SAE AMS4202D-2005
Aluminum Alloy Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated UNS A97475

Standard No.
SAE AMS4202D-2005
Release Date
2005
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4202D-2012
Latest
SAE AMS4202E-2019
Scope
This specification covers an aluminum alloy in the form of plate. This plate has been used typically for structural applications requiring high strength and resistance to stress-corrosion, moderate fatigue strength, and high fracture toughness, but usage is not limited to such applications.

SAE AMS4202D-2005 Referenced Document

  • ASTM B594-02 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*2024-04-18 Update
  • ASTM B645-02 Standard Practice for Plane-Strain Fracture Toughness Testing of Aluminum Alloys*2024-04-18 Update
  • ASTM B646-04 Standard Practice for Fracture Toughness Testing of Aluminum Alloys*2024-04-18 Update
  • ASTM B660-02 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-18 Update
  • ASTM E1304-97 Standard Test Method for Plane-Strain (Chevron-Notch) Fracture Toughness of Metallic Materials
  • ASTM E399-05 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness KIC of Metallic Materials*2024-04-18 Update
  • ASTM E602-03 Standard Test Method for Sharp-Notch Tension Testing with Cylindrical Specimens *2024-04-18 Update
  • ASTM E645-02 Standard Test Method for Efficacy of Microbicides Used in Cooling Systems*2024-04-18 Update
  • 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)
  • SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4202D-2005 history

  • 2019 SAE AMS4202E-2019 Aluminum Alloy Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated@ Stress Relieved by Stretching@ and Precipitation Heat Treated (UNS A97475)
  • 2012 SAE AMS4202D-2012 Aluminum Alloy Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated
  • 2005 SAE AMS4202D-2005 Aluminum Alloy Plate 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated UNS A97475
  • 1994 SAE AMS4202C-1994 ALUMINUM ALLOY PLATE 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated
  • 1989 SAE AMS4202C-1989 Aluminum Alloy, Plate, 5.7Zn 2.2Mg 1.6Cu 0.22Cr, Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated (Reaffirmed: 01 Apr 1994)
  • 1987 SAE AMS4202B-1987 ALUMINUM ALLOY PLATE 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) Solution Heat Treated@ Stress Relieved by Stretching@ and Precipitation Heat Treated (UNS A97475)
  • 1981 SAE AMS4202A-1981 ALUMINUM ALLOY PLATE 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) (UNS A97475)
  • 1978 SAE AMS4202-1978 ALUMINUM ALLOY PLATE 5.7Zn - 2.2Mg - 1.6Cu - 0.22Cr (7475-T7351) (UNS A97475)



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