SAE AMS4306B
Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T6151) Solution Heat Treated, Stress Relieved, and Aged
Historical
Standard by SAE International, 2012-09-27
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About This Item
This specification covers an aluminum alloy in the form of plate.
AMS4306B has been reaffirmed to comply with the SAE five-year review policy.
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Standard Details
- Publication Date: 2012-09-27
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Aluminum alloys, Tensile strength, Magnesium alloys, Conductivity, Quality assurance, Corrosion, Aluminum, Identification
- Official SAE: Doi link
Document History
- New Version Available: AMS4306C (2018-01-12)
- This Version: AMS4306B (2012-09-27)
- Previous Version: AMS4306A (2000-09-01)
- Previous Version: AMS4306 (1988-10-01)
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