• AMS4939
• Revision: B

• 2013-02-26

• Ams G Titanium And Refractory Metals Committee

This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.60 mm). This material has been used typically for parts to be formed or machined in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 °F (288 °C) in the precipitation heat treated condition, but usage is not limited to such applications.

• SAE AMS 4939

• Aerospace

• Metallurgy
• Beryllium alloys
• Titanium alloys
• Titanium
• Materials properties
• Refractory materials
• Beryllium