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Master Bond adhesives
TIMET TIMETAL® 10-2-3 Titanium Alloy (Ti-10V-2Fe-3Al), Aged Billet/Bar per ASTM 4986
Categories: Metal; Nonferrous Metal; Titanium Alloy; Beta Titanium Alloy

Material Notes: High-Strength Forging Alloy. Mechanical property data reported per ASTM 4986 after solution treatment and aging 950°-1000°F (510°-538°C) then air cool.

Industry Specifications: USA Aerospace: AMS 4986.

A readily forgeable alloy that offers excellent combinations of strength, ductility, fracture toughness and high cycle fatigue strength. Typically used for critical aircraft structures, such as landing gear, actuators, flap tracks, and rotor heads.

Typical heat treatment for this alloy: Solution heat treat: 28-56°C below beta transus for a minimum for 30 mins, then water quench Age then air cool.

Data provided by TIMET.

Available Properties
  • Density, Typical
  • Tensile Strength, Ultimate, Typical
  • Tensile Strength, Yield, Typical
  • Elongation at Break, Typical
  • Reduction of Area
  • Modulus of Elasticity, Typical
  • Tensile Modulus
  • Tensile Modulus
  • Compressive Yield Strength
  • Compressive Modulus
  • Ultimate Bearing Strength, e/D = 1.5
  • Ultimate Bearing Strength, e/D = 2.0
  • Bearing Yield Strength, e/D = 1.5
  • Bearing Yield Strength, e/D = 2.0
  • Poissons Ratio
  • Fatigue Strength, Limit; test specifics not reported
  • Fracture Toughness
  • Shear Modulus
  • Shear Strength
  • CTE, linear
  • Beta Transus
  • Aluminum, Al
  • Carbon, C
  • Hydrogen, H
  • Iron, Fe
  • Nitrogen, N
  • Other, each
  • Other, total
  • Oxygen, O
  • Titanium, Ti, Calculated as remainder
  • Vanadium, V
Property Data

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