SAE AMS5662N
Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50AI - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable
Historical
Standard by SAE International, 2016-06-21
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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 10.00 inches (254 mm) and under in nominal diameter or least distance between parallel sides, having a maximum cross-sectional area of 78 in2 (503 cm2), and forging stock of any size (see 8.5).
AMS5662N revises Composition (Table 1), Condition (3.3.1.3), Properties (3.5, Tables 2 and 3), added properties for product 5 to 10 inches (127 to 254 mm) in diameter or least distance between parallel sides, adds conformance to AS6279 (3.8), and revises Reports (4.4), and is a Five Year Review and update of this specification.
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Standard Details
- Publication Date: 2016-06-21
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Heat treatment, Nickel alloys, Cobalt alloys, Tensile strength, Identification numbers, Welding, Metals, Identification, Production
- Official SAE: Doi link
Document History
- New Version Available: AMS5662P (2022-08-17)
- This 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)
- Previous Version: AMS5662B (1967-11-01)
- Previous Version: AMS5662A (1966-03-15)
- Previous Version: AMS5662 (1965-09-01)
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