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SAE - American standards - Page 2649

Standards SAE - American standards - Page 2649

SAE – The company, SAE International, is a global association of more than 128,000 engineers and other related technical experts from the area of aerospace and aircraft industry, automotive industry and commercial-vehicle industry. The main activity of SAE International is life-long learning and the development of standards stated on the principle of consensus. SAE International has got its charitable branch called SAE Foundation, which supports a lot of programs including the program A World In Motion® and the program Collegiate Design Series.

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Preview SAE AMS5663C 1.5.1972
SAE AMS5663C Historical

ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT Nickel Base - 19Cr - 3.1Mo - 5.1(Cb + Ta) - 0.90Ti - 0.50Al - 19Fe Consumable Electrode or Vacuum Induction Melted 1750 F (954.4 C) Solution and Precipitation Heat Treated

Historical published on 1.5.1972

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Preview SAE AMS5663D 1.10.1980
SAE AMS5663D Historical

ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 52.5Ni - 19Cr - 3.0Mo - 5.1(Cb + Ta) - 0.90Ti - 0.50Al - 19Fe Consumable Electrode or Vacuum Induction Melted 1750°F (955°C) Solution and Precipitation Heat Treated

Historical published on 1.10.1980

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105.10 USD


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Preview SAE AMS5663E 1.4.1987
SAE AMS5663E Historical

ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 52.5Ni - 19Cr - 3.0Mo - 5.1(Cb + Ta) - 0.90Ti - 0.50Al - 19Fe Consumable Electrode or Vacuum Induction Melted 1750°F (955°C) Solution and Precipitation Heat Treated

Historical published on 1.4.1987

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electronic design (pdf) (121.90 USD)


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121.90 USD


IN STOCK
Preview SAE AMS5663F 1.1.1989
SAE AMS5663F Historical

ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 52.5Ni - 19Cr - 3.0Mo - 5.1(Cb + Ta) - 0.90Ti - 0.50Al - 19Fe Consumable Electrode or Vacuum Induction Melted 1775°F (968°C) Solution and Precipitation Heat Treated

Historical published on 1.1.1989

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electronic design (pdf) (114.00 USD)


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114.00 USD


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Preview SAE AMS5663G 1.7.1989
SAE AMS5663G Historical

ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT 52.5Ni - 19Cr - 3.0Mo - 5.1(Cb + Ta) - 0.90Ti - 0.50Al - 19Fe Consumable Electrode or Vacuum Induction Melted 1775°F (968°C) Solution and Precipitation Heat Treated

Historical published on 1.7.1989

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electronic design (pdf) (114.00 USD)


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114.00 USD


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Preview SAE AMS5663H 1.1.1996
SAE AMS5663H Historical

NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS, FORGINGS, AND RINGS 52.5Ni - 19Cr - 3.0Mo - 5.1Cb - 0.90Ti - 0.50Al - 19Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution and Precipitation Heat Treated

Historical published on 1.1.1996

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electronic design (pdf) (110.00 USD)


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110.00 USD


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Preview SAE AMS5663J 1.9.1997
SAE AMS5663J Historical

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution and Precipitation Heat Treated

Historical published on 1.9.1997

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electronic design (pdf) (114.00 USD)


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114.00 USD


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Preview SAE AMS5663K 1.11.2002
SAE AMS5663K Historical

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution and Precipitation Heat Treated

Historical published on 1.11.2002

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114.00 USD


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Preview SAE AMS5663L 1.7.2003
SAE AMS5663L Historical

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution and Precipitation Heat Treated

Historical published on 1.7.2003

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114.00 USD


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Preview SAE AMS5663M 1.6.2009
SAE AMS5663M Historical

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution and Precipitation Heat Treated

Historical published on 1.6.2009

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114.00 USD


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