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SAE AMS4328
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SAE AMS4328 Revision A, July 1, 2006
Aluminum Alloy, Plate (2397-T87) 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn
Solution Heat Treated, Cold Worked, and Artificially Aged
Description / Abstract:
Form:
This specification covers an aluminum alloy in the form of plate.
Application
This product has been used typically in aerospace applications where low density is needed in combination with moderate strength, high fatigue resistance, good stress corrosion properties, and improved stiffness, but usage is not limited to such applications.
This specification covers an aluminum alloy in the form of plate.
Application
This product has been used typically in aerospace applications where low density is needed in combination with moderate strength, high fatigue resistance, good stress corrosion properties, and improved stiffness, but usage is not limited to such applications.
SAE AMS4328 Revision A, July 1, 2006
Aluminum Alloy, Plate (2397-T87) 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn
Solution Heat Treated, Cold Worked, and Artificially Aged