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Ti-10V-2Fe-3Al (Ti-10-2-3)

R56410
Titaniumnear_beta
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Near-beta titanium alloy developed for high-strength airframe forgings. UNS R56410. Solution treated + aged: Rm ~1195–1241 MPa, Rp0.2 ~1100–1120 MPa, A ~10%. Density 4.65 g/cm³, E-Modul 110 GPa. Best hot-die forgeability of any commercial titanium alloy. Deep-hardenable. AMS 4983/4984/4986/4987. Applications: aircraft landing gear (Boeing 777, Airbus A380), actuation components, helicopter rotor hubs, high-strength structural forgings.

International equivalents

FlagStandardCountryGradeNumberMatch
🇺🇸UNSUSAR56410%
🇺🇸AMSUSAAMS 4983/4984/4986/4987%
🇺🇸TIMETUSATIMETAL 10-2-3%

Sources: SAE/ASTM, SAE AMS, timet.com

Mechanical properties

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