SAE AS7471A

Bolts and Screws, Nickel Alloy, UNS N07001 Tensile Strength 165 ksi, Corrosion and Heat Resistant, Procurement Specification.

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Standard:
  • AS7471
  • Revision: A
Revised:
  • 1995-09-01
Revision:
  • Historical. Access the latest revision: AS7471F
Issuing:
  • E-25 General Standards For Aerospace And Propulsion Systems
Scope:

This procurement specification 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:AS7471165 ksi minimum ultimate tensile strength at room temperature. 75 ksi stress-rupture strength at 1350 °F.AS7471-1165 ksi minimum ultimate tensile strength at room temperature . 99 ksi minimum ultimate shear strength at room temperature.Primarily for aerospace propulsion systems applications where a good combination of tensile strength, and resistance to relaxation at elevated temperatures up to approximately 1500 °F is required.

History:
StandardPublishedRevisionStatus
AS7471F2013-01-15LatestRevised
AS7471E2009-07-16HistoricalRevised
AS7471D2007-08-29HistoricalRevised
AS7471C2006-01-13HistoricalRevised
AS7471B1997-07-01HistoricalReaffirmed
AS7471A1995-09-01HistoricalRevised
AKA:
  • SAE AS 7471
Sector:
  • Aerospace
Topic:
  • Nickel
  • Parts
  • Gas turbines
  • Hybrid engines
  • Jet engines

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