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)

6.0 (150) MIN

IMPREGNATED REINFORCEMENT

1.0 (25)

0.25 (6.2)

6.0 (150)

1.0	1.0	0.25	0.03
(25)	(25)	(6.2)	(0.8)

1.0 (25)

0.125 (3.2)

2.75 (70.0)

TEST PANEL

NOTES:	1.	DIMENSIONS ARE IN inch (MILLIMETERS).
	2.	UNLESS OTHERWISE SPECIFIED, DIMENSIONS SHOWN SHALL BE NOMINAL.
	3.	SEALANT AND FABRIC COVERS LOWER 1 IN. (25 MM) OF PANEL IN THE
		OPTIONAL SPECIMEN.

FIGURE 2. Peel Specimen Configuration