• AMS6910

• 2004-01-13

• Historical. Access the latest revision: AMS6910A

• Ams G Titanium And Refractory Metals Committee

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

This alloy has been used typically for parts requiring strength up to 800 degrees F (427 degrees C), but usage is not limited to such applications.

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

• SAE AMS 6910

• Aerospace

• Titanium alloys
• Titanium