• AMS4914
• Revision: C

• 2003-07-23

• Historical. Access the latest revision: AMS4914E

• Ams G Titanium And Refractory Metals Committee

This specification covers a titanium alloy in the form of sheet and strip.

These products have been used typically for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 degrees F (288 degrees C) in the precipitation heat treated condition, but usage is not limited to such applications.

• SAE AMS 4914

• Aerospace

• Nonferrous alloys
• Titanium alloys