Browse Standards AMS4966M
Historical Revised 2003-06-16

Titanium Alloy, Forgings 5al 2.5sn Annealed, 110 Ksi (758 Mpa) Yield Strength AMS4966M

This specification covers a titanium alloy in the form of forgings and forging stock.

These forgings have been used typically for parts requiring strength up to 800 degrees F (427 degrees C) and which may be welded during fabrication, but usage is not limited to such applications.

AMS4966R
2017-06-05
Latest
Revised
AMS4966P
2013-02-26
Historical
Revised
AMS4966N
2008-12-19
Historical
Revised
AMS4966M
2003-06-16
Historical
Revised
AMS4966L
1998-10-01
Historical
Revised
AMS4966K
1994-06-01
Historical
Revised
AMS4966J
1993-05-01
Historical
Reaffirmed
AMS4966H
1983-04-01
Historical
Revised
AMS4966G
1979-07-16
Historical
Revised
AMS4966F
1977-01-15
Historical
Revised
AMS4966D
1972-11-15
Historical
Revised
AMS4966C
1969-11-01
Historical
Revised
AMS4966B
1966-03-15
Historical
Revised
AMS4966A
1965-09-01
Historical
Revised
AMS4966
1959-01-15
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 off a customized subscription plan that lets you pay for just the documents that you neeed, when you need them.

Get Involved

Want to participate in updating this standard?

X