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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Superseded By: SAE AMS4617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
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 parts requiring high strength and resistance to stresscorrosion cracking, but usage is not limited to such applications.