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Steel, Bars, and Forgings 3.5Cr - 9.5Ni - 18Co - 1.1Mo (0.13 - 0.17C) Double Vacuum Melted, Normalized, Annealed

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS6517B
  • Current
Published 2019-10-10 by SAE International in United States
This specification covers a premium aircraft-quality alloy steel in the form of bars, forgings, and forging stock.
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Heat Treatment of Carbon and Low-Alloy Steel Parts Minimum Tensile Strength Below 220 ksi (1517 MPa)

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS2759/1H
  • Current
Published 2019-09-19 by SAE International in United States
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of carbon and low-alloy steel parts to minimum ultimate tensile strengths below 220 ksi (1517 MPa). Parts are defined in AMS2759. Due to limited hardenability in these materials, there are size limits in this specification.
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Steel, Bars, Forgings, and Tubing 1.45Cr (0.93 - 1.05C) (SAE 52100) Premium Aircraft-Quality, Consumable Electrode Vacuum Remelted

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS6444N
  • Current
Published 2019-08-01 by SAE International in United States
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
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Steel Bars 1.0Cr - 0.20Mo - 0.45Se (0.39 - 0.48C) (4142H Modified) Die-Drawn, 130 ksi (896 MPa) Yield Strength Free Machining

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS6378H
  • Current
Published 2019-07-26 by SAE International in United States
This specification covers a free-machining, low-alloy steel in the form of round bars 3.50 inches (88.9 mm) and under in nominal diameter produced by a die-drawing process.
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Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1517 MPa) and Higher

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS2759/2J
  • Current
Published 2019-07-15 by SAE International in United States
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of low-alloy steel parts to minimum ultimate tensile strengths of 220 ksi (1517 MPa) and higher. Parts are defined in AMS2759. The requirements for heat treatment of alloy Aermet100 are no longer part of this specification and can be found in AMS2759/3. Due to the limited hardenability of these materials, size limits have been added to this specification.
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Heat Treatment of Carbon and Low-Alloy Steel Parts Minimum Tensile Strength Below 220 ksi (1517 MPa)

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS2759/1G
  • Historical
Published 2019-06-17 by SAE International in United States
This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of carbon and low-alloy steel parts to minimum ultimate tensile strengths below 220 ksi (1517 MPa). Parts are defined in AMS2759. Due to limited hardenability in these materials, there are size limits in this specification.
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Steel, Carburizing Grade, Bars, Forgings, and Tubing 1.2Cr - 3.2Ni - 0.12Mo (0.14 - 0.20C) (9317)

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS6264M
  • Current
Published 2019-06-17 by SAE International in United States
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
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Nickel-Iron Alloy, Magnetic, Sheet and Strip 50Ni - 50Fe Annealed, Forming Grade

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS7717E
  • Current
Published 2019-05-29 by SAE International in United States
This specification covers a magnetically soft nickel-iron alloy in the form of sheet and strip.
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Nickel-Iron Alloy, Magnetic, Sheet and Strip 50Ni - 50Fe Stamping Quality, Half-Hard Temper

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS7719E
  • Current
Published 2019-05-29 by SAE International in United States
This specification covers a magnetic nickel-iron alloy in the form of sheet and strip.
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Heat Treatment of Steel Raw Materials

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMSH6875B
  • Current
Published 2019-05-29 by SAE International in United States
This specification covers the requirements for heat-treatment of four classes of steel (See 1.2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (See 6.3) test procedures. This specification is applicable only to the heat treatment of raw material (See 6.3.1); it does not cover the requirements for the heat treatment of steel parts (See 3.4 and 6.3.2). This specification also describes procedures that, when followed, will produce the desired properties and material qualities within the limitations of the respective alloys tabulated in Tables 1A, 1B, 1C and 1D. Alloys other than those specifically covered herein may be heat treated using all applicable requirements of this specification.
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