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A286, AMS 5732

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A-286 AMS 5732 is an iron base superalloy designed for applications requiring high strength and good corrosion resistance at temperatures up to 1300°F (704 °C). A-286 AMS 5732 from Rockwell Industries attains its high strength levels through a solution heat treatment followed by a precipitation hardening. Its oxidation resistance remains high for continuous service to 1500°F.

It attains its high strength levels through a solution heat treatment followed by a precipitation hardening. Its oxidation resistance remains high for continuous service to 1500°F.

Common applications are jet engine components, bolts, fasteners, afterburners, oil & gas.

Common Industry Trade Names:


Our common stock sizes from = .3125” to 6.000” diameters.

Rockwell-Industries-A-286-AMS-5732

Common Specifications:

  • AMS 5732
  • Pratt & Whitney LCS F-17
  • General Electric S-400 / S-SPEC-35
  • Rolls Royce Sabre

Heat treatment: Heat to 1800 °F ±25 (982 °C), hold at heat for a time commensurate with cross-sectional thickness, and quench in oil or water.

Precipitation heat treatment: Heat to a temperature within the range of 1300 to 1400°F (704 to 760 °C), hold at temperature for a total of not less than 16 hours, and cool at a rate equivalent to cooling in air.

Hardness requirement = 241 to 341 HB.


Minimum Room Temperature Tensile Properties:

Rockwell-Industries-A-286-AMS-5732-Minimum-Tensile-Properties

Composition

Element

MIN

MAX

Carbon -- 0.08
Manganese -- 2.00
Silicon -- 1.00
Phosphorus -- 0.025
Sulfur -- 0.025
Chromium 13.50 16.00
Nickel 24.00 27.00
Molybdenum 1.00 1.50
Titanium 1.90 2.35
Boron 0.003 0.010
Vanadium 0.10 0.50
Cobalt -- 1.00
Aluminum -- 0.35
Copper -- 0.50

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