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Tolerances Corrosion and Heat Resistant Steel, Iron Alloy, Titanium, and Titanium Alloy Sheet, Strip, and Plate

  • Aerospace Material Specification
  • AMS2242G
  • Current
Published 2020-10-21 by SAE International in United States
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Heat Treatment Martensitic Corrosion-Resistant Steel Parts

  • Aerospace Material Specification
  • AMS2759/5F
  • Current
Published 2020-09-29 by SAE International in United States
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Heat Treatment of Parts in a Vacuum

  • Aerospace Material Specification
  • AMS2769D
  • Current
Published 2020-09-22 by SAE International in United States
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Steel, Corrosion-Resistant, Laminated, Sheet Surface Bonded

  • Aerospace Material Specification
  • AMS5500G
  • Current
Published 2020-09-09 by SAE International in United States
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Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 59Ni - 22Cr - 2Mo - 14W - 0.35Al - 0.03La Solution Heat Treated

  • Aerospace Material Specification
  • AMS5878E
  • Current
Published 2020-08-26 by SAE International in United States
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Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb - 4.0Cu Solution Heat Treated, Precipitation Hardenable Consumable Electrode Remelted

  • Aerospace Material Specification
  • AMS5622G
  • Current
Published 2020-08-24 by SAE International in United States
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Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb - 2.5Ti - 0.70Al - 7.0Fe Equalized, Precipitation Hardenable

  • Aerospace Material Specification
  • AMS5667P
  • Current
Published 2020-08-04 by SAE International in United States
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Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 57Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.006B - 0.05Zr Consumable Electrode or Vacuum Induction Melted 1825 to 1900 °F Solution Heat Treated

  • Aerospace Material Specification
  • AMS5706N
  • Current
Published 2020-08-04 by SAE International in United States
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Nickel Alloy, Corrosion and Heat Resistant, Forgings 57Ni - 19.5Cr - 13.5Co - 4.6Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted 1825 to 1900 °F (996 to 1038 °C) Solution, Stabilization, and Precipitation Heat Treated

  • Aerospace Material Specification
  • AMS5704L
  • Current
Published 2020-08-03 by SAE International in United States
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Annotation ability available
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Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted, Annealed

  • Aerospace Material Specification
  • AMS5544L
  • Current
Published 2020-07-14 by SAE International in United States
This content contains downloadable datasets
Annotation ability available