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SAE AMS4200

Revision C, June 2017

Complete Document

Aluminum Alloy Plate 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T7351) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

Includes all amendments and changes through Stabilization Notice (No longer revised / updated) , June 2017


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Product Details:

  • Revision: Revision C, June 2017
  • Published Date: June 2017
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 7
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form:

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

Application:

This product has been used typically for parts requiring high strength and resistance to stress-corrosion, but usage is not limited to such applications
AIA/NAS Aerospace Standards