SAE AMS2666C
Steel, Corrosion Resistant, Bars, Wire, Forgings, Tubing, and Rings, 16cr 4.0ni 0.30cb 4.0cu Solution Heat Treated, Precipitation Hardenable.
Standard:
AKA:
- AMS2666
- Revision: C
- 1972-11-15
- Historical. Access the latest revision: AMS2666D
- Ams F Corrosion Heat Resistant Alloys Committee
1. SCOPE:1.1 Purpose: This specification covers the engineering requirements for production of brazed joints inparts made of iron, nickel, and cobalt base alloys by use of silver alloys and the properties of suchjoints.1.2 Application: Primarily for use where joints having high strength up to 800 F (427 C) are required.This specification covers a premium aircraft-quality corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging, flash welded rings, or heading.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS2666D | 1984-01-01 | Latest | |
| AMS2666C | 1972-11-15 | Historical | |
| AMS2666B | 1967-04-01 | Historical | |
| AMS2666A | 1965-02-01 | Historical | |
| AMS2666 | 1950-06-01 | Historical |
- SAE AMS 2666
- Aerospace
- Metallurgy
- Metals
- Steel
- Materials properties