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SAE AMS4303

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

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Organization: SAE
Publication Date: 1 April 2017
Status: active
Page Count: 7
scope:

Form:

This specification covers an aluminum alloy in the form of plate.

Application:

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.

Document History

SAE AMS4303
April 1, 2017
Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
Form: This specification covers an aluminum alloy in the form of plate. Application: This plate has been used typically for aerospace structural parts requiring strength similar to that of...
April 1, 2007
Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
Form: This specification covers an aluminum alloy in the form of plate. Application: This plate has been used typically for aerospace structural parts requiring strength similar to that of...
April 1, 2007
Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
Form This specification covers an aluminum alloy in the form of plate. Application This plate has been used typically for aerospace structural parts requiring strength similar to that of 7075-T651...
August 1, 2000
Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
SCOPE: Form: This specification covers an aluminum alloy in the form of plate. Application: This plate has been used typically for aerospace structural parts requiring strength similar to that of...
January 1, 1990
Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged
A description is not available for this item.

References

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