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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 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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Heat Treatment of Parts in a Vacuum

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS2769C
  • Current
Published 2019-07-12 by SAE International in United States
This specification establishes the requirements and procedures for heat treating parts in vacuum/partial pressure and shall be used as a supplementary document to primary heat treating specifications as applicable.
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Aluminum Alloy, Extruded Profiles (2043-T85) 2.8Cu - 1.65Li - 0.35Mg - 0.1Zr Solution Heat Treated, Stress Relieved by Stretching, and Aged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4450
  • Current
Published 2019-07-03 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) produced with thickness between 0.040 and 2.500 inches (1.02 to 38.10 mm) in thickness, and having a maximum cross sectional area of 23 in2 (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 16 inches (406 mm) (see 8.4.1).
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Aluminum Alloy, Extruded Bar, Rod, and Shapes 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr 7075-T76(51X) Solution Heat Treated and Overaged

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4317B
  • Current
Published 2019-07-02 by SAE International in United States
This specification covers an aluminum alloy in the form of extruded bars, rods, and shapes up to 4.000 inches, incl (101.60 mm, incl) in nominal diameter or least thickness, and having a nominal cross-sectional area up to 20 in2 (129 cm2) (see 8.5).
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Titanium Alloy, Bars, Wire, and Rings 5Al - 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4926P
  • Current
Published 2019-06-20 by SAE International in United States
This specification covers a titanium alloy in the form of bars, wire, flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and 16 in2 (103 cm2) and under in cross-sectional area, and stock of any size for flash welded rings.
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