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Nickel Alloy, Corrosion and Heat Resistant, Forgings 57Ni 19.5Cr 13.5Co 4.3Mo 3.0Ti 1.4Al 0.05Zr 0.006B, Consumable Electrode or Vacuum Induction Melted, 1825 to 1900°F (996 to 1038°C) Solution, Stabilization, and Precipitation Heat Treated

1982-01-01
HISTORICAL
AMS5704C
This specification covers a corrosion and heat resistant nickel alloy in the form of forgings and forging stock. These forgings have been used typically for rotating parts, such as compressor blades, discs, hubs, shafts, and spacers requiring high strength up to 1500 degrees F (816 degrees C) and oxidation resistance up to 1750 degrees F (954 degrees C), but usage is not limited to such applications.
Standard

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 57Ni 19.5Cr 13.5Co 4.3Mo 3.0Ti 1.4Al 0.006B 0.05Zr Consumable Electrode or Vacuum Induction Melted 1825 to 1900°F Solution Heat Treated

1982-01-01
HISTORICAL
AMS5706F
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading procured in inch/pound units. MAM 5706 is the metric version of this AMS. These products have been used typically for parts, such as fasteners, flanges, and rings, requiring high strength up to 1500 degrees F and oxidation resistance up to 1750 degrees F, 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, Corrosion and Heat-Resistant, Bars, Forgings and Rings, 74Ni - 7.0Cr - 16.5Mo, Solution Heat Treated

1982-01-01
HISTORICAL
AMS5771B
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts, such as turbine air-sealing components, requiring moderate strength up to 1400 °F (760 °C) and oxidation resistance up to 1600 °F (871 °C), particularly where a low coefficient of expansion is desirable, but usage is not limited to such applications.
Standard

Core, Flexible Honeycomb, Polyamide Paper Base, Phenolic Coated

1982-01-01
HISTORICAL
AMS3713
This specification covers honeycomb core made of polymide paper sheets in a non-hexagonal, flexible cell configuration and supplied in the form of blocks, slices, and ordered shapes. This honeycomb core has been used tyipcally in sandwich structures in single or compound curvature parts requiring high strength and corrosion resistance in the temperature range -55 to +82 degrees C (-67 to +180 degrees F) but usage is not limited to such applications.
Standard

Fabric, Glass (181) (Decorative Grade)

1982-01-01
CURRENT
AMS3835
This specification is declared "CANCELLED" by the Aerospace Materials Division, SAE, as of 1-1-82. By this action, subject specification number and title will be deleted from the active specification index of Aerospace Material Specifications. This fabric style is no longer manufactured. See the latest issue of AMS 3824 for other glass cloth styles.
Standard

Fabric, Glass (181) (Chrome Treated)

1982-01-01
CURRENT
AMS3825
This specification was declared "NONCURRENT"^by the Aerospace Materials Division, SAE, as of 2-1-56. It was recommended that this specification not be specified for new designs. This cover sheet should be attached to the initial issue of the subject specification. This specification is declared J/CANCELLED" by the Aerospace Materials Division, SAE, as of 1-1-82. By this acfflWP^Wfft^c^^pecification number and title will be deleted from the active specification index of Aerospace Material Specifications. This fabric style is no longer manufactured. See the latest issue of AMS 3824 for other glass cloth styles.
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