APPLICATION: Primarily for parts which are machined after solution and precipitation heat treatment. Suitable for parts@ such as pressure vessels and other aerospace structures@ requiring high strength-to-weight ration at@ or near@ room temperature.
SAE AMS4965-1966 history
2022SAE AMS4965N-2022 Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Solution Heat Treated and Aged
2018SAE AMS4965M-2018 Titanium Alloy@ Bars@ Wire@ Forgings@ and Rings 6.0Al - 4.0V Solution Heat Treated and Aged (UNS R56400)
2014SAE AMS4965L-2014 Titanium Alloy, Bars, Wire, Forgings, and Rings, 6.0AI - 4.0V, Solution Heat Treated and Aged
2011SAE AMS4965K-2011 Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged
2007SAE AMS4965J-2007 Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged
2002SAE AMS4965H-2002 Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al 4.0V Solution Heat Treated and Aged
1996SAE AMS4965G-1996 Titanium Alloy@ Bars@ Wire@ Forgings@ and Rings 6.0Al - 4.0V Solution Heat Treated and Aged (UNS R56400)
1990SAE AMS4965F-1990 Titanium Alloy Bars@ Forgings@ and Rings 6.0Al - 4.0V Solution and Precipitation Heat Treated (UNS R56400)
1985SAE AMS4965E-1985 Titanium Alloy Bars@ Forgings@ and Rings 6.0Al - 4.0V Solution and Precipitation Heat Treated (UNS R56400)
1977SAE AMS4965D-1977 Titanium Alloy Bars@ Forgings@ and Rings 6Al - 4V Solution and Precipitation Heat Treated
1971SAE AMS4965B-1971 Titanium Alloy Bars@ Forgings@ and Rings 6Al - 4V Solution and Precipitation Heat Treated
1969SAE AMS4965A-1969 Titanium Alloy Bars and Forgings 6Al - 4V Solution and Precipitation Heat Treated