SAE AMS4303B-2000
Aluminum Alloy Plate, 2.7Cu 2.2Li 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged

Standard No.
SAE AMS4303B-2000
Release Date
2000
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4303B-2007
Latest
SAE AMS4303C-2017
Scope
This specification covers an aluminum alloy in the form of plate. This plate has been used typically for aerospace structural parts requiring strength similar to that of 7075-T651 but having 7.8% lower nominal density, but usage is not limited to such applications. This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 2007. It is recommended, therefore, that this specification not be specified for new designs. NONCURRENT refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs.

SAE AMS4303B-2000 history

  • 2017 SAE AMS4303C-2017 Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated@ Cold Worked@ and Aged
  • 2012 SAE AMS4303B-2012 Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
  • 2007 SAE AMS4303B-2007 Aluminum Alloy Plate, 2.7Cu - 2.2Li - 0.12Zr (2090-T81), Solution Heat Treated, Cold Worked, and Aged
  • 2000 SAE AMS4303B-2000 Aluminum Alloy Plate, 2.7Cu 2.2Li 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
  • 2000 SAE AMS4303A-2000 Aluminum Alloy Plate, 2.7Cu 2.2Li 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
  • 1994 SAE AMS4303-1994 ALUMINUM ALLOY PLATE 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
  • 1990 SAE AMS4303-1990 Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated@ Cold Worked@ and Aged



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