SAE AMS4242B-2007
Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged

Standard No.
SAE AMS4242B-2007
Release Date
2007
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4242B-2012
Latest
SAE AMS4242C-2015
Scope
This specification covers an aluminum alloy in the form of castings. These castings have been used typically for aircraft components requiring high strength and reliability, both at room and elevated temperatures, but usage is not limited to such applications. Alloy B201.0, the alloy designated in this specification, has restricted composition within the limits of alloy A201.0.

SAE AMS4242B-2007 Referenced Document

  • ASTM B557-06 Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products*2024-04-18 Update
  • ASTM B557M-06 Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products [Metric]*2024-04-18 Update
  • ASTM B557M-07 Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products [Metric]*2024-04-18 Update
  • ASTM B660-02 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-18 Update
  • ASTM E101-91 
  • ASTM E1251-07 Standard Test Method for Analysis of Aluminum and Aluminum Alloys by Atomic Emission Spectrometry*2024-04-18 Update
  • ASTM E1417-05 Standard Practice for Liquid Penetrant Testing*2024-04-18 Update
  • ASTM E155-05 Standard Reference Radiographs for Inspection of Aluminum and Magnesium Castings*2024-04-18 Update
  • ASTM E1742-06 Standard Practice for Radiographic Examination*2024-04-18 Update
  • ASTM E29-06 Standard Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications
  • ASTM E607-02 Standard Test Method for Atomic Emission Spectrometric Analysis Aluminum Alloys by the Point to Plane Technique Nitrogen Atmosphere*2024-04-18 Update
  • ASTM G44-99 Standard Practice for Exposure of Metals and Alloys by Alternate Immersion in Neutral 3.5% Sodium Chloride Solution

SAE AMS4242B-2007 history

  • 2015 SAE AMS4242C-2015 Aluminum Alloy@ Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged (UNS A02010)
  • 2012 SAE AMS4242B-2012 Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
  • 2007 SAE AMS4242B-2007 Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
  • 1997 SAE AMS4242A-1997 Aluminum Alloy, Castings, 4.7Cu 0.60Ag 0.35Mn 0.25Mg 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft
  • 1986 SAE AMS4242-1986 Aluminum Alloy Castings@ Sand Composite 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft Structural Quality



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