Refine Your Search

Topic

Search Results

Standard

Standards and Test Methods

1981-07-01
HISTORICAL
AMS2350AV
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

COATING, PLASMA SPRAY DEPOSITION

1981-07-01
HISTORICAL
AMS2437A
This specification covers the engineering requirements for applying coatings to parts by the plasma spray process and the properties of such coatings.
Standard

Cobalt Alloy, Corrosion and Heat-Resistant, Welding Wire 54Co - 25.5Cr - 10.5Ni - 7.5W

1981-07-01
HISTORICAL
AMS5789A
This specification covers a corrosion and heat resistant cobalt alloy in the form of welding wire. This wire has been used typically as as filler metal for gas-metal-arc or gas-tungsten-arc welding of parts fabricated from similar or dissimilar corrosion and heat resistant steels or alloys, but usage is not limited to such applications.
Standard

Steel, Corrosion and Heat-Resistant, Welding Wire, 16.5Cr - 4.5Ni - 2.9Mo - 0.10N

1981-07-01
HISTORICAL
AMS5774B
This specification covers a corrosion and heat resistant steel in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-arc or gas-metal-arc welding of parts fabricated from steels or alloys of similar composition requiring joints with strength and corrosion resistance comparable to those of the basis metal, but usage is not limited to such applications.
Standard

Steel, Low Carbon, Bars, Forgings, Tubing, Sheet, Strip, and Plate, 0.25 Carbon, Maximum

1981-07-01
HISTORICAL
AMS5062D
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
Standard

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

1981-07-01
HISTORICAL
AMS5597B
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

RADIOGRAPHIC INSPECTION

1981-07-01
HISTORICAL
AMS2635C
This specification covers the procedures for radiographic inspection.
Standard

COATING OF FASTENERS Aluminum Filled, Ceramic Bonded Coating

1981-07-01
HISTORICAL
AMS2506B
This specification covers the procedure for application to fasteners of a corrosion and heat resistant aluminum coating material having a thermosetting inorganic binder and the properties of the finished coating.
Standard

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

1981-07-01
HISTORICAL
AMS4182C
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.
X