SAE AMS5662P PDF | Request Standard
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SAE AMS5662P

Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings, and Stock for 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

Standard by SAE International, 2022-08-17

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  • Language: English
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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 in the solution heat treated condition. Product covered by this specification is limited to 10.00 inches (254 mm) and under in nominal diameter or maximum cross-sectional dimension between parallel sides (thickness) and nominal cross sectional area of 78.54 in2 (503 cm2) in cross-sectional area. Stock for forging, ring, or heading may be of any size. AMS5662 is the result of a Five-Year Review and update of the specification. The revision updates the title to match the scope, clarifies sizes and size limits (1.1, 3.5.1.2, Tables 2 and 3), updates composition and reporting requirements (3.1, 3.1.1), updates cooling rate requirements (3.5.1.2), adds strain rate control (3.5.1.2.1.6), clarifies transverse testing requirement (3.5.1.2.1.4), updates allowable size range for testing (3.5.1.2.3.1), prohibits unauthorized exceptions (3.5.1.4 3.9, 4.4.1.1, 4.4.2, 5.2.1.1, 8.5), updates forging stock ordering options (4.4.3, 8.6), and allows prior revisions (8.4).
SKU: 824dad625719

  • Publication Date: 2022-08-17
  • Standard Status: latest
  • Publisher: SAE International
  • Document Type: Aerospace Material Specification
  • Subject: Nickel alloys, Heat resistant alloys, Metals, Coatings, colorants, and finishes, Materials properties, Cobalt alloys, Heat treatment, Tensile strength, Heat resistant materials
  • Official SAE: Doi link

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