Browse Standards AMS5843D
Historical Revised 2000-10-01

Cobalt-Nickel Alloy, Corrosion and Heat Resistant, Bars 19cr 36co 25ni 7.0mo 0.50cb 2.9ti 0.20al 9.0fe Vacuum Induction Plus Vacuum Consumable Electrode Melted, Solution Heat Treated Work Strengthened and Aged AMS5843D

This specification covers a high strength, corrosion and heat resistant cobalt-chromium-nickel alloy in the form of bars.

These bars have been used typically for applications requiring a combination of high strength up to 1100 degrees F (593 degrees C), good tension-tension fatigue strength, toughness, and ductility, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice-corrosion, stress-corrosion cracking, and elevated temperature relaxation.

AMS5843G
2016-06-06
Latest
Revised
AMS5843F
2011-09-13
Historical
Revised
AMS5843E
2006-08-03
Historical
Revised
AMS5843D
2000-10-01
Historical
Revised
AMS5843C
1995-01-01
Historical
Revised
AMS5843B
1989-07-01
Historical
Revised
AMS5843
1977-03-01
Historical
Issued
AMS5843A
1943-07-01
Historical
Revised

SAE MOBILUS

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

Access SAE MOBILUS »

Members save up to 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