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SAE AMS4468

2012 Edition, January 1, 2012

Complete Document

Aluminum Alloy, Plate 5.0Cu - 0.4Mn - 0.5Mg - 0.4Ag (2139-T84) Solution Heat Treated, Cold Worked, and Artificially Aged

Includes all amendments and changes through Reaffirmation Notice , September 2017


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Product Details:

  • Revision: 2012 Edition, January 1, 2012
  • Published Date: September 2017
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 6
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form

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

Application

This product has been used typically for parts requiring a high level of mechanical properties and good resistance to stress-corrosion cracking, but usage is not limited to such applications.
AIA/NAS Aerospace Standards