SAE AMS4599-2011
Aluminum Alloy, Sheet and Plate 6.3Cu 0.30Mn 0.06Ti 0.10V 0.18Zr Solution and Precipitation Heat Treated (2219-T81/-T851)

Standard No.
SAE AMS4599-2011
Release Date
2011
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4599A-2017
Latest
SAE AMS4599B-2023
Scope
This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for parts requiring high strength up to 500 φF (260 φC), but usage is not limited to such applications. Product may be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

SAE AMS4599-2011 Referenced Document

  • ASTM B594-09 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*2024-04-19 Update
  • SAE AMS2355 TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
  • 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 AS1990-1990 Aluminum Alloy Tempers

SAE AMS4599-2011 history

  • 2023 SAE AMS4599B-2023 Aluminum Alloy, Sheet, and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution and Precipitation Heat Treated (2219 -T81/-T851)
  • 2017 SAE AMS4599A-2017 Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr Solution and Precipitation Heat Treated (2219 -T81/-T851)
  • 2011 SAE AMS4599-2011 Aluminum Alloy, Sheet and Plate 6.3Cu 0.30Mn 0.06Ti 0.10V 0.18Zr Solution and Precipitation Heat Treated (2219-T81/-T851)



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