SAE AMS4343G-2024
Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged

Standard No.
SAE AMS4343G-2024
Release Date
2024
Published By
Society of Automotive Engineers (SAE)
Latest
SAE AMS4343G-2024
 

Scope
This specification covers extruded bars, rods, wire, shapes, and tubes of aluminum alloys having a nominal diameter or minimum thickness (see 8.5) not exceeding 5.000 in. (127.00 mm). These extrusions are generally used for structural components requiring high strength, moderate fatigue strength, good stress corrosion resistance, and good fracture toughness, but use is not limited to such applications.

SAE AMS4343G-2024 Referenced Document

  • ANSI H35.2 American National Standard Dimensional Tolerances for Aluminum Mill Products
  • ANSI H35.2M Dimensional Tolerances for Aluminum Mill Products (Metric)
  • ASTM B594 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications
  • ASTM B660 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products
  • ASTM B666/B666M Standard Practice for Identification Marking of Aluminum and Magnesium Products
  • ASTM E399 Standard Test Method for Plane-Strain Fracture Toughness of Metallic Materials
  • ASTM G47 Standard Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum Alloy Products

SAE AMS4343G-2024 history

  • 2024 SAE AMS4343G-2024 Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged
  • 2018 SAE AMS4343F-2018 Aluminum Alloy@ Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated@ Stress Relieved by Stretching@ and Overaged (UNS A97149)
  • 2018 SAE AMS4343E-2018 Aluminum Alloy@ Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated@ Stress Relieved by Stretching@ and Overaged (UNS A97149)
  • 2012 SAE AMS4343D-2012 Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged
  • 2004 SAE AMS4343D-2004 Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged UNS A97149
  • 1996 SAE AMS4343C-1996 Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged (UNS A97149)
  • 1989 SAE AMS4343B-1989 ALUMINUM ALLOY@ EXTRUSIONS 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated@ Stress Relieved and Overaged (UNS A97149)
  • 1987 SAE AMS4343A-1987 ALUMINUM ALLOY@ EXTRUSIONS 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated@ Stress Relieved and Overaged (UNS A97149)
  • 1980 SAE AMS4343-1980 ALUMINUM ALLOY@ EXTRUSIONS 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511)
Aluminum Alloy, Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7149-T73511) Solution Heat Treated, Stress Relieved by Stretching, and Overaged

Standard and Specification




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