• AS7471
• Revision: B

• 2001-10-01

• 1997-07-01

• Historical. Access the latest revision: AS7471F

• E-25 General Standards For Aerospace And Propulsion Systems

This document covers 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 N07001. The following specification designations and their properties are covered: AS7471 165 ksi minimum ultimate tensile strength at room temperature, 75 ksi stress-rupture strength at 1350° F and AS7471-1 165 ksi minimum ultimate tensile strength at room temperature, 99 ksi minimum ultimate shear strength at room temperature. Primarily for aerospace propulsion system applications where a good combination of tensile strength, and resistance to relaxation at elevated temperatures up to approximately 1500°F is required.

• SAE AS 7471

• Aerospace

• Nickel
• Parts
• Gas turbines
• Hybrid engines
• Jet engines