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Nickel Alloy, Corrosion and Heat-Resistant, Bars and Forgings, 57Ni - 20Cr - 10Co - 8.5Mo - 2.1Ti - 1.5Al - 0.005B, Vacuum Induction and Consumable Electrode Melted, Solution Heat Treated, Precipitation Heat Treatable

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5915A
  • Current
Published 2019-12-02 by SAE International in United States

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and stock for forging.

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Aluminum Alloy, Hand Forgings 8.0Zn - 1.0Cu - 1.6Mg - 0.12Zr (7037-T7452) Solution Heat Treated, Compression Stress Relieved, and Overaged (Composition similar to UNS A97037)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4456A
  • Current
Published 2019-11-25 by SAE International in United States

This specification covers an aluminum alloy in the form of hand forgings 11.000 inches (280 mm) and under in nominal thickness and of forging stock of any size (see 8.6).

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Aluminum Alloy, Plate (2397-T87), 2.8Cu - 1.4Li - 0.30Mn - 0.12Zr - 0.10Zn, Solution Heat Treated, Cold Worked, and Artificially Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4328B
  • Current
Published 2019-11-25 by SAE International in United States

This specification covers an aluminum alloy in the form of plate 3.000 to 6.000 inch (76.20 to 152.40 mm), inclusive, in nominal thickness (see 8.5).

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Titanium Alloy, Sheet and Strip 4Al - 2.5V - 1.5Fe Electron Beam Single Melted. Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6949A
  • Current
Published 2019-11-25 by SAE International in United States

This specification covers a titanium alloy in the form of sheet and strip up to 0.143 inches (3.63 mm), inclusive, in nominal thickness.

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Cobalt Alloy, Corrosion and Heat-Resistant, Round Wire 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Vacuum Induction Plus Consumable Electrode Melted Solution Heat Treated, Cold Drawn, and Aged

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5834E
  • Current
Published 2019-11-25 by SAE International in United States

This specification covers a corrosion and heat-resistant cobalt alloy in the form of round wire 0.001 to 0.140 inch (0.025 to 3.56 mm) inclusive in nominal diameter supplied in straight lengths or coils (see 8.6).

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Cobalt Alloy, Corrosion and Heat-Resistant, Round Wire 20Cr - 15Ni - 40Co - 7.0Mo - 16Fe Solution Heat Treated and Cold Drawn

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5833E
  • Current
Published 2019-11-25 by SAE International in United States

This specification covers a corrosion and heat-resistant cobalt alloy in the form of round wire 0.001 to 0.140 inch (0.025 to 3.56 mm) inclusive in nominal diameter supplied in straight lengths or coils (see 8.5).

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Aluminum Alloy, Extrusion 3.7Cu - 1.15Li - 0.5Zn - 0.45Ag - 0.4Mg - 0.3Mn - 0.1Zr (2055-T84) Solution Heat Treated, Stress Relieved by Stretching 2% to 5% and Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4257
  • Current
Published 2019-11-12 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles.
This content contains downloadable datasets
Annotation ability available
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Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La Solution Heat Treated

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5891C
  • Current
Published 2019-11-05 by SAE International in United States
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.
This content contains downloadable datasets
Annotation ability available
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Titanium Alloy Sheet, Strip, and Plate 6Al - 6V - 2Sn Solution Heat Treated and Aged

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4990D
  • Current
Published 2019-11-05 by SAE International in United States
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4 inches (101.6 mm).
This content contains downloadable datasets
Annotation ability available
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Steel, Corrosion-Resistant, Investment Castings 15Cr - 4.6Ni - 0.22Cb - 2.8Cu Solution Heat Treated, Precipitation Hardenable

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5357E
  • Current
Published 2019-11-05 by SAE International in United States
This specification covers a corrosion-resistant steel in the form of investment castings.
This content contains downloadable datasets
Annotation ability available