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BOLTS AND SCREWS, STEEL, CORROSION AND HEAT RESISTANT Upset Headed, Heat Treated, Roll Threaded 1800°F Solution and Precipitation Heat Treated
- Aerospace Standard
Published December 05, 1990 by SAE International in United States
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant precipitation 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.
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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