SAE AMS6478-2000
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
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SAE AMS6478-2000
Standard No.
SAE AMS6478-2000
Release Date
2000
Published By
Society of Automotive Engineers (SAE)
Status
Be replaced
Replace By
SAE AMS6478A-2001
Latest
SAE AMS6478B-2005
Scope
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
SAE AMS6478-2000 history
2005
SAE AMS6478B-2005
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 (UNS K92580)
2001
SAE AMS6478A-2001
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 UNS K92580
2000
SAE AMS6478-2000
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
1994
SAE AMS6478-1994
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 (UNS K92580)
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