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SAE AMS4089

Revision E, July 1, 2014

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Aluminum Alloy, Plate 1.6Cu - 2.2Mg - 0.22Cr - 5.7Zn (7475-T7651) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated



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Product Details:

  • Revision: Revision E, July 1, 2014
  • Published Date: July 2014
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 5
  • ANSI Approved: No
  • DoD Adopted: Yes

Description / Abstract:

Form

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

Application

This plate has been used typically for structural applications requiring material with high strength and resistance to exfoliation-corrosion, moderate fatigue strength, and high fracture-toughness, but usage is not limited to such applications.

AIA/NAS Aerospace Standards