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STUDS - STEEL, CORROSION AND HEAT RESISTANT,ROLL THREADED AFTER HEAT TREATMENT, 1800F (980 C) SOL HEAT TREATED
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Available format(s): Hardcopy, PDF
Superseded date: 07-01-1991
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.
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