOVAL/INSTALLATION
___________________________________________
 1.  General_______
 A.  This procedure gives instructions for installation of press-in type lubrication fittings.
 B.  For repair instructions for lubrication fittings on the landing gear components, refer to the Component Maintenance Manual, CMM 32-00-03.
 TASK 20-10-24-424-001
 2.  Lubrication Fittings - Installation___________________________________
 A.  General
 (1)  This task has instructions for installation of new lube fittings and lube fittings that were blown-out.
 B.  Equipment
 (1)  
Drive Tool - 5253-3 (for Alemite Type 1728B
 lubrication fittings)

 (2)  
Drive Tool - 5254-1 (for Alemite 1646B and
 1992B lubrication angle fittings)

 

 C.  Consumable Materials
 (1)  
B00025 Solvent - P-D-680

 (2)  
Cleaner:

 NOTE: Choose one of the cleaners that follow.
____
 (a)  
B00143 Solvent (Freon) MIL-C-81302

 (b)  
G00262 Nitrogen - Liquid, MIL-P-27401

 (3)  
C00316 Primer - Loctite Grade T (747)

 (4)  
Adhesive:

 (a)  G00106 Compound Retaining Loctite 675 or MIL-R-46082

 (5)  
G00106 Loctite - RC/680 or MIL-R-46082

 (6)  
Cotton swabs, Commercially Available

 D.  References
 (1) Component Maintenance Manual, CMM 32-00-03, Landing Gear Parts
 E.  Procedure - Installation of a New Lube Fitting
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 20-10-24
 ALL  ú ú 01 Page 401 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
DESIGN LUBE HOLE DIA IS .188/.189 INCHES
LUBE HOLE  LUBE FITTING 
DIA (X)  DIA 
(INCHES)  (INCHES) 
0.194 MAX  3/16  1 
0.195-0.247  1/4 MODIFIED  1 
0.248-0.249  1/4  2 
0.250-0.254  1/4  1 

INSTALL WITH ADHESIVE INSTALLATION WITH ADHESIVE OPTIONAL

ALL DIMENSIONS ARE IN INCHES
X (NOT SHOWN) = HOLE DIA IN MATING COMPONENT
A = SHANK DIA (X MINUS 0.007/0.012)
　
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