Titanium Alloy Sheet, Strip, and Plate 13.5v 11cr 3.0al Solution Heat Treated

Standard:
Revised:
  • 2003-03-14
 
  • HISTORICAL Access the latest revision: AMS4917J
Publisher:
  • SAE International
Pages:
8
Scope:

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

This material has 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 conditions, but usage is not limited to such applications.

This alloy may have poor crack propagation resistance in the precipitation heat treated condition.

Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; ARP982 recommends practices to minimize such conditions.

History:
Standard Published Revision Status
AMS4917J 2017-06-26 Latest Revised
2012-10-19 Historical Revised
2008-03-26 Historical Revised
2003-03-14 Historical Revised
1994-04-01 Historical Reaffirmed
1984-10-01 Historical Revised
1979-07-16 Historical Revised
1969-05-01 Historical Revised
1968-11-01 Historical Revised
1963-01-15 Historical Issued
AKA:
  • SAE AMS 4917
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