BAC 1509-100401 2024-T3511

Description: Aluminum Extrusion

Details: High-strength aluminum-copper alloy extrusion in the T3511 temper, solution heat-treated and naturally aged for stress relief. Tensile strength of 470 MPa with excellent strength-to-weight ratio and good machinability make it suitable for aircraft structures, frames, and components requiring high structural performance with minimal weight penalty. Widely specified for aerospace fuselage and wing applications where fatigue resistance and corrosion durability are critical operational requirements.

Status: In-stock