SAE AMS4050K
Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged
Latest
Standard by SAE International, 2021-04-22
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| AMS4050K.pdf |
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About This Item
This specification covers an aluminum alloy in the form of plate.
AMS4050K prohibits unauthorized exceptions (3.3.1.1, 3.7, 4.4.1, 5.1.3, 8.5, 8.6), adds AS6279 controls (3.6), adds SI tensile elongation values and testing option (Table 2, 8.3), allows the use of immediate prior revision of document (8.4), and results from a Five-Year Review and update of this specification.
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Standard Details
- Publication Date: 2021-04-22
- Standard Status: latest
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Metals, Materials properties, Aluminum alloys, Tensile strength, Magnesium alloys, Fatigue, Conductivity, Wrought alloys
- Official SAE: Doi link
Document History
- This Version: AMS4050K (2021-04-22)
- Previous Version: AMS4050J (2014-12-22)
- Previous Version: AMS4050H (2011-11-03)
- Previous Version: AMS4050G (2000-06-01)
- Previous Version: AMS4050F (1998-11-01)
- Previous Version: AMS4050E (1992-07-01)
- Previous Version: AMS4050D (1991-10-01)
- Previous Version: AMS4050C (1984-10-01)
- Previous Version: AMS4050B (1984-04-01)
- Previous Version: AMS4050A (1977-07-15)
- Previous Version: AMS4050 (1974-12-15)
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