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Quality Assurance Sampling and Testing Corrosion and Heat-Resistant Steels and Alloys Wrought Products and Forging Stock

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS2371L
  • Current
Published 2019-12-17 by SAE International in United States

This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable material specification requirements of wrought corrosion and heat-resistant steel and alloy products and of forging stock.

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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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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.
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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).
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Titanium Alloy Bars, Forgings, and Rings 6Al - 4V Extra Low Interstitial (ELI) Duplex Annealed, Fracture Toughness

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4931G
  • Current
Published 2019-11-05 by SAE International in United States
This specification covers a titanium alloy in the form of bars 6.000 inches (152.40 mm) and under in nominal diameter or least distance between parallel sides, forgings and flash welded rings 6.000 inches (152.40 mm) and under in thickness, and stock for forging and stock for flash welded rings of any size.
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Titanium Alloy Wire 44.5 Cb

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4982F
  • Current
Published 2019-10-29 by SAE International in United States
The specification covers a titanium alloy in the form of wire.
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Titanium Alloy Bars, Wire, Forgings, and Rings 6Al - 4V, Extra Low Interstitial Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4930K
  • Current
Published 2019-10-10 by SAE International in United States
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or distance between parallel sides, and stock for forging or flash welded rings of any size.
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Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 70.0 ksi (485 MPa)

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4901U
  • Current
Published 2019-10-04 by SAE International in United States
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate up through 1.000 inch (25.40 mm), inclusive.
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Nickel Alloy, Corrosion and Heat-Resistant, Bars and Forgings 58Ni - 19.5Cr - 13.5Co - 4.3Mo - 3.0Ti - 1.4Al - 0.05Zr - 0.006B Consumable Electrode or Vacuum Induction Melted 1975 °F (1079 °C) Solution, Stabilization, and Precipitation Heat Treated

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5709J
  • Current
Published 2019-09-04 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and forging stock.
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Aluminum Alloy, Clad One Side, Sheet 1.25Mn - 0.12Cu (No. 11-0 Brazing Sheet) Annealed

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4063F
  • Current
Published 2019-07-18 by SAE International in United States
This specification covers an aluminum alloy in the form of clad sheet from 0.006 to 0.249 inches (0.15 to 6.32 mm), inclusive, in thickness (see 8.6).
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