SAE AMS4050J
Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged
Historical
Standard by SAE International, 2014-12-22
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| AMS4050J.pdf |
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About This Item
This specification covers an aluminum alloy in the form of plate.
AMS4050J revises Properties (3.3.1.1, Tables 2 and 3), Fracture Toughness Testing (3.3.5, Table 3), Fatigue Specimen Finishing (3.3.6.2), Acceptance Tests (4.2.1) Sampling and Testing (4.3.2), Reports (4.4.1), and is a Five Year Review and update of this specification.
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Standard Details
- Publication Date: 2014-12-22
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Aluminum alloys, Magnesium alloys, Tensile strength, Conductivity, Quality assurance, Identification, Corrosion,
- Official SAE: Doi link
Document History
- New Version Available: AMS4050K (2021-04-22)
- This 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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