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SAE AMS4416

Aluminum Alloy, Extruded Profiles (2196-T8511) 2.9Cu - 1.7Li - 0.4Mg - 0.4Ag - 0.10Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged

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Organization: SAE
Publication Date: 1 May 2017
Status: active
Page Count: 5
scope:

Form

This specification covers an aluminum-lithium alloy in the form of extruded profiles 0.040 to 1.000 inch, incl in thickness.

Application

These extrusions have been used typically for machined parts requiring dimensional stability during machining processes, and high strength, but usage is not limited to such applications.

Certain processing procedures may cause this product to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Document History

SAE AMS4416
May 1, 2017
Aluminum Alloy, Extruded Profiles (2196-T8511) 2.9Cu - 1.7Li - 0.4Mg - 0.4Ag - 0.10Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged
Form This specification covers an aluminum-lithium alloy in the form of extruded profiles 0.040 to 1.000 inch, incl in thickness. Application These extrusions have been used typically for machined...
October 1, 2012
Aluminum Alloy, Extruded Profiles (2196-T8511) 2.9Cu - 1.7Li - 0.4Mg - 0.4Ag - 0.10Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged
Form This specification covers an aluminum-lithium alloy in the form of extruded profiles. Application These extrusions have been used typically for machined parts requiring dimensional stability...
July 1, 2008
Aluminum Alloy, Extruded Profiles (2196-T8511) 2.9Cu - 1.7Li - 0.4Mg - 0.4Ag - 0.10Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged
Form This specification covers an aluminum-lithium alloy in the form of extruded profiles. Application These extrusions have been used typically for machined parts requiring dimensional stability...

References

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