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)

Standard No.
SAE AMS4249-1992
Release Date
1992
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE AMS4249A-2005
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 torlerance structural aircraft components(see 8.2)requiring fatugue resistance and fracture toughness,but usage is not limited to such applications.While the material,methods,applications,and processes described or referenced in this specification may involve the use of hazardous materials,this specification does not address the hazards which may be involved in such use.It is the sole repnsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.

SAE AMS4249-1992 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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