SAE 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
This specification covers an aluminum alloy in the form of extruded bars, rods, and integrated profiles. These extrusions have been used typically for parts requiring high strength, good toughness and fatigue properties and good maximum corrosion resistance, but usage is not limited to such applications.
SAE AMS4326-2004 Referenced Document
ASTM B594-02 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications
ASTM B660-02 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products
ASTM B666/B666M-01 Standard Practice for Identification Marking of Aluminum and Magnesium Products
ASTM G34-01 Standard Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test)
SAE AMS2355G-2002 Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloys Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings
SAE AMS2772-1997 Heat Treatment of Aluminum Alloy Raw Materials (01 1997)
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