SAE AMS4328A-2006
Aluminum Alloy, Plate (2397-T87) 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn Solution Heat Treated, Cold Worked, and Artificially Aged UNS A92397

Standard No.
SAE AMS4328A-2006
Release Date
2006
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4328A-2013
Latest
SAE AMS4328B-2019
Scope
This specification covers an aluminum alloy in the form of plate. This product has been used typically in aerospace applications where low density is needed in combination with moderate strength, high fatigue resistance, good stress corrosion properties, and improved stiffness, but usage is not limited to such applications.

SAE AMS4328A-2006 Referenced Document

  • ASTM B594-02 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*2024-04-18 Update
  • ASTM B594-06 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 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
  • ASTM E1251-04 Test Method for Analysis of Aluminum and Aluminum Alloys by Atomic Emission Spectrometry*2024-04-18 Update
  • ASTM E399-05 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness KIC of Metallic Materials*2024-04-18 Update
  • ASTM E399-06 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials*2006-12-15 Update
  • ASTM G34-01 Standard Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test)*2024-04-18 Update
  • ASTM G47-98 Standard Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum Alloy Products
  • 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 AS1990-1990 Aluminum Alloy Tempers

SAE AMS4328A-2006 history

  • 2019 SAE AMS4328B-2019 Aluminum Alloy, Plate (2397-T87) 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn Solution Heat Treated, Cold Worked, and Artificially Aged
  • 2013 SAE AMS4328A-2013 Aluminum Alloy, Plate (2397-T87) 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn Solution Heat Treated, Cold Worked, and Artificially Aged
  • 2006 SAE AMS4328A-2006 Aluminum Alloy, Plate (2397-T87) 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn Solution Heat Treated, Cold Worked, and Artificially Aged UNS A92397
  • 2003 SAE AMS4328-2003 Aluminum Alloy, Plate (2397-T87) 2.8Cu 1.4Li 0.30Mn 0.12Zr 0.10Zn Solution Heat Treated, Cold Worked, and Artificially Aged



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