SAE AMS4329B-2017
Aluminum Alloy@ Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated@ Stress-Relieved@ and Overaged (UNS A97085)
- Standard No.
- SAE AMS4329B-2017
- Release Date
- 2017
- Published By
- SAE - SAE International
- Latest
- SAE AMS4329B-2017
- Scope
- Form This specification covers an aluminum alloy in the form of plate 4.001 to 7.000 inch@ incl. (101.62 to 177.80 mm@ incl.) in thickness. Application This product has been used in aerospace applications requiring a high level of mechanical properties and fracture toughness@ moderate resistance to stress-corrosion cracking and resistance to exfoliation corrosion@ but usage is not limited to such applications.
SAE AMS4329B-2017 history
- 2017 SAE AMS4329B-2017 Aluminum Alloy@ Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated@ Stress-Relieved@ and Overaged (UNS A97085)
- 2011 SAE AMS4329A-2011 Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged
- 2006 SAE AMS4329A-2006 Aluminum Alloy, Plate (7085-T7651) 7.5Zn - 1.6Cu - 1.5Mg - 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged UNS A97085
- 2003 SAE AMS4329-2003 Aluminum Alloy, Plate (7085-T7651) 7.5Zn 1.6Cu 1.5Mg 0.12ZrSolution Heat Treated, Stress-Relieved, and Overaged
