AS7482 Studs, Corrosion and Heat Resistant Steel, UNS S66286, Tensile Strength 130 ksi, 1800 °F Solution Heat Treated, Aged Before Roll Threading Procurement Specification
08/16/2011
- Issuing Committee
- Content
- This specification covers aircraft quality studs amde 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.
- Pages
- 21
- Citation
- SAE International Technical Standard, Studs, Corrosion and Heat Resistant Steel, UNS S66286, Tensile Strength 130 ksi, 1800 °F Solution Heat Treated, Aged Before Roll Threading Procurement Specification, SAE Standard AS7482, Reaffirmed August 2011, https://doi.org/10.4271/AS7482.