AMS4917E: Titanium Alloy, Sheet, Strip, and Plate, 13.5v 11cr 3.0al, Solution Heat Treated - SAE International
Browse Standards AMS4917E
Historical REAFFIRMED 1994-04-01

Titanium Alloy, Sheet, Strip, and Plate, 13.5v 11cr 3.0al, Solution Heat Treated AMS4917E

This specification covers a titanium alloy in the form of sheet, strip, and plate. Primarily for parts to be formed in the solution heat treated condition and subsequently precipitation heat treated. Suitable for parts, such as pressure vessels and aircraft structures, requiring high strength-to-weight ratio and stability up to 550 degrees F (288 degrees C). 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.
AMS4917J
2017-06-26
Latest
Revised
AMS4917H
2012-10-19
Historical
Revised
AMS4917G
2008-03-26
Historical
Revised
AMS4917F
2003-03-14
Historical
Revised
AMS4917E
1994-04-01
Historical
Reaffirmed
AMS4917D
1984-10-01
Historical
Revised
AMS4917C
1979-07-16
Historical
Revised
AMS4917B
1969-05-01
Historical
Revised
AMS4917A
1968-11-01
Historical
Revised
AMS4917
1963-01-15
Historical
Issued

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