SAE AMS5662B
ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT Nickel Base - 19Cr - 3.1Mo - 5.1(Cb + Ta) - 0.90Ti - 0.50Al Consumable Electrode or Vacuum Induction Melted 1750 F (954.4 C) Solution Heat Treated
Historical
Standard by SAE International, 1967-11-01
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Standard Details
- Publication Date: 1967-11-01
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat resistant materials, Corrosion resistant alloys, Heat treatment, Coatings, colorants, and finishes, Tensile strength, Manufacturing systems, Identification, ,
- Official SAE: Doi link
Document History
- New Version Available: AMS5662P (2022-08-17)
- Previous Version: AMS5662N (2016-06-21)
- Previous 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)
- This Version: AMS5662B (1967-11-01)
- Previous Version: AMS5662A (1966-03-15)
- Previous Version: AMS5662 (1965-09-01)
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