SAE AMS4165H-2003
Aluminum Alloy, Extrusions 4.4Cu 1.5Mg 0.60Mn (2024-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened

Standard No.
SAE AMS4165H-2003
Release Date
2003
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4165H-2013
Latest
SAE AMS4165J-2019
Scope
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These extrusions have been used typically for parts subject to excessive warpage during machining due to residual stresses and for parts requiring high strength and whose fabrication does not normally involve welding, but usage is not limited to such applications. Certain processing procedures may cause these extrusions to be susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.

SAE AMS4165H-2003 Referenced Document

  • ASTM B594-02 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*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
  • 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 ARP823 MINIMIZING STRESS CORROSION IN WROUGHT HEAT TREATABLE ALUMINUM ALLOY PRODUCTS
  • SAE ARP823D-1997 Minimizing Stress-Corrosion in Wrought Heat-Treatable Aluminum Alloy Products
  • SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4165H-2003 history

  • 2019 SAE AMS4165J-2019 Aluminum Alloy@ Extrusions 4.4Cu – 1.5Mg – 0.60Mn (2024-T3511) Solution Heat Treated@ Cold Worked@ Stress-Relieved by Stretching@ and Straightened (UNS A92024)
  • 2013 SAE AMS4165H-2013 Aluminum Alloy, Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened
  • 2003 SAE AMS4165H-2003 Aluminum Alloy, Extrusions 4.4Cu 1.5Mg 0.60Mn (2024-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened
  • 1998 SAE AMS4165G-1998 Aluminum Alloy@ Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T3511) Solution Heat Treated@ Stress-Relieved by Stretching@ and Straightened (UNS A92024)
  • 1992 SAE AMS4165F-1992 Aluminum Alloy Extrusions 4.4Cu - 1.5Mg - 0.60Mn (2024-T3511) Stress- Relieved Stretched and Straightened
  • 1978 SAE AMS4165E-1978 ALUMINUM ALLOY EXTRUSIONS 4.4Cu - 1.5Mg - 0.60Mn (2024-T3511) Stress- Relief Stretched and Straightened (UNS A92024)
  • 1968 SAE AMS4165D-1968 ALUMINUM ALLOY EXTRUSIONS 4. 4Cu - 1.5Mg - 0. 60Mn (2024-T3511) Stress-Relief Stretched and Straightened
  • 1964 SAE AMS4165C-1964 ALUMINUM ALLOY EXTRUSIONS 4.4Cu - 1.5Mg - 0.60Mn (2024-T3511) Stress-Relief Stretched and Straightened
  • 1963 SAE AMS4165B-1963 ALUMINUM ALLOY EXTRUSIONS 4.4Cu - 1.5Mg - 0.6Mn (2024-T3511) Stress-Relief Stretched and Straightened
  • 1962 SAE AMS4165A-1962 ALUMINUM ALLOY EXTRUSIONS 4.4Cu - 1.5Mg - 0.6Mn (2024-T3511) Stress-Relief Stretched and Straightened
  • 1960 SAE AMS4165-1960 ALUMINUM ALLOY EXTRUSIONS 4.5Cu - 1.5Mg - 0.6Mn (2024-T3511) Stress-Relief Stretched and Straightened



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