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SAE AS7481

Superseded

Superseded

View Superseded by

STUDS, STEEL, CORROSION AND HEAT RESISTANT 1800°F Solution Heat Treated Precipitation Heat Treated After Roll Threaded

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-07-1991

Superseded date

06-01-1997

Superseded by

SAE AS7481A

US$158.12
Excluding Tax where applicable

DocumentType
Standard
Pages
21
PublisherName
SAE International
Status
Superseded
SupersededBy

This procurement specification covers aircraft quality studs 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.

US$158.12
Excluding Tax where applicable