SAE AMS6317F
Steel Bars and Forgings 1.8ni 0.25mo (0.38-0.43c) Heat Treated, 125 Ksi (862 Mpa) Tensile Strength.
Standard:
AKA:
- AMS6317
- Revision: F
- 1995-05-01
- 1991-07-01
- Historical. Access the latest revision: AMS6317J
- Ams E Carbon And Low Alloy Steels Committee
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings. Primarily for parts with sections 1.0 inch (25 mm) and under in nominal thickness requiring a minimum tensile strength of 125 ksi (862 MPa).
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS6317J | 2012-11-05 | Latest | |
| AMS6317H | 2007-10-16 | Historical | |
| AMS6317G | 2003-01-22 | Historical | |
| AMS6317F | 1991-07-01 | Historical | |
| AMS6317E | 1986-01-01 | Historical | |
| AMS6317D | 1978-10-16 | Historical | |
| AMS6317C | 1971-11-15 | Historical | |
| AMS6317B | 1945-07-01 | Historical | |
| AMS6317A | 1942-03-01 | Historical | |
| AMS6317 | 1939-12-04 | Historical |
- SAE AMS 6317
- Aerospace
- Metallurgy
- Ferrous metals and alloys
- Steel
- Materials properties
- Ferrous metals