SAE AMS6478B
Steel, Bars and Forgings, 3.1Cr - 11.5Ni - 13.5Co - 1.2Mo (0.21 - 0.25C), Vacuum Melted, Annealed, Heat Treatable to 290 ksi (1999 MPa) Tensile Strength (Cancelled Sep 2005)
Standard:
AKA:
- AMS6478
- Revision: B
- 2005-09-30
- Ams E Carbon And Low Alloy Steels Committee
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
These products have been used typically for parts requiring a combination of high strength, high toughness, and weldability, but usage is not limited to such applications. Product after proper heat treatment should attain a minimum tensile strength of 290 ksi (1999 MPa) and yield strength of 245 ksi (1689 MPa).
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS6478B | 2005-09-30 | Latest | |
| AMS6478A | 2001-10-01 | Historical | |
| AMS6478 | 1994-05-01 | Historical |
- SAE AMS 6478
- Aerospace
- Metallurgy
- Ferrous metals and alloys
- Steel
- Materials properties
- Ferrous metals