• AMS6905

• 2004-01-12

• Historical. Access the latest revision: AMS6905A

• 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 and toughness and good creep resistance up to 1000 degrees F (538 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 6905

• Aerospace

• Titanium alloys
• Titanium