SAE AMS4313D
Aluminum Alloy, Rolled or Forged Rings 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T351, 2219-T352) Solution Heat Treated and Mechanically Stress Relieved
Historical
Standard by SAE International, 2010-01-05
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About This Item
This specification covers an aluminum alloy in the form of rolled or forged rings.
AMS4313D removes hardness as a technical requirement and results from a Five Year Review and update of this specification.
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Standard Details
- Publication Date: 2010-01-05
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Aluminum alloys, Heat treatment, Magnesium alloys, Alloys, Tensile strength, Identification numbers, Aluminum, Magnesium, Manganese
- Official SAE: Doi link
Document History
- New Version Available: AMS4313F (2022-11-14)
- Previous Version: AMS4313E (2016-12-14)
- This Version: AMS4313D (2010-01-05)
- Previous Version: AMS4313C (2006-04-24)
- Previous Version: AMS4313B (1994-05-01)
- Previous Version: AMS4313A (1988-10-01)
- Previous Version: AMS4313 (1977-01-15)
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