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SAE AMS4050

Revision J, December 1, 2014

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Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged



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Product Details:

  • Revision: Revision J, December 1, 2014
  • Published Date: December 2014
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 8
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form

This specification covers an aluminum alloy in the form of plate

This specification covers products from 0.250 to 8.000 inches (6 to 203 mm) in thickness, inclusive (See 8.4).

Application

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