Ti-10V-2Fe-3Al

UNS R56410 titanium
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High-strength beta titanium alloy developed for aircraft structural forgings. Achieves tensile strengths >1200 MPa with excellent fatigue properties for large bulkhead forgings.

Applicable Standards

  • AMS 4984
  • UNS R56410

Composition Ranges (wt %)

Element Min (%) Max (%) Typical Range
Ti 82.0 87.0 ~84.5
V 9.0 11.0 ~10.0
Al 2.6 3.4 ~3.0
Fe 1.6 2.4 ~2.0
O — 0.16 ~0.08
Ti 82.0–87.0% V 9.0–11.0% Al 2.6–3.4% Fe 1.6–2.4% O 0.0–0.16%

Typical Applications

  • Aircraft bulkhead forgings
  • Landing gear
  • Wing attach fittings
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