SAE AMS4166G PDF

SAE AMS4166G PDF

Name:
SAE AMS4166G PDF

Published Date:
01/09/2012

Status:
Active

Description:

Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution Heat Treated and Overaged

Publisher:
SAE International

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Russian version):
200 business days

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$24.9
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This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of January 2012 and has been superseded by SAE AMS 4617. The requirements of the latest issue of SAE AMS 4617 shall be fulfilled whenever reference is made to the cancelled AMS 4166. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Materials Specifications, noting that it has been superseded by SAE AMS 4617.

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 stress-corrosion cracking, but usage is not limited to such applications.
File Size : 1 file , 1.6 MB
Note : This product is unavailable in Ukraine, Russia, Belarus
Published : 01/09/2012

History

SAE AMS4166G
Published Date: 01/09/2012
Aluminum Alloy, Extrusions 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution Heat Treated and Overaged
$24.9
SAE AMS4166F
Published Date: 07/01/2003
Aluminum Alloy, Extrusions 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T73) Solution Heat Treated and Overaged ( Reaffirmed: May 2008 )
$21

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