Aluminum Alloy, Sheet and Plate, 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T8), Solution Heat Treated, Cold Worked, and Artificially Aged

Standard:
Issued:
  • 2012-10-19
 
  • HISTORICAL Access the latest revision: AMS4474A
Publisher:
  • SAE International
Pages:
4
Scope:

This product has been used typically for aerospace srructural parts requiring strength similar to that of 7475-T7351 but having 4% lower nominal density, but usage is not limited to such applications.

Rationale:

This is a new material specification which covers aluminum-lithium alloy 2195-T8 in the form of sheet and plate.

History:
Standard Published Revision Status
AMS4474A 2015-08-12 Latest Revised
2012-10-19 Historical Issued
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