SAE AMS6327G
Steel Bars and Forgings, 0.50cr 0.55ni 0.25mo (0.38 0.43c) (SAE 8740), Heat Treated, 125,000 Psi (862 Mpa) Tensile Strength.
Standard:
AKA:
- AMS6327
- Revision: G
- 2000-10-01
- 1988-10-01
- Historical. Access the latest revision: AMS6327K
- Ams E Carbon And Low Alloy Steels Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings. Primarily for parts, such as nuts, bolts, and screws, 1.50 inch (38.1 mm) and under in section thickness, requiring a minimum tensile strength of 125,000 (862 MPa).
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS6327K | 2012-10-03 | Latest | |
| AMS6327J | 2007-10-16 | Historical | |
| AMS6327H | 2003-01-22 | Historical | |
| AMS6327G | 1988-10-01 | Historical | |
| AMS6327F | 1981-01-15 | Historical | |
| AMS6327E | 1972-11-15 | Historical | |
| AMS6327D | 1966-09-30 | Historical | |
| AMS6327C | 1951-06-01 | Historical | |
| AMS6327B | 1945-07-01 | Historical | |
| AMS6327A | 1943-04-01 | Historical | |
| AMS6327 | 1942-09-01 | Historical |
- SAE AMS 6327
- Aerospace
- Metallurgy
- Ferrous metals and alloys
- Steel
- Materials properties
- Ferrous metals