• AMS6915

• 2004-01-13

• Historical. Access the latest revision: AMS6915A

• Ams G Titanium And Refractory Metals Committee

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

These products have been used typically for parts requiring high strength up to 900 degrees F (482 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 6915

• Aerospace

• Titanium alloys
• Titanium