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AMS 4928 Aerospace Material Specification Ti-6AL-4V
Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes, 6Al - 4V, AnnealedUNS R56400
Alpha-Beta titanium alloy
It is part of the Aerospace Material Standards series from SAE International.
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes, and stock for forging or flash welded rings.
Application: These products have been used typically for parts requiring moderate strength with a maximum service temperature in the 750 to 900°F (399 to 510°C) range depending on time at temperature where the product is to be used in the annealed condition, but usage is not limited to such applications.
Annealing: Heat to a temperature within the range 1300 to 1450°F (704 to 788°C),hold at the selected temperature within +/-25°F (+/-14°C) for not less than 1 hour, and cool as required, held at heat for 20 minutes +/-3, cooled in air, and rescaled.
FIRST can supply Ti-6AL-4V Titanium Alloy Bar AMS 4928 UNS R56400
Designations: GR5 Ti-6Al-4V
Size: (Rolled) DIA8mm TO DIA30mm*L Length=1000mm-4000mm
(Forged) DIA30mm TO DIA400mm*L Length=1000mm-4000mm
Condition: Annealing (M) with rescaled, ground, machined, rough turned.
Specification: AMS 4928
QAC: 100% Ultrasonic Testing; Supply the third party Quality Testing (including chemical composition and mechanical properties)
Packaging: in standard export wooden case with plastic paper
Payment: 30% T/T in advance against PI, the balance should be paid before shipment.
Application: Titanium alloy bars can be used in aerospace fields.