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MIL-S-83318 Sealing Compound, Low Temperature Curing, Quick Repair Integral Fuel Tanks And Fuel Cell Cavities S/S By Sae-Ams-S-83318This specification covers a two component, temperature??resistant ??65??F to +250??F ??54??C to +120??C, low temperature 20??F minimum curing synthetic rubber compounds for quick repair of aircraft integral fuel tanks and fuel cell cavities. During application, the sealing compounds shall be a suitable, fluid consistency.

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MIL-S-83318A(USAF)




1.750 (44.50 mm)

0.125 (3.00 mm)


0.750 (19.00 mm)




7.00 (44.50 mm)

(9.50 mm)

0.250 (6.50 mm)


1.500 (38.00 mm)



1.500 (38.00 mm)


0


0.250 (6.50 mm)


0.375 (9.50 mm)

0.250 (6.50 mm)

1

0.625

(16.00 mm)


4


2.250 (57.00 mm)


1.000 (25.40 mm)


MATERIAL:  ALUMINUM ALLOY DIMENSIONS IN INCHES (MILLIMETERS)

UNLESS OTHERWISE SPECIFIED, TOLERANCES;

DECIMALS   + 0.016 INCH   (    + 0.40 MM).                         (NOT TO SCALE)




FIGURE 1. Flow-test fixture.


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