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Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate, 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

1988-07-01
HISTORICAL
AMS5597C
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate. These products have been used typically for parts, such as cases and ducts, requiring high strength at cryogenic temperatures and for short time use up to 1000 °F (538 °C), particularly those parts which are formed or welded and then heat treated to develop required properties, but usage is not limited to such applications.
Standard

Nickel Alloy, Brazing Filler Metal 73Ni 4.5Si 14Cr 3.1B 4.5Fe (Low Carbon) 1790 to 1970°F (977 to 1077°C) Solidus-Liquidus Range

1988-07-01
HISTORICAL
AMS4776C
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder. This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. Also may be used as a corrosion and oxidation resistant hard coating.
Standard

Aluminum Alloy, Wire, 5.0Mg - 0.12Mn - 0.12Cr (5056-0), Annealed

1988-07-01
HISTORICAL
AMS4182D
This specification covers an aluminum alloy in the form of wire. This wire has been used typically for the manufacture of screen for reinforcement of, and to provide electrical conductivity through, rubber gaskets, but usage is not limited to such applications.
Standard

Silicone Potting Compound, Elastomeric, Two-Part, General Purpose, 200 - 600 Poise Viscosity

1988-07-01
CURRENT
AMS3360
This specification covers a room-temperature-vulcanizing, elastomeric silicone compound. Primarily for potting and encapsulating electronic products for use at temperatures from -65 to +260 degrees C (-85 to +500 degrees F) where resistance to reversion is not required. This specification has been "Cancelled" by the Aerospace Materials Division, SAE, as of October 26, 1987. By this action subject specification number and title will be deleted from the active specification index of Aerospace Material Specifications. For those components previously requiring the use of AMS 3360, either of the following are recommended for use, as applicable: AMS 3358 or AMS 3359.
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