• AMS6936

• 2004-01-13

• Historical. Access the latest revision: AMS6936A

• 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 which require high mechanical properties in the annealed condition and a high strength to weight ratio up to 750 degrees F (399 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; SAE ARP 982 recommends practices to minimize such conditions.

• SAE AMS 6936

• Aerospace

• Titanium alloys
• Titanium