Browse Standards AMS4926K
Historical REVISED 2001-11-19

Titanium Alloy, Bars, Wire, and Rings, 5al 2.5sn, Annealed, 110 Ksi (758 Mpa) Yield Strength AMS4926K

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 strength up to 800 degrees F (427 degrees C) and which may be welded during fabrication, but usage is not limited to such applications.

AMS4926P
2019-06-20
Latest
Revised
AMS4926N
2015-07-06
Historical
Revised
AMS4926M
2011-09-13
Historical
Revised
AMS4926L
2007-07-05
Historical
Revised
AMS4926K
2001-11-19
Historical
Revised
AMS4926J
1994-08-01
Historical
Revised
AMS4926H
1988-04-01
Historical
Revised
AMS4926G
1983-07-01
Historical
Revised
AMS4926F
1977-01-15
Historical
Revised
AMS4926E
1976-01-15
Historical
Revised
AMS4926D
1972-11-15
Historical
Revised
AMS4926C
1969-11-01
Historical
Revised
AMS4926B
1966-03-15
Historical
Revised
AMS4926A
1965-09-01
Historical
Revised

SAE MOBILUS

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

Access SAE MOBILUS »

Members save up to 10% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.
We also recommend:
STANDARD

Titanium Alloy, Sheet 6Al - 2Sn - 2Zr - 2Mo - 2Cr - 0.15Si Annealed

AMS4898E

View Details

STANDARD

Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated

AMS4903D

View Details

STANDARD

Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated and Aged

AMS4904D

View Details

Get Involved

Want to participate in updating this standard?

X