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BOLTS AND SCREWS, NICKEL ALLOY, CORROSION AND HEAT RESISTANT Forged Head, Roll Threaded, Fatigue Rated
- Aerospace Standard
Published January 22, 1991 by SAE International in United States
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.
Data Sets - Support Documents
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E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
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