Document ID:	MIL-S-83318       Scroll down to access document images

Overview

Title:  SEALING COMPOUND, LOW TEMPERATURE CURING, QUICK REPAIR INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES (S/S BY SAE-AMS-S-83318) Scope:  This 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. Status:  Canceled Cancellation Date:  28-SEP-1999       FSC/Area:  8030 Doc Category:   Detail Specification

Responsibilities

Lead Standardization Activity:  MR  Army Research Laboratory, Weapons and Materials Research Directorate     Preparing Activity: 11  Air Force Life Cycle Management Center - Aircraft Systems Coordination:  Limited   Air Force Custodian:  11   Air Force Life Cycle Management Center - Aircraft Systems

Amendments to military specifications or specification sheets issued after August 1, 2003 are incorporated in the modified document.

Revision History

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