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SAE AMS4166 Revision G, January 1, 2012
Complete Document
Superseded By: SAE AMS4617
Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution Heat Treated and Overaged
Includes all amendments and changes through Cancellation Notice , January 2012
Additional Comments: CNCL S/S BY SAE AMS4617
Page Count:9
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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 parts requiring high strength and resistance to stresscorrosion cracking, but usage is not limited to such applications.