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Aerospace Standard Test Methods for Aerospace Sealants Two-Component Synthetic Rubber Compounds

AMS G9 Aerospace Sealing Committee
  • Aerospace Standard
  • AS5127/1D
  • Current
Published 2020-03-18 by SAE International in United States
This SAE Aerospace Standard (AS) describes test methods to determine the application and performance properties of two-component sealing compounds. It shall be used in conjunction with AS5127 and the applicable material specification. When modifications to these test methods are called out in material specifications, the material specification shall take precedence.
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Titanium Alloy, Welding Wire 6AI - 2Sn - 4Zr - 2Mo

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4952G
  • Current
Published 2020-03-18 by SAE International in United States
This specification covers a titanium alloy in the form of welding wire.
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Lubricant Application, Solid Film, Heat Cured, Corrosion Inhibiting

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS5528D
  • Current
Published 2020-03-10 by SAE International in United States
This SAE Aerospace Standard (AS) establishes the surface pretreatment, temperature, and baking time required to cure AS5272 lubricant when it is applied over the surfaces of manufactured parts of various metals.
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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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Advancements of Superplastic Forming and Diffusion Bonding of Titanium Alloys for Heat Critical Aerospace Applications

The Boeing Company-Eve Taylor Burkhart, Larry Hefti
  • Technical Paper
  • 2020-01-0033
Published 2020-03-10 by SAE International in United States
Titanium’s high strength-to-weight ratio and corrosion resistance makes it ideal for many aerospace applications, especially in heat critical zones. Superplastic Forming (SPF) can be used to form titanium into near-net, complex shapes without springback. The process uses a machined die where inert gas is applied uniformly to the metal sheet, forming the part into the die cavity. Standard titanium alpha-beta alloys, such as 6Al-4V, form at temperatures between 900 and 925°C (1650-1700°F). Recent efforts have demonstrated alloys that form at lower temperatures ranging between 760 and 790°C (1400-1450°F). Lowering the forming temperature reduces the amount of alpha case that forms on the part, which must be removed. This provides an opportunity of starting with a lower gauge material. Lower forming temperatures also limit the amount of oxidation and wear on the tool and increase the life of certain press components, such as heaters and platens. A variation of this process is SPF combined with Diffusion Bonding (SPF/DB) of two or more titanium sheets to produce integrally stiffened structures with limited fasteners and less weight than…
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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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Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 45.5Ni - 25.5Cr - 3.2Mo - 3.2W - 18.5Fe Solution Heat Treated

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5717J
  • Current
Published 2020-02-17 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
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Steel, Corrosion Resistant, Sheet and Strip 18Cr - 8Ni (SAE 30301) Cold Rolled, 185 ksi (1276 MPa) Tensile Strength

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5519P
  • Current
Published 2020-02-14 by SAE International in United States
This specification covers a corrosion-resistant steel in the form of sheet and strip 0.005 inch (0.13 mm) and over in nominal thickness (see 8.7).
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Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Texture Controlled Cold Worked, Stress Relieved

AMS G Titanium and Refractory Metals Committee
  • Aerospace Material Specification
  • AMS4946F
  • 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 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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