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Viewing 164041 to 164070 of 169714
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.
1948-05-01
Standard
AMS2414
This specification covers the requirements for electrodeposed lead on metal part.
1948-05-01
Standard
AMS2409
This specification covers the engineering requirements for producing a thin tin coating on aluminum alloys by an immersion process.
1948-05-01
Standard
AMS3120A
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
1948-05-01
Standard
AMS3125A
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
1948-05-01
Standard
AMS3132
null, null
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
1948-05-01
Standard
AMS3170
This specification covers a blend of alcohols and esters in the form of a liquid.
1948-05-01
Standard
AMS3564A
This specification covers vulcanized fiber in the form of sheet. This sheet has been used typically for gaskets and reinforcements on packaging enclosures, but usage is not limited to such applications.
1948-05-01
Standard
AMS3565
ABSTRACT
1948-05-01
Standard
AMS3414
This specification covers an aluminum welding flux in the form of powder.
1948-05-01
Standard
AMS3412
This specification covers the requirements for an aluminum brazing flux in the form of powder or paste. This flux has been used typically for brazing aluminum and aluminum alloys in accordance with AMS2672 at 1050 °F (566 °C) and above, but usage is not limited to such applications.
1948-05-01
Standard
AMS3605A
This specification covers phenol/formaldehyde-resin-impregnated, cotton fabric laminates in the form of sheet. This sheet has been used typically for drawing and bending by the post-forming method into parts where good mechanical and burn resistance properties are important but electrical properties are of secondary importance, and used for fair leads and tubing supports, but usage is not limited to such applications.
1948-05-01
Standard
AMS3607
This specification covers phenol/formaldehyde-resin-impregnated, cotton fabric laminates in the form of sheet. This sheet has been used typically for parts requiring good mechanical properties but where electrical properties are of secondary importance and no post-forming is required, but usage is not limited to such applications. Often used for fairleads and tubing supports.
1948-05-01
Standard
AMS4067A
This specification covers an aluminum alloy in the form of seamless drawn tubing.
1948-05-01
Standard
AMS4065A
This specification covers an aluminum alloy in the form of drawn seamless tubing.
1948-05-01
Standard
AMS4130E
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 materials which may have been widely used previously 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
Standard
AMS3851
ABSTRACT
1948-05-01
Standard
AMS7311
This specification covers a centrifugally-cast, alloyed iron in the form of sleeves for the fabrication of piston rings. Primarily for use as top compression rings in aircraft piston engines. Rings usually require chromium plating for compatibility with the cylinder barrel material.

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