SAE AMS4464-2012
Aluminum Alloy Plate (2624-T351) 4.1Cu 1.4Mg 0.6Mn Solution Heat Treated, Cold Worked and Naturally Aged

Standard No.
SAE AMS4464-2012
Release Date
2012
Published By
Society of Automotive Engineers (SAE)
Status
 2017-10
Replace By
SAE AMS4464A-2017
Latest
SAE AMS4464A-2017
Scope
This specification covers an aluminum alloy in the form of plate. This product has been used typically for structural parts requiring a high level of mechanical properties and good damage tolerance, but usage is not limited to such applications.

SAE AMS4464-2012 Referenced Document

  • ASTM B594-09 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*2024-04-19 Update
  • ASTM B645-10 Standard Practice for Linear-Elastic Plane-Strain Fracture Toughness Testing of Aluminum Alloys*2024-04-19 Update
  • ASTM B646-06 Standard Practice for Fracture Toughness Testing of Aluminum Alloys*2024-04-19 Update
  • ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-19 Update
  • ASTM B666/B666M-08 Standard Practice for Identification Marking of Aluminum and Magnesium Products*2024-04-19 Update
  • ASTM E399-09 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials*2024-04-19 Update
  • ASTM E561-10 Standard Test Method forK-R Curve Determination*2024-04-19 Update
  • SAE AMS2355 TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
  • SAE AMS2772-1997 Heat Treatment of Aluminum Alloy Raw Materials (01 1997)
  • SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4464-2012 history

  • 2017 SAE AMS4464A-2017 Aluminum Alloy Plate (2624-T351) 4.1Cu - 1.4Mg - 0.6Mn Solution Heat Treated@ Cold Worked and Naturally Aged (UNS A92624)
  • 2012 SAE AMS4464-2012 Aluminum Alloy Plate (2624-T351) 4.1Cu 1.4Mg 0.6Mn Solution Heat Treated, Cold Worked and Naturally Aged



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