• AMS6940

• 2004-01-13

• Historical. Access the latest revision: AMS6940A

• Ams G Titanium And Refractory Metals Committee

This specification covers a titanium alloy in the form of bars, forgings, and stock for forging.

This material has been used typically for parts requiring strength and oxidation resistance up to 600 degrees F ( 316 degrees C) and weldability, but usage is not limited to such applications.

Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion; SAE ARP 982 recommends practices to minimize such conditions.

• SAE AMS 6940

• Aerospace

• Titanium alloys
• Titanium