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SAE AMS4232

Revision C, October 1, 2012

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Aluminum Alloy Extrusions 2.7Cu - 2.2Li - 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated



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Product Details:

  • Revision: Revision C, October 1, 2012
  • Published Date: October 2012
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 5
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form

This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles.

Application

These extrusions have been used typically for parts in structural applications requiring strength similar to 7050-T6 alloy with good exfoliation resistance and with a lower density of approximately 7.8%, but usage is not limited to such applications.

AIA/NAS Aerospace Standards