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

Standard No.

SAE AMS4241B-2002

Release Date

2002

Published By

SAE - SAE International

Status

Be replaced

Replace By

SAE AMS4241C-2002

Latest

SAE AMS4241E-2015

SAE AMS4241B-2002 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)