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Bolt, Machine - Double Hexagon Extended Washer Head, Drilled, Pd Shank, Silver Plated, Nickel Alloy, UNS N07718, 185 ksi Min, .3750-24 UNJF-3A

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3253D
  • Current
Published 2019-06-03 by SAE International in United States

Scope is unavailable.

 
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Nickel-Iron Alloy, Magnetic, Sheet and Strip 50Ni - 50Fe Annealed, Forming Grade

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS7717E
  • Current
Published 2019-05-29 by SAE International in United States
This specification covers a magnetically soft nickel-iron alloy in the form of sheet and strip.
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Nickel-Iron Alloy, Magnetic, Bars, Rods, Tubing, and Forgings 50Ni - 50Fe

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS7718H
  • Current
Published 2019-05-29 by SAE International in United States
This specification covers a magnetically soft nickel-iron alloy in the form of bars, rods, forgings, mechanical tubing, and forging stock.
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Bolt, Machine - Double Hexagon Extended Washer Head, Drilled, Pd Shank, Nickel Alloy, UNS N07718, 185 ksi Min, .5625-18 UNJF-3A

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS3249D
  • Current
Published 2019-05-24 by SAE International in United States

Scope is unavailable.

 
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Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS2261L
  • Current
Published 2019-05-10 by SAE International in United States

This specification covers established manufacturing tolerances applicable to bars, rods, and wire of nickel, nickel alloy, and cobalt alloys ordered to inch-pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of a specified range.

 

Cobalt Alloy, Corrosion and Heat Resistant, Hardfacing Rod and Wire 62Co - 27Cr - 2.9Ni - 5.5Mo

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5819A
  • Current
Published 2019-04-30 by SAE International in United States
This specification covers a corrosion and heat-resistant cobalt alloy in the form of welding rods or wrought wire.
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CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
  • Aerospace Standard
  • AS8443
  • Current
Published 2019-04-29 by SAE International in United States
No Abstract Available.
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Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 7.0Fe - 2.5Ti - 1.0Cb (Nb) - 0.70Al 2100 °F (1149 °C) Solution and Precipitation Heat Treated

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5668K
  • Current
Published 2019-04-11 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 10.0 inches (254 mm) and under in nominal diameter or distance between parallel sides, and stock of any size for forging, flash welded rings, or heading (see 8.6).
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Nickel Alloy, Corrosion and Heat-Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95 (Cb (Nb) + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode, Remelted or Vacuum Induction Melted, Solution Heat Treated, Precipitation-Hardenable

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5598F
  • Current
Published 2019-04-11 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet and strip up to 0.187 inch (4.75 mm) thick, inclusive, and plate up to 4.000 inches (101.6 mm) thick, inclusive, procured in inch/pound units (see 8.6).
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Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
  • Aerospace Standard
  • AS5960C
  • Current
Published 2019-04-11 by SAE International in United States
This document defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic braid reinforced, hose assembly suitable for use in 400 °F (204 °C), 5080 psi (35000 kPa) aircraft hydraulic systems.
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