SAE AMS4162E
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, 2014-09-19
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About This Item
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing under 3.00 inches (76.2 mm) in diameter, least thickness, or wall thickness and 25 in2 (161 cm2) or less in cross-sectional area (See 8.5).
AMS4162E revises Composition (3.1.1), Properties (3.3.1), and Reports (4.4.1), and is a Five Year Review and update of this specification.
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Standard Details
- Publication Date: 2014-09-19
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Aluminum alloys, Magnesium alloys, Coatings, colorants, and finishes, Wrought alloys, Extrusion, Tensile strength, Heat treatment, ,
- Official SAE: Doi link
Document History
- New Version Available: AMS4162G (2025-04-14)
- Previous Version: AMS4162F (2020-07-01)
- This Version: AMS4162E (2014-09-19)
- Previous Version: AMS4162D (2008-05-01)
- Previous Version: AMS4162C (1998-03-01)
- Previous Version: AMS4162B (1990-04-01)
- Previous Version: AMS4162A (1977-01-01)
- Previous Version: AMS4162 (1968-05-01)
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