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Viewing 164041 to 164070 of 184351
1968-05-01
Standard
AMS4395B
This specification covers a magnesium alloy in the form of welding wire.
1968-05-01
Standard
AMS5085A
This specification covers a carbon steel in the form of sheet, strip, and plate.
1968-05-01
Standard
AMS4153F
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes and tubing. These products have been used typically for parts requiring good strength and where fabrication does not usually involve welding, but usage is not limited to such applications. Certain design and processing procedures may cause these extrusions to be susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.
1968-05-01
Standard
AMS4154J
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing.
1968-05-01
Standard
AMS4975
This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock for flash welded rings.
1968-05-01
Standard
AMS5069A
This specification covers a low-carbon steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts requiring low strength and high ductility, but usage is not limited to such applications.
1968-05-01
Standard
AMS5040F
This specification covers a carbon steel in the form of sheet and strip.
1968-05-01
Standard
AMS2350K
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.
1968-05-01
Standard
AMS4116C
This specification covers an aluminum alloy in the form of bars, rods, and wire. These products have been used typically for parts requiring moderate ductility, formability, and response to precipitation heat treatment, but usage is not limited to such applications.
1968-05-01
Standard
AMS4150E
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing, flash welded rings fabricated from extruded stock, and stock for flash welded rings. These products have been used typically for parts requiring moderate strength, especially where such parts require brazing or welding during fabrication, but usage is not limited to such applications.
1968-05-01
Standard
AMS4765
This specification covers a silver alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, chips, and a viscous mixture (paste) of powder in a suitable binder. This material has been used typically for joining ferrous metals, particularly austenitic steels and alloys, by atmosphere furnace brazing without flux, where high joint strength up to 800 degrees F (427 degrees C) is required, or for nonferrous metals except those having base of aluminum or magnesium, but usage is not limited to such applications.
1968-05-01
Standard
AMS4123D
This specification covers an aluminum alloy in the form of bars and rods. These products have been used typically for machined parts subject to excessive warpage during machining due to residual stresses and for parts requiring high strength and whose fabrication does not involve welding or forming, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.
1968-05-01
Standard
AMS4951B
This specification covers one grade of commercially pure titanium in the form of wire for welding filler metal.
1968-05-01
Standard
AMS5706C
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.
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
AMS4976
This specification covers a titanium alloy in the form of forgings and forging stock.
1968-05-01
Standard
AMS6487C
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
1968-05-01
Standard
AMS2667A
This specification covers the engineering requirements for producing brazed joints in parts fabricated from austenitic corrosion and heat resistant steels, but may also be used on carbon or low-alloy steels or copper alloys, and the properties of such joints.
1968-05-01
Standard
AMS4935B
This specification covers a titanium alloy in the form of extruded bars and shapes, flash welded rings, and stock for flash welded rings. These products have been used typically for parts that do not require heat treatment but require high mechanical properties in the annealed condition and for which processing above the beta transus is permissible, but usage is not limited to such applications. This alloy exhibits high strength-to-weight ratios up to 750 °F (399 °C).
1968-05-01
Standard
AMS4118E
This specification covers an aluminum alloy in the form of bars, rods, and wire. These products have been used typically for parts requiring good strength and whose fabrication does not involve welding, but usage is not limited to such applications.
1968-05-01
Standard
AMS4036C
This specification covers an aluminum alloy in the form of sheet and plate clad on one side with a different aluminum alloy.
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
AMS4063
This specification covers an aluminum alloy in the form of clad sheet.
1968-05-01
Standard
AMS4064
This specification covers an aluminum alloy in the form of clad sheet.
1968-05-01
Standard
AMS4455A
This specification covers a magnesium alloy in the form of investment castings.
1968-05-01
Standard
AMS4420J
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
AMS4443B
This specification covers a magnesium alloy in the form of sand castings.
1968-05-01
Standard
AMS4437A
This specification covers a magnesium alloy in the form of sand castings. These products have been used typically for parts operating in service up to 300 degrees F (149 degrees C) but usage is not limited to such applications.
1968-05-01
Standard
AMS4453A
This specification covers a magnesium alloy in the form of investment castings.

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