This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718 and of 185 000 psi tensile strength at room temperature, with maximum test temperature of parts at 800°F.
BOLTS AND SCREWS, NICKEL ALLOY, CORROSION AND HEAT RESISTANT Forged Head, Roll Threaded, Fatigue Rated
1991-01-22
Conference paper
English
SAE Technical Papers | 1991
BOLTS AND SCREWS, CORROSION-RESISTANT WORK-STRENGTHENED ALLOY Forged Head, Roll Threaded After Aging
SAE Technical Papers | 1991
SAE Technical Papers | 1995
SAE Technical Papers | 1991