SAE AMS5662M
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable
Historical
Standard by SAE International, 2009-06-11
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About This Item
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
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Standard Details
- Publication Date: 2009-06-11
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Nickel alloys, Cobalt alloys, Tensile strength, Identification numbers, Welding, Corrosion, Heat resistant materials, Chemicals
- Official SAE: Doi link
Document History
- New Version Available: AMS5662P (2022-08-17)
- Previous Version: AMS5662N (2016-06-21)
- This Version: AMS5662M (2009-06-11)
- Previous Version: AMS5662L (2000-07-01)
- Previous Version: AMS5662K (1998-01-01)
- Previous Version: AMS5662J (1994-09-01)
- Previous Version: AMS5662H (1994-08-01)
- Previous Version: AMS5662G (1993-01-01)
- Previous Version: AMS5662F (1989-01-01)
- Previous Version: AMS5662E (1985-10-01)
- Previous Version: AMS5662D (1979-07-01)
- Previous Version: AMS5662C (1972-05-01)
- Previous Version: AMS5662B (1967-11-01)
- Previous Version: AMS5662A (1966-03-15)
- Previous Version: AMS5662 (1965-09-01)
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