• AS7479
• Revision: D

• 2013-09-26

• E-25 General Standards For Aerospace And Propulsion Systems

This specification covers 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.

• SAE AS 7479

• Aerospace

• Heat treatment
• Steel
• Parts
• Fasteners
• Gas turbines
• Hybrid engines
• Jet engines