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SAE AMS4249A
- 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 by SAE International, 04/01/2012
- Publisher: SAE
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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.
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