SAE AMS4413
Aluminum Alloy, Plate 3.5 Cu - 1.0Li - .40Mg - .35 Mn - .45Ag - 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged
Historical
Standard by SAE International, 2007-10-31
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About This Item
This specification covers an aluminum-lithium alloy in the form of plate.
AMS 4413 is a proposed draft of a new material specification which covers aluminum-lithium alloy 2050-T84.
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Standard Details
- Publication Date: 2007-10-31
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Aluminum alloys, Magnesium alloys, Tensile strength, Quality assurance, Test procedures, Aluminum, Magnesium, Identification
- Official SAE: Doi link
Document History
- New Version Available: AMS4413C (2023-12-20)
- Previous Version: AMS4413B (2019-05-10)
- Previous Version: AMS4413A (2012-12-20)
- This Version: AMS4413 (2007-10-31)
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