AMS4975H: Titanium Alloy, Bars, Wire and Rings, 6.0al 2.0sn 4.0zr 2.0mo 0.08si, Solution and Precipitation Heat Treated - SAE International
Browse Standards AMS4975H
Historical REVISED 2002-06-14

Titanium Alloy, Bars, Wire and Rings, 6.0al 2.0sn 4.0zr 2.0mo 0.08si, Solution and Precipitation Heat Treated AMS4975H

This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock for flash welded rings.

These products have been used typically for parts requiring high strength and toughness and good creep resistance up to 1000 degrees F (538 degrees C), but usage is not limited to such applications.

Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking. ARP 982 recommends practices to minimize such conditions.

AMS4975N
2017-07-20
Latest
Revised
AMS4975M
2014-03-07
Historical
Revised
AMS4975L
2012-09-14
Historical
Revised
AMS4975K
2011-06-23
Historical
Revised
AMS4975J
2007-04-13
Historical
Revised
AMS4975H
2002-06-14
Historical
Revised
AMS4975G
1994-06-01
Historical
Revised
AMS4975F
1988-10-01
Historical
Revised
AMS4975E
1985-04-01
Historical
Revised
AMS4975D
1983-10-01
Historical
Revised
AMS4975C
1983-04-01
Historical
Revised
AMS4975B
1971-11-15
Historical
Revised
AMS4975A
1970-05-01
Historical
Revised
AMS4975
1968-05-01
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Purchase more aerospace standards and aerospace material specifications and save! AeroPaks offer a customized subscription plan that lets you pay for just the documents that you need, when you need them.

Get Involved

Want to participate in updating this standard?

X