Aluminum Alloy, Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T34) Solution Heat Treated and Stress Relieved
|Publication Date:||1 February 2017|
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).
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.