SAE AMS4413A-2012
Aluminum Alloy, Plate 3.5 Cu 1.0Li 0.40Mg 0.35Mn 0.45Ag 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged

Standard No.
SAE AMS4413A-2012
Release Date
2012
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4413B-2019
Latest
SAE AMS4413C-2023
Scope
This specification covers an aluminum-lithium alloy in the form of plate. This plate has been used typically for parts where low density is needed in combination with a high level of mechanical properties and very good resistance to stress-corrosion cracking, but usage is not limited to such applications.

SAE AMS4413A-2012 Referenced Document

  • ASTM B594-09 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*2024-04-20 Update
  • ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-20 Update
  • ASTM B666/B666M-08 Standard Practice for Identification Marking of Aluminum and Magnesium Products*2024-04-20 Update
  • ASTM E399-09 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials*2024-04-20 Update
  • ASTM G47-98 Standard Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum Alloy Products
  • 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 AMS4413A-2012 history

  • 1970 SAE AMS4413C-2023 Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged
  • 2019 SAE AMS4413B-2019 Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged
  • 2012 SAE AMS4413A-2012 Aluminum Alloy, Plate 3.5 Cu 1.0Li 0.40Mg 0.35Mn 0.45Ag 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged
  • 2007 SAE AMS4413-2007 Aluminum Alloy@ Plate 3.5 Cu - 1.0Li - .40Mg - .35 Mn - .45Ag - 0.12Zr (2050-T84) Solution Heat Treated@ Stress Relieved@ and Artificially Aged (UNS A92050)



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