SAE AMS 7482 : 1995

Superseded

View Superseded by

STUDS - STEEL, CORROSION AND HEAT RESISTANT,ROLL THREADED AFTER HEAT TREATMENT, 1800F (980 C) SOL HEAT TREATED

Available format(s)

Hardcopy , PDF

Superseded date

01-07-1991

Language(s)

English

Published date

01-01-1995

Publisher

SAE International

Covers aircraft quality studs made from a heat and corrosion resistant age hardenable iron base alloy UNS S66286 and of 130,000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200 degrees F.

DocumentType	Standard
Pages	18
PublisherName	SAE International
Status	Superseded
SupersededBy	SAE AS 7482 : 2015

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