SAE AMS4268-2011
Aluminum Alloy, Sheet and Plate 4.4Cu 1.5Mg 0.60Mn; (2024-T81 Sheet, -T851 Plate) Solution Heat Treated, Cold Worked and Artificially Aged

Standard No.
SAE AMS4268-2011
Release Date
2011
Published By
Society of Automotive Engineers (SAE)
Status
 2017-12
Replace By
SAE AMS4268A-2017
Latest
SAE AMS4268A-2017
Scope
This specification covers an aluminum alloy in the form of sheet and plate supplied in the -T81/-T851. These products have been used typically for high strength parts requiring higher yield strength than is afforded by naturally aged tempers of this alloy and whose fabrication does not involve welding; but usage is not limited to such applications.

SAE AMS4268-2011 Referenced Document

  • ASTM B594-09 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*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
  • 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 AMS4268-2011 history

  • 2017 SAE AMS4268A-2017 Aluminum Alloy@ Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn; (2024-T81 Sheet@ -T851 Plate) Solution Heat Treated@ Cold Worked and Artificially Aged (UNS A92024)
  • 2011 SAE AMS4268-2011 Aluminum Alloy, Sheet and Plate 4.4Cu 1.5Mg 0.60Mn; (2024-T81 Sheet, -T851 Plate) Solution Heat Treated, Cold Worked and Artificially Aged



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