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D14AD - Aluminum Alloy, Extrusion 3.7 Cu-1.15 Li - 0.50 Zn -0.40 Mg, 0.30 Mn - 0.10 Zr Solution Heat Treated, Stress Relieved by Stretching 2% to 5% and Aged

Details
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Document Number: D14AD
Project Initiation: 04-17-2014
Project Number: PN14-50
Revision Number:
Sponsor Name: Rebecca K. Wyss
Title
Aluminum Alloy, Extrusion 3.7 Cu-1.15 Li - 0.50 Zn -0.40 Mg, 0.30 Mn - 0.10 Zr Solution Heat Treated, Stress Relieved by Stretching 2% to 5% and Aged
Scope
Form: This specification covers an aluminum alloy in the form of an extrusion. Application: This product has been used in aerospace applications requiring a combination of high strength and compressive properties and with good corrosion resistance, but usage is not limited to such applications.
Rationale
This SAE Aerospace Material Specification is intended to provide technical requirements such as composition and mechanical properties as well as Quality Assurance provisions for 2055-T84 aluminum extrusion.
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