SAE AMS4162C
Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T8511) Solution Treated, Stress Relief Stretched, Straightened, and Precipitation Heat Treated
Historical
Standard by SAE International, 1998-03-01
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About This Item
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
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Standard Details
- Publication Date: 1998-03-01
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Aluminum alloys, Magnesium alloys, Extrusion, Coatings, colorants, and finishes, Tensile strength, Heat treatment, Welding, ,
- Official SAE: Doi link
Document History
- New Version Available: AMS4162G (2025-04-14)
- Previous Version: AMS4162F (2020-07-01)
- Previous Version: AMS4162E (2014-09-19)
- Previous Version: AMS4162D (2008-05-01)
- This Version: AMS4162C (1998-03-01)
- Previous Version: AMS4162B (1990-04-01)
- Previous Version: AMS4162A (1977-01-01)
- Previous Version: AMS4162 (1968-05-01)
Please request information about the document. Contact Page
