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Standard

Iron Castings, Pearlitic Malleable

1951-06-01
HISTORICAL
AMS5310B
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of November 1994. It is recommended, therefore, that this specification not be specified for new designs.
Standard

Iron-Nickel Alloy, Strip, 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al, Solution Heat Treated, Cold Rolled, 50% Reduction

1963-07-01
HISTORICAL
AMS5225A
This specification covers an iron-nickel alloy in the form of strip. This strip has been used typically for diaphragms, leaf springs, and helical springs, requiring a precipitation-hardenable alloy with a temperature coefficient of modulus of elasticity of -20 to +20 x 10-6 per degree Fahrenheit from -50 to +150 °F (-36 to +36 x 10-6 per degree Celsius from -46 to +66 °C) after suitable heat treatment, but usage is not limited to such applications.
Standard

Iron-Nickel Alloy, Strip, 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al, Solution Heat Treated, Cold Rolled, 50% Reduction

1974-12-01
HISTORICAL
AMS5225B
This specification covers an iron-nickel alloy in the form of strip. This strip has been used typically for diaphragms, leaf springs, and helical springs, requiring a precipitation-hardenable alloy with a temperature coefficient of modulus of elasticity of -20 to +20 x 10-6 per degree Fahrenheit from -50 to +150 °F (-36 to +36 x 10-6 per degree Celsius from -46 to +66 °C) after suitable heat treatment, but usage is not limited to such applications.
Standard

Iron-Nickel Alloy, Strip, 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al, Solution Heat Treated, Cold Rolled, 50% Reduction

1982-04-01
HISTORICAL
AMS5225C
This specification covers an iron-nickel alloy in the form of strip. This strip has been used typically for diaphragms, leaf springs, and helical springs, requiring a precipitation-hardenable alloy with a temperature coefficient of modulus of elasticity of -20 to +20 x 10-6 per degree Fahrenheit from -50 to +150 °F (-36 to +36 x 10-6 per degree Celsius from -46 to +66 °C) after suitable heat treatment, but usage is not limited to such applications.
Standard

Iron-Nickel Alloy, Strip, 49Fe - 5.3Cr - 42Ni - 2.5Ti - 0.55Al, Solution Heat Treated, Cold Rolled, 50% Reduction

1955-08-01
HISTORICAL
AMS5225
This specification covers an iron-nickel alloy in the form of strip. This strip has been used typically for diaphragms, leaf springs, and helical springs, requiring a precipitation-hardenable alloy with a temperature coefficient of modulus of elasticity of -20 to +20 x 10-6 per degree Fahrenheit from -50 to +150 °F (-36 to +36 x 10-6 per degree Celsius from -46 to +66 °C) after suitable heat treatment, but usage is not limited to such applications.
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