SAE AMS4470-2009
Aluminum Alloy, Plate (7085-T7451) 7.5Zn 1.6Cu 1.5Mg 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
- Standard No.
- SAE AMS4470-2009
- Release Date
- 2009
- Published By
- Society of Automotive Engineers (SAE)
- Status
- Replace By
- SAE AMS4470A-2012
- Latest
- SAE AMS4470C-2018
- Scope
- This specification covers an aluminum alloy in the form of plate. This product may be used in aerospace applications requiring a high level of mechanical properties and fracture toughness, good resistance to stress-corrosion cracking and resistance to exfoliation corrosion, but usage is not limited to such applications.
SAE AMS4470-2009 history
- 2018 SAE AMS4470C-2018 Aluminum Alloy@ Plate (7085-T7451) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated@ Stress-Relieved@ and Overaged (UNS A97085)
- 2018 SAE AMS4470B-2018 Aluminum Alloy, Plate (7085-T7451) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
- 2012 SAE AMS4470A-2012 Aluminum Alloy, Plate (7085-T7451) 7.5Zn 1.6Cu 1.5Mg 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
- 2009 SAE AMS4470-2009 Aluminum Alloy, Plate (7085-T7451) 7.5Zn 1.6Cu 1.5Mg 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
