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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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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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Steel, Corrosion and Heat-Resistant, Bars, Wire, and Forgings 18Cr - 10.5Ni - 0.60Cb Free-Machining, Solution Heat Treated

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5642M
  • Current
Published 2019-11-05 by SAE International in United States
This specification covers two types of free-machining, corrosion and heat-resistant steel in the form of bars, wire, forgings, and forging stock.
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Titanium Alloy Welding Wire 5Al - 2.5Sn

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4953H
  • Current
Published 2019-11-05 by SAE International in United States
This specification covers a titanium alloy in the form of welding wire.
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Steel, Corrosion Resistant, Bars and Wire 18Cr - 9Ni (303F) Free Machining, High Yield Strength Solution Heat Treated and Cold Worked

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5738E
  • Current
Published 2019-11-05 by SAE International in United States
This specification covers a free-machining, corrosion-resistant steel in the form of cold-worked bars and wire up to 1.750 inches (44.45 mm) inclusive, in nominal diameter or least distance between parallel sides (see 8.5).
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Steel, Corrosion Resistant, Bars and Wire 19Cr - 10Ni (304) High Yield Strength Solution Heat Treated and Cold Worked

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5857D
  • Current
Published 2019-11-05 by SAE International in United States
This specification covers a corrosion-resistant steel in the form of cold-worked bars and wire up to 1.750 inch (44.45 mm) inclusive, in nominal diameter or least distance between parallel sides (see 8.4).
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Shot Peening, Ultrasonically Activated

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2580A
  • Current
Published 2019-11-04 by SAE International in United States
This specification covers the requirements for inducing compressive residual stresses on the surface of metal parts using ultrasonically activated shot peening.
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FITTING ASSEMBLY, UNION, AXIALLY SWAGED, HYDRAULIC 5080 PSI

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
  • Aerospace Standard
  • AS5969F
  • Current
Published 2019-10-31 by SAE International in United States
No Abstract Available.
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Anodic Treatment - Titanium and Titanium Alloys Solution pH 13 or Higher

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2488E
  • Current
Published 2019-10-31 by SAE International in United States
This specification establishes the engineering requirements for producing an anodic coating on titanium and titanium alloys and the properties of the coating.
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