SAE AMS4241E-2015
Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled (UNS A43570)

Standard No.

SAE AMS4241E-2015

Release Date

2015

Published By

SAE - SAE International

Latest

SAE AMS4241E-2015

Scope

Form This specification covers an aluminum alloy in the form of castings. Application These castings have been used typically for structural aircraft components (see 8.3) requiring DAS quality control@ but usage is not limited to such applications.

SAE AMS4241E-2015 history

• 2015 SAE AMS4241E-2015 Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled (UNS A43570)
• 2009 SAE AMS4241D-2009 Aluminum Alloy Castings 7.0Si 0.58Mg 0.15Ti 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
• 2007 SAE AMS4241C-2007 Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
• 2002 SAE AMS4241C-2002 Aluminum Alloy Castings 7.0Si 0.58Mg 0.15Ti 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
• 2002 SAE AMS4241B-2002 Aluminum Alloy Castings 7.0Si 0.58Mg 0.15Ti 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
• 2000 SAE AMS4241A-2000 Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled
• 1992 SAE AMS4241A-1992 Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Dendrite Arm Spacing (DAS) Controlled (UNS A43570)
• 1991 SAE AMS4241-1991 ALUMINUM ALLOY CASTINGS, SAND COMPOSITE 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Aircraft Structural Quality
• 1986 SAE AMS4241-1986 ALUMINUM ALLOY CASTINGS@ SAND COMPOSITE 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated Aircraft Structural Quality (UNS A03570)