SAE AMS4338A-2007
Aluminum Alloy, Extrusions 4.0Cu - 1.3Mg - 0.60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by Stretching UNS A92026

Standard No.
SAE AMS4338A-2007
Release Date
2007
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4338A-2012
Latest
SAE AMS4338B-2018
Scope
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes). These extrusions have been used typically for machined parts requiring dimensional stability during machining processes and for parts requiring high strength and damage tolerance, where fabrication does not normally involve welding, but usage is not limited to such applications. Certain processing procedures may cause this product to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

SAE AMS4338A-2007 Referenced Document

  • ASTM B594-06 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*2024-04-18 Update
  • ASTM B660-02 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-18 Update
  • ASTM B666/B666M-01 Standard Practice for Identification Marking of Aluminum and Magnesium Products*2024-04-18 Update
  • SAE AMS2355H-2005 Quality Assurance Sampling and Testing of 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)
  • SAE ARP823 MINIMIZING STRESS CORROSION IN WROUGHT HEAT TREATABLE ALUMINUM ALLOY PRODUCTS
  • SAE ARP823D-1997 Minimizing Stress-Corrosion in Wrought Heat-Treatable Aluminum Alloy Products
  • SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4338A-2007 history

  • 2018 SAE AMS4338B-2018 Aluminum Alloy@ Extrusions 4.0Cu - 1.3Mg - 0.60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by Stretching (UNS A92026)
  • 2012 SAE AMS4338A-2012 Aluminum Alloy, Extrusions 4.0Cu - 1.3Mg - 0.60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by Stretching
  • 2007 SAE AMS4338A-2007 Aluminum Alloy, Extrusions 4.0Cu - 1.3Mg - 0.60Mn (2026-T3511) Solution Heat Treated and Stress Relieved by Stretching UNS A92026
  • 2001 SAE AMS4338-2001 Aluminum Alloy@ Extrusions (2026-T3511) 4.0Cu - 1.3Mg - 0.60Mn Solution Heat Treated and Stress Relieved by Stretching (UNS A92026)



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