AND 10138-0709 2024-T3511

Description: Aluminum Extrusion

Details: High-strength aluminum extrusion conforming to Army-Navy Drawing 10138 specifications for equal leg zee profile sections in aerospace applications. The 2024-T3511 temper designation indicates solution heat treatment followed by controlled stretching and natural aging, providing excellent strength-to-weight ratio with typical tensile strength above 470 MPa and yield strength exceeding 325 MPa. This copper-alloyed material offers high fatigue resistance and good machinability, commonly employed in aircraft structural components including fuselage frames, stringers, and internal bracing members where superior mechanical properties are required without welding operations.

Status: In-stock