SAE AMS4116B
Aluminum Alloy, Bars, Rods, and Wire, 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T4), Cold Finished, Solution Heat Treated and Naturally Aged.
Standard:
AKA:
- AMS4116
- Revision: B
- 1966-03-01
- Historical. Access the latest revision: AMS4116H
- Ams D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of bars, rods, and wire.These products have been used typically for parts requiring moderate ductility, formability, and response to precipitation heat treatment, but usage is not limited to such applications.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS4116H | 2009-07-16 | Latest | |
| AMS4116G | 2002-09-04 | Historical | |
| AMS4116F | 1996-09-01 | Historical | |
| AMS4116E | 1995-05-01 | Historical | |
| AMS4116D | 1978-01-01 | Historical | |
| AMS4116C | 1968-05-01 | Historical | |
| AMS4116B | 1966-03-01 | Historical | |
| AMS4116A | 1960-11-01 | Historical | |
| AMS4116 | 1960-06-01 | Historical |
- SAE AMS 4116
- Aerospace
- Aluminum alloys
- Aluminum