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SAE AMS4166

Revision G, January 1, 2012

Complete Document

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


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Detail Summary

Superseded By: SAE AMS4617

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Additional Comments:
CNCL S/S BY SAE AMS4617
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Product Details:

  • Revision: Revision G, January 1, 2012
  • Published Date: January 2012
  • Status: Superseded By:
  • Superseded By: SAE AMS4617
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 9
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

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.

AIA/NAS Aerospace Standards