SAE AMS4025L
Aluminum Alloy, Sheet and Plate 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-0) Annealed
Historical
Standard by SAE International, 2008-07-15
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About This Item
This specification covers an aluminum alloy in the form of sheet and plate.
AMS4025L is a limited scope change to correct the omission of appropriate tensile and bend properties for -T42 material and the full range of tensile properties (to 4 inch thickness) for -T62 material. Amended per Spring 2008 Committee D Minutes.
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Standard Details
- Publication Date: 2008-07-15
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Aluminum alloys, Magnesium alloys, Tensile strength, Identification, Production, Aluminum, Magnesium,
- Official SAE: Doi link
Document History
- New Version Available: AMS4025N (2020-07-14)
- Previous Version: AMS4025M (2014-11-07)
- This Version: AMS4025L (2008-07-15)
- Previous Version: AMS4025K (2005-01-24)
- Previous Version: AMS4025J (2001-11-19)
- Previous Version: AMS4025 (1994-07-01)
- Previous Version: AMS4025H (1989-07-01)
- Previous Version: AMS4025G (1981-10-01)
- Previous Version: AMS4025F (1974-12-01)
- Previous Version: AMS4025E (1968-11-01)
- Previous Version: AMS4025C (1957-01-01)
- Previous Version: AMS4025D (1954-01-01)
- Previous Version: AMS4025B (1951-10-01)
- Previous Version: AMS4025A (1946-04-01)
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