BAC1505-100283 7075-T73511

Description: Aluminum Extrusion

Details: High-strength aluminum extrusion composed of aluminum, zinc, magnesium, and copper in the T73511 temper condition, solution heat treated and stress relieved. This alloy exhibits excellent strength-to-weight ratio, good fatigue resistance, and average machinability. Widely used in aircraft structural components, airframes, and high-load bearing applications where lightweight strength is critical.

Status: In-stock