• AMS4897

• 1997-01-01

• Historical. Access the latest revision: AMS4897C

• 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 tob e formed in the solution heat treated condition and subsequently precipitation heat treated to obtain high strength-to-weight ratio or stability up to 1100 degrees F (593 degrees C), but usage is not limited to such applications.

• SAE AMS 4897

• Aerospace

• Nonferrous alloys
• Titanium alloys