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SAE AMS4303

Revision C, April 2017

Complete Document

Aluminum Alloy Plate 2.7Cu - 2.2Li - 0.12Zr (2090-T81) Solution Heat Treated, Cold Worked, and Aged

Includes all amendments and changes through Stabilization Notice (No longer revised / updated) , April 2017


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Product Details:

  • Revision: Revision C, April 2017
  • Published Date: April 2017
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 7
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form:

This specification covers an aluminum alloy in the form of plate.

Application:

This plate has been used typically for aerospace structural parts requiring strength similar to that of 7075-T651 but having 7.8% lower nominal density, but usage is not limited to such applications.
AIA/NAS Aerospace Standards