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Titanium Alloy Bars, Forgings and Forging Stock, 13V - 11Cr - 3Al, Solution Heat Treated and Aged

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6926C
  • Current
Published 2019-01-31 by SAE International in United States

This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.6).

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Titanium Alloy Bars, Forgings and Forging Stock, 13V - 11Cr - 3Al, Solution Heat Treated

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6925C
  • Current
Published 2019-01-28 by SAE International in United States

This specification covers a titanium alloy in the form of bars up through 7.000 inches (177.80 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 7.000 inches (177.80 mm), inclusive, and stock for forging of any size.

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Titanium Alloy Bars, Forgings and Forging Stock, 3Al - 8V - 6Cr - 4Mo - 4Zr, Solution Heat Treated and Aged

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6921C
  • Current
Published 2019-01-25 by SAE International in United States

This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.6).

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Titanium Alloy Bars, Forgings and Forging Stock, 3Al - 8V - 6Cr - 4Mo - 4Zr, Solution Heat Treated

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6920D
  • Current
Published 2019-01-25 by SAE International in United States

This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.6).

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Titanium Alloy Bars, Forgings, and Forging Stock 6.0Al - 2.0Sn - 4.0Zr - 6.0Mo Solution Heat Treated and Aged

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6906C
  • Current
Published 2019-01-07 by SAE International in United States
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.7).
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Titanium Alloy, Bars, Wire, Forgings, Rings, and Drawn Shapes 4Al - 2.5V -1.5 Fe Annealed, Heat Treatable

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6947B
  • Current
Published 2019-01-07 by SAE International in United States
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes 4.000 inches (101.60 mm) and under, and stock for forging, heading, or flash welded rings of any size.
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Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 55 ksi (379 MPa) Yield Strength

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4900R
  • Current
Published 2019-01-04 by SAE International in United States
This specification covers one grade of commercially-pure titanium in the form of sheet, strip, and plate 1.000 inch (25.40 mm) and under in nominal thickness.
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Titanium Alloy Bars, Wire, and Rings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4972J
  • Current
Published 2019-01-04 by SAE International in United States
This specification covers a titanium alloy in the form of bars, wire, flash welded rings up through 4.000 inches (101.60 mm), inclusive in diameter or least distance between parallel sides, and stock for flash welded rings or heading of any size.
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Aluminum Beryllium, Preforms Hot Isostatic Pressed and Heat Treated 38Al - 62Be

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS7911D
  • Current
Published 2018-12-28 by SAE International in United States
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of bar, rod, tubing, and shapes.
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Aluminum-Beryllium Alloy, Extrusions 38Al - 62Be Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS7912D
  • Current
Published 2018-12-28 by SAE International in United States
This specification covers an aluminum-beryllium alloy in the form of bars, rods, tubing, and shapes consolidated from powder by extrusion.
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