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Fittings, 37 Degree Internal Flare, Fluid Connection, Procurement Specification

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
  • Aerospace Standard
  • AS4841C
  • Current
Published 2020-03-10 by SAE International in United States
This SAE Aerospace Standard (AS) establishes the requirements for 37 degree flared tube fittings or machined internal cone fluid connection fittings for use with 37 degree external cone, spherical nose, and seal ring fittings in all types of aerospace fluid systems (see Section 6).
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Titanium Alloy, Hydraulic, Seamless Tubing 3.0Al - 2.5V Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4943L
  • Current
Published 2020-02-18 by SAE International in United States
This specification covers a titanium alloy in the form of seamless tubing.
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Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4945H
  • Current
Published 2020-02-13 by SAE International in United States
This specification covers a titanium alloy in the form of seamless tubing.
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Titanium Alloy Tubing, Seamless, Hydraulic 3.0Al - 2.5V Cold Worked, Stress Relieved

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4944M
  • Current
Published 2020-01-30 by SAE International in United States
This specification covers a titanium alloy in the form of seamless tubing.
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Titanium Alloy, Round Bar and Wire 3Al - 8V - 6Cr - 4Mo - 4Zr Consumable Electrode Melted Solution Heat Treated and Cold Drawn

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4957G
  • Current
Published 2020-01-14 by SAE International in United States
This specification covers a titanium alloy in the form of round bar and wire, 0.625 inch (15.88 mm) and under in nominal diameter or thickness.
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Chemical Film Treatment for Aluminum Alloys General Purpose Coating

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2473J
  • Current
Published 2020-01-14 by SAE International in United States
This specification establishes the requirements for chemical-film (conversion) coatings on aluminum alloys.
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Titanium Alloy Sheet, Strip, and Plate 6Al - 4V Solution Heat Treated

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4903D
  • Current
Published 2020-01-14 by SAE International in United States
This specification covers a titanium alloy in the form of sheet strip and plate up through 2.000 inches (50.80 mm), inclusive.
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Titanium Alloy Bars, Forgings and Forging Stock 7.0Al - 4.0Mo Annealed

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS6915C
  • Current
Published 2020-01-14 by SAE International in United States
This specification covers a titanium alloy in the form of bars up through 6.000 inches (152.40 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 6.000 inches (152.40 mm), inclusive and stock for forging of any size.
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Anodic Treatment of Aluminum Alloys Sulfuric Acid Process, Dyed Coatings

AMS B Finishes Processes and Fluids Committee
  • Aerospace Material Specification
  • AMS2472H
  • Current
Published 2020-01-13 by SAE International in United States
This specification establishes the requirements for dyed anodic coatings on aluminum alloys.
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Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7651) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4204D
  • Current
Published 2019-12-27 by SAE International in United States
This specification covers an aluminum alloy in the form of plate 0.250 to 5.500 inch (6.35 to 139.70 mm), inclusive in nominal thickness (see 8.5).
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