Standard

SAE AS7479

May 1995 Withdrawn

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Language English

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Abstract

This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, and of 130 000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200°F.

Document information

Standard from SAE International
Published: 1 May 1995
Withdrawn: 10 May 2006
Document type: IS
Pages
ISBN:

Publisher SAE International
Distributor SAE International

Product Relations

Referred by: SAE AS5355B
Refers: SAE AMS2750
Refers: SAE AS3063
Refers: SAE AMS2645

SAE AS7479

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