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Viewing 164041 to 164070 of 169735
1948-07-01
Standard
AMS3201C
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. These products have been typically used for parts, such as packings, bushings, grommets, and applications requiring resistance to dry heat, but usage is not limited to such applications. Each application should be considered individually.
1948-07-01
Standard
AMS4086B
This specification covers an aluminum alloy in the form of drawn, round, seamless hydraulic tubing.
1948-07-01
Standard
AMS4114
This specification covers an aluminum alloy in the form of bars and rods.
1948-07-01
Standard
AMS4102
This specification covers an aluminum alloy in the form of bars, rods, and wire. Primarily for parts requiring good formability and weldability in fabrications where strength is unimportant.
1948-07-01
Standard
AMS5540C
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
1948-07-01
Standard
AMS5680A
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 corrosion and heat resistant steels and alloys, but usage is not limited to such applications.
1948-07-01
Standard
AMS5665A
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.
1948-07-01
Standard
AMS5376
This specification covers a corrosion and heat resistant iron alloy in the form of investment castings.
1948-07-01
Standard
AMS2406A
This specification covers the requirements for electrodeposited hard chromium plate.
1948-06-01
Magazine
1948-06-01
Standard
AMS7301
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.
1948-05-01
Magazine
1948-05-01
Standard
AMS2205A
This specification covers established manufacturing tolerances applicable to aluminum alloy and magnesium alloy extruded bar, rod, wire, shapes, and tubing ordered to inch/pound dimensions. Tolerances greater than standard may be necessary for some shapes; tolerances closer than standard may be possible for others. Tolerances shown here, however, apply unless otherwise agreed upon by purchaser and vendor and apply to all tempers, unless otherwise noted.
1948-05-01
Standard
AMS3640
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.
1948-05-01
Standard
AMS5030
This specification covers a low-carbon steel in the form of welding wire.
1948-05-01
Standard
AMS5392
This specification covers a moderate corrosion and heat resistant alloy iron in the form of sand castings.
1948-05-01
Standard
AMS5651
This specification covers a corrosion and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
1948-05-01
Standard
AMS5681
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996, and has been superseded by AWS A5.4 E347. Alloy: 30347 UNS Number: W34710
1948-05-01
Standard
AMS5575D
This specification covers a corrosion and heat-resistant steel in the form of welded tubing.
1948-05-01
Standard
AMS5570E
This specification covers a corrosion and heat resistant steel in the form of seamless tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when such parts are welded during fabrication, and also for parts requiring oxidation resistance up to 1500 degrees F (816 degrees C) but useful at that temperature only when stresses are low; usage is not limited to such applications.
1948-05-01
Standard
AMS5626
This specification has been 'Cancelled' by the Aerospace Materials Division, SAE, as of January 1997. Alloy: T1 UNS Number: T12001
1948-05-01
Standard
AMS4824
This specification covers bearings of a leaded bronze cast on one or both faces of a steel backing with a layer of babbitt metal cast on the leaded bronze.
1948-05-01
Standard
AMS4180
This specification covers an aluminum alloy in the form of wire.
1948-05-01
Standard
AMS4184
This specification covers an aluminum alloy in the form of wire, sheet, foil, pig, grains, shot, and chips.
1948-05-01
Standard
AMS4190
This specification covers an aluminum alloy in the form of welding wire. This wire has been used typically as filler metal for gas-metal-arc or gas-tungsten-arc welding of aluminum alloys of similar composition, but usage is not limited to such applications.
1948-05-01
Standard
AMS5565B
This specification covers a corrosion-resistant steel in the form of welded tubing. This tubing has been used typically for parts, such as fluid-conducting lines not subjected to high pressure, requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 degrees F (427 degrees C) during fabrication may impair corrosion resistance.
1948-05-01
Standard
AMS5768
This specification covers a corrosion and heat resistant iron-chromium-nickel-cobalt alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
1948-05-01
Standard
AMS2485
This specification covers the requirements for black oxide coatings on parts.
1948-05-01
Standard
AMS2261
null, null
This specification covers established manufacturing tolerances applicable to bars, rods, and wire of nickel, nickel alloy, and cobalt alloys ordered to inch-pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of a specified range. Where the terms “nickel”, “nickel-copper”, “nickel-chromium”, “nickel-molybdenum”, “nickel-molybdenum-chromium”, and “cobalt” are used without qualification, they refer to both non-heat-treatable and heat-treatable alloys as applicable, unless otherwise noted.

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