• AMS4919
• Revision: C

• 1994-04-01

• Historical. Access the latest revision: AMS4919G

• Ams G Titanium And Refractory Metals Committee

This specification covers a titanium alloy in the form of sheet, strip, and plate. Primarily for parts requiring a combination of high strength and toughness and good creep resistance up to 1000 degrees F (538 degrees C). 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 4919

• Aerospace

• Nonferrous alloys
• Titanium alloys