Form This specification covers a titanium alloy in the form of sheet@ strip@ and plate up through 2.000 inches (50.80 mm)@ inclusive. Application This material has been used typically requiring high strength-to-weight ratio and stability up to 550 ??(288 ?? in the precipitation heat treated condition in material thicknesses 2.000 inches (50.80 mm) and under@ but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stresscorrosion cracking; ARP982 recommends practices to minimize such conditions.
SAE AMS4904D-2018 history
2023SAE AMS4904E-2023 Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated and Aged
2018SAE AMS4904D-2018 Titanium Alloy Sheet@ Strip@ and Plate 6Al - 4V Solution Heat Treated and Aged (UNS R56400)
2015SAE AMS4904C-2015 Titanium Alloy Sheet@ Strip@ and Plate 6Al - 4V Solution Heat Treated and Aged (UNS R56400)
2011SAE AMS4904B-2011 Titanium Alloy Sheet, Strip, and Plate 6Al 4V Solution Heat Treated and Aged
2007SAE AMS4904A-2007 Titanium Alloy Sheet, Strip, and Plate 6Al 4V Solution Heat Treated and Aged
2003SAE AMS4904-2003 Titanium Alloy Sheet, Strip, and Plate 6Al 4V Solution Heat Treated and Aged