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Viewing 36781 to 36810 of 43038
1968-05-01
Standard
AMS4447B
This specification covers a magnesium alloy in the form of sand castings.
1968-05-01
Standard
AMS4440B
This specification covers a magnesium alloy in the form of sand castings. Primarily for parts operating in service in the range 300 degrees - 500 degrees F (150 degrees - 260 degrees C).
1968-05-01
Standard
AMS4455A
This specification covers a magnesium alloy in the form of investment castings.
1968-05-01
Standard
AMS4441B
This specification covers a magnesium alloy in the form of sand castings.
1968-05-01
Standard
AMS4453A
This specification covers a magnesium alloy in the form of investment castings.
1968-05-01
Standard
AMS4443B
This specification covers a magnesium alloy in the form of sand castings.
1968-05-01
Standard
AMS4424G
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of August, 1992. It is recommended, therefore, that this specification not be specified for new designs.
1968-05-01
Standard
AMS4445C
This specification covers a magnesium alloy in the form of sand castings.
1968-05-01
Standard
AMS4444A
This specification covers a magnesium alloy in the form of sand castings.
1968-05-01
Standard
AMS4483A
This specification covers a magnesium alloy in the form of permanent mold castings.
1968-05-01
Standard
AMS4484F
This specification covers a magnesium alloy in the form of permanent mold castings.
1968-05-01
Standard
AMS3693
This specification covers a modified epoxy adhesive in the form of supported film supplied in rolls or sheets.
1968-05-01
Standard
ARP953A
This document establishs limits or parameters for designing bolt heads with proper control of flowlines to assure sufficient strength to resist stresses induced by static or dynamic loads without being affected by lightening and lockwire holes.
1968-05-01
Standard
ARP936
This recommended practice describes the requirements of a special purpose 10µF feed through capacitor to be used in series with the power line to an electrical or electronic device during EMI tests.
1968-05-01
Standard
AMS7724
This specification covers a corrosion and heat resistant iron alloy sintered wire mesh in the form of sheet and strip.
1968-05-01
Standard
AMS4162
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These extrusions have been used typically for structural parts requiring high strength up to 500 degrees F (260 degrees C), but usage is not limited to such applications. May be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking.
1968-05-01
Standard
AMS3196B
ABSTRACT
1968-05-01
Standard
AMS5132D
This specification covers a high-carbon steel in the form of bars.
1968-05-01
Standard
AMS4909B
This specification covers a titanium alloy in the form of sheet, strip, and plate.
1968-05-01
Standard
AMS5120E
This specification covers a carbon steel in the form of strip. This product has been used typically for heat treated springs, spring pins, shims, spacers, and other applications where spring temper is required, but usage is not limited to such applications.
1968-05-01
Standard
AMS5121C
This specification covers a carbon steel in the form of sheet and strip. This material has been used typically for heat treated springs, shims, spacers, and other applications where spring temper is required, but usage is not limited to such applications.
1968-05-01
Standard
AMS5122C
This specification covers a carbon steel in the form of strip. This material hs been used typically for washers and other stamped parts requiring a smooth finish and only slight or no forming, but usage is not limited to such applications.
1968-05-01
Standard
AMS5062B
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.
1968-05-01
Standard
AMS5050F
This specification covers a low-carbon steel in the form of seamless tubing. This tubing has been used typically for oil lines and other parts requiring high-quality tubing suitable for severe forming and for welding or brazing, but usage is not limited to such applications.
1968-05-01
Standard
AMS5060C
This specification covers a low-carbon steel in the form of bars, forgings, mechanical tubing, and forging stock.
1968-05-01
Standard
AMS4490E
This specification covers a magnesium alloy in the form of die castings.
1968-05-01
Standard
AMS2420A
This specification covers the requirements for preparation of aluminum and aluminum alloys for soldering by zinc immersion pre-treatment followed by copper plating and tin or tin-zinc alloy plating.
1968-05-01
Standard
AMS4651
This specification covers a copper-beryllium alloy in the form of bars and rods. These products have been used typically for parts requiring high strength with good electrical conductivity and the nonmagnetic properties are important, but usage is not limited to such applications.
1968-05-01
Standard
AMS4782
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of 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.