SAE AMS6325A
Steel, Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength.
Standard:
AKA:
- AMS6325
- Revision: A
- 1943-04-01
- Historical. Access the latest revision: AMS6325J
- 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.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS6325J | 2010-04-19 | Latest | |
| AMS6325H | 2004-10-18 | Historical | |
| AMS6325G | 1994-05-01 | Historical | |
| AMS6325F | 1988-07-01 | Historical | |
| AMS6325E | 1972-11-15 | Historical | |
| AMS6325D | 1966-09-30 | Historical | |
| AMS6325C | 1951-06-01 | Historical | |
| AMS6325B | 1945-07-01 | Historical | |
| AMS6325A | 1943-04-01 | Historical | |
| AMS6325 | 1942-09-01 | Historical |
- SAE AMS 6325
- Aerospace
- Metallurgy
- Ferrous metals and alloys
- Steel
- Materials properties
- Ferrous metals