SAE AMS4242-1986
Aluminum Alloy Castings@ Sand Composite 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft Structural Quality

Standard No.

SAE AMS4242-1986

Release Date

1986

Published By

SAE - SAE International

Status

Be replaced

Replace By

SAE AMS4242A-1997

Latest

SAE AMS4242C-2015

SAE AMS4242-1986 history

• 2015 SAE AMS4242C-2015 Aluminum Alloy@ Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged (UNS A02010)
• 2012 SAE AMS4242B-2012 Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
• 2007 SAE AMS4242B-2007 Aluminum Alloy, Castings 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg - 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged
• 1997 SAE AMS4242A-1997 Aluminum Alloy, Castings, 4.7Cu 0.60Ag 0.35Mn 0.25Mg 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft
• 1986 SAE AMS4242-1986 Aluminum Alloy Castings@ Sand Composite 4.7Cu - 0.60Ag - 0.35Mn - 0.25Mg 0.25Ti (B201.0-T7) Solution Heat Treated and Overaged Aircraft Structural Quality