SAE AMS4249A-2005
Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing) UNS A43570

Standard No.
SAE AMS4249A-2005
Release Date
2005
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4249A-2012
Latest
SAE AMS4249B-2018
Scope
This specification covers an aluminum alloy in the form of castings. These castings have been used typically for durability and damage tolerance structural aircraft components requiring fatigue resistance and fracture toughness, but usage is not limited to such applications.

SAE AMS4249A-2005 Referenced Document

  • ASTM B557-02 Standard Test Methods of Tension Testing Wrought and Cast Aluminum- and Magnesium-Alloy Products*2024-04-18 Update
  • ASTM B557M-02 Standard Test Methods of 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 E10-01 Standard Test Method for Brinell Hardness of Metallic Materials*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 E1304-97 Standard Test Method for Plane-Strain (Chevron-Notch) Fracture Toughness of Metallic Materials
  • ASTM E1417-99 Standard Practice for Liquid Penetrant Examination
  • ASTM E155-00 Standard Reference Radiographs for Inspection of Aluminum and Magnesium Castings*2024-04-18 Update
  • ASTM E155-05 Standard Reference Radiographs for Inspection of Aluminum and Magnesium Castings*2024-04-18 Update
  • ASTM E29-04 Standard Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications*2024-04-18 Update
  • ASTM E466-96 Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials
  • 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

SAE AMS4249A-2005 history

  • 2018 SAE AMS4249B-2018 Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing) (UNS A43570)
  • 2012 SAE AMS4249A-2012 Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing)
  • 2005 SAE AMS4249A-2005 Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing) UNS A43570
  • 1992 SAE AMS4249-1992 Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing)



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