Bolts and Screws, Steel, UNS S66286 1650 °F Solution Heat Treated Precipitation Heat Treated Before Roll Threaded
- Aerospace Standard
This specification covers bolts and screws made from a corrosion and heat resistant age 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.
Primarily for aerospace propulsion system applications where a good combination of strength and resistance to relaxation at elevated temperatures is required.
|Aerospace Standard||Bolts and Screws, Steel, UNS S66286 1650 °F Solution Heat Treated Precipitation Heat Treated Before Roll Threaded|
|Aerospace Material Specification||BOLTS AND SCREWS, LOW-ALLOY STEEL Heat Treated, Roll Threaded|
|Aerospace Material Specification||Bolts and Screws, Titanium Alloy 6al 4v, Upset Headed, Heat Treated, Roll Threaded|
Data Sets - Support Documents
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.