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Steel, Corrosion and Heat-Resistant, Bars and Forgings 15.5Cr - 4.5Ni - 2.9Mo - 0.10N Solution Heat Treated, Sub-Zero Cooled, Equalized, and Over-Tempered

1981-04-01
HISTORICAL
AMS5743E
This specification covers a corrosion and heat resistant steel in the form of bars, forgings, and forging stock. These products have been used typically for parts requiring oxidation resistance and high strength up to 800 degrees F (427 degrees C) and where such parts may require welding during fabrication, but usage is not limited to such applications.
Standard

Alloy Bars and Forgings, Corrosion and Heat Resistant, 15cr 45ni 4.1mo 4.1w 3.0ti 1.0al 31fe, Consumable Electrode Vacuum Melted, Solution and Precipitation Heat Treated

1981-04-01
HISTORICAL
AMS5746C
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. These products have been used for parts such as turbine rotors, shafts, blades, bolts, dowels, and fittings, requiring high strength up to 1600°F (871°C) and oxidation resistance up to 1800°F (982°C).
Standard

Nickel Alloy, Corrosion and Heat-Resistant, Seamless Tubing, 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe, Consumable Electrode or Vacuum Induction Melted 1950 °F (1066 °C) Solution Heat Treated

1981-04-01
HISTORICAL
AMS5590A
This specification covers a corrosion and heat resistant nickel alloy in the form of seamless tubing. This tubing has been used typically for fluid lines and structural components requiring high strength at cryogenic temperatures and for short-time service up to 1200 degrees F (649 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C), particularly those parts which are formed or welded and then heat treated to develop desired properties, but usage is not limited to such applications.
Standard

Steel, Corrosion and Heat Resistant, Welded Tubing, 25Cr - 20Ni (SAE 30310), Solution Heat Treated

1981-04-01
HISTORICAL
AMS5577D
This specification covers a corrosion and heat resistant steel in the form of welded tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when such parts are welded during fabrication and for parts requiring oxidation resistance up to 2000 degrees F (1093 degrees C) but useful at that temperature only when stresses are low, but usage is not limited to such applications.
Standard

TOLERANCES Nickel, Nickel Alloy, and Cobalt Alloy Tubing

1981-04-01
HISTORICAL
AMS2263C
This specification covers established inch-pound manufacturing tolerances applicable to seamless and welded thin-wall aircraft tubing of nickel, nickel alloys, and cobalt alloys ordered to inch-pound dimensions. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. The term "excl" is used to apply only to the higher figure of a specified range.
Standard

Standards and Test Methods

1981-04-01
HISTORICAL
AMS2350AT
To establish the issue of specifications, standards, and recommended practices published by standardizing agencies other than divisions and committees of the Aerospace Council of SAE approved for use in determining conformance to requirements of Aerospace Material Specifications (AMS) and other specifications in which this specification is referenced.
Standard

Tolerances, Metric, Nickel, Nickel Alloy, and Cobalt Alloy Tubing

1981-04-01
HISTORICAL
MAM2263
This specification covers established metric manufacturing tolerances applicable to seamless and welded thin-wall aircraft tubing of nickel, nickel alloys, and cobalt alloys ordered to metric dimensions. These tolerances apply to all conditions and are based on individual measurements, unless otherwise noted. The term "excl" is used to apply only to the higher figure of a specified range.
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