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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
Form

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

Application

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.