This standard specifies the requirements for aluminum alloy 2013 extruded bars, rods, and sections with a composition of approximately 1.0Mg, 0.80Si, 1.8Cu, and 0.20Cr in the solution heat treated, stretch straightened, and aged temper condition designated as -T6511. It outlines detailed specifications for material properties, chemical composition, mechanical performance, and manufacturing processes to ensure consistency and quality in the production of these aluminum alloy components.
*** Please note: This description may not be accurate, please refer to the official documentation.
SAE AMS4326B-2023 history
2023SAE AMS4326B-2023 Aluminum Alloy, 2013, Extruded Bar, Rod, and Profiles, 1.0Mg - 0.80Si - 1.8Cu - 0.20Cr (2013 -T6511), Solution Heat Treated, Stress-Relieved by Stretching, and Aged
2018SAE AMS4326A-2018 Aluminum Alloy@ 2013@ Extruded Bar@ Rod@ and Profiles 1.0 Mg - 0.80 Si - 1.8 Cu - 0.20 Cr (2013 -T6511) Solution Heat Treated@ Stress-Relieved by Stretching@ and Aged (UNS A92013)
2017SAE AMS4326-2017 Aluminum Alloy, 2013, Extruded Bar, Rod, and Profiles 1.0 Mg - 0.80 Si - 1.8 Cu - 0.20 Cr (2013 - T6511) Solution Heat Treated, Stress-Relieved by Stretching, and Aged
2004SAE AMS4326-2004 Aluminum Alloy, 2013, Extruded Bar, Rod, and Profiles 1.0 Mg - 0.80 Si - 1.8 Cu - 0.20 Cr (2013 -T6511) Solution Heat Treated, Stress-Relieved by Stretching, and Aged UNS A92013