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SAE AMS4342 Revision E, August 1, 2007
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Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T74511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged
Includes all amendments and changes through Reaffirmation Notice , September 2012
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AIA/NAS Aerospace Standards

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.


These products have been used typically for structural applications requiring a combination of high mechanical properties and good resistance to stress-corrosion cracking, but usage is not limited to such applications.