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About This Item

 

Full Description

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.
 

Document History

  1. SAE AMS4249B


    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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  2. SAE AMS4249A

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    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)

    • Historical Version