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SAE AMS4204

Revision C, January 1, 2003

Complete Document

Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7651) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

Includes all amendments and changes through Reaffirmation Notice , May 2013


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Product Details:

  • Revision: Revision C, January 1, 2003
  • Published Date: May 2013
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 9
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form:

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

Application:

This plate has been used typically for parts requiring higher tensile strength than AMS 4203 (7010-T7351) or AMS 4205 (7010-T7451), resistance to exfoliation corrosion, and fracture toughness, but usage is not limited to such applications.
AIA/NAS Aerospace Standards