SAE AMS4415A-2008
Aluminum Alloy Extrusions 8.9Zn 2.2Cu 2.2Mg 0.15Zr (7136-T76511, -T76510) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged

Standard No.
SAE AMS4415A-2008
Release Date
2008
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4415A-2015
Latest
SAE AMS4415B-2021
Scope
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles (shapes) and tubing. These extrusions have been used typically for structural applications requiring a combination of high tensile and compressive strength and good corrosions resistance, but usage is not limited to such applications. Certain processing procedures may cause this product to become susceptible to stress-corrosion cracking; ARP 823 recommends practices to minimize such conditions.

SAE AMS4415A-2008 Referenced Document

  • ASTM B594-06 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*2024-04-19 Update
  • ASTM B660-02 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-19 Update
  • ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-19 Update
  • ASTM B666/B666M-08 Standard Practice for Identification Marking of Aluminum and Magnesium Products*2024-04-19 Update
  • ASTM E1004-02 Standard Practice for Determining Electrical Conductivity Using the Electromagnetic (Eddy-Current) Method*2024-04-19 Update
  • ASTM G34-01 Standard Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test)*2024-04-19 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 ARP823 MINIMIZING STRESS CORROSION IN WROUGHT HEAT TREATABLE ALUMINUM ALLOY PRODUCTS
  • SAE ARP823E-2007 Minimizing Stress-Corrosion Cracking in Wrought Heat-Treatable Aluminum Alloy Products
  • SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4415A-2008 history

  • 2021 SAE AMS4415B-2021 Aluminum Alloy Extrusions 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T76511, -T76510) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged
  • 2015 SAE AMS4415A-2015 Aluminum Alloy Extrusions 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T76511, -T76510) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged
  • 2008 SAE AMS4415A-2008 Aluminum Alloy Extrusions 8.9Zn 2.2Cu 2.2Mg 0.15Zr (7136-T76511, -T76510) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged
  • 2008 SAE AMS4415-2008 Aluminum Alloy Extrusions 8.9Zn-2.2Cu-2.2Mg-0.15Zr (7136-T76511, -T76510) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged



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