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Material Name:
AND10136-1703 7075-T6511
Description:
Aluminum Extersion
Details:
High-strength aluminum tee-section extrusion in the 7075-T6511 temper, solution heat treated, artificially aged, and stress relieved through stretching. This alloy delivers excellent fatigue resistance and strength-to-weight ratio for highly stressed structural applications. Widely used in aircraft frames, wing components, and fuselage fittings where superior load-carrying capacity and damage tolerance are essential.
Status:
In-stock |
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