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SAE AMS4472

Aluminum Alloy, Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T34) Solution Heat Treated and Stress Relieved

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Organization: SAE
Publication Date: 1 February 2017
Status: active
Page Count: 5
scope:

Form

This specification covers an aluminum alloy in the form of plate 0.500 to 2.250 inch (12.70 to 57.15 mm) in nominal thickness (see 8.5).

Application

This plate has been used typically for aerospace structural parts requiring strength similar to that of 7475-T7351 but having 4% lower nominal density, but usage is not limited to such applications. Material is delivered in T34 temper and precipitation heat treated to obtain T82 temper by the end user.

Document History

SAE AMS4472
February 1, 2017
Aluminum Alloy, Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T34) Solution Heat Treated and Stress Relieved
Form This specification covers an aluminum alloy in the form of plate 0.500 to 2.250 inch (12.70 to 57.15 mm) in nominal thickness (see 8.5). Application This plate has been used typically for...
June 1, 2011
Aluminum Alloy, Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T34) Solution Heat Treated and Stress Relieved
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...

References

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