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Viewing 36781 to 36810 of 43275
1968-11-01
Standard
AMS6467A
This specification covers a low-alloy steel in the form of covered welding electrodes.
1968-11-01
Standard
AMS5799A
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of April 1996 and has been superseded by AWS A5.11 ENiCrMo-2.
1968-11-01
Standard
AMS5310C
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of November 1994. It is recommended, therefore, that this specification not be specified for new designs.
1968-11-01
Standard
AMS4168C
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These products have been used typically for parts subject to excessive warpage during machining 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 extrusions to become susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.
1968-11-01
Standard
AMS4908B
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of April 1994. It is recommended, therefore, that this specification not be specified for new designs.
1968-11-01
Standard
AMS4022D
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: Alclad 6061-T4 (Sheet)/6061-T451 (Plate) UNS Number: A86061
1968-11-01
Standard
J370_196811
This SAE Recommended Practice covers the use of preferred bolt and capscrew sizes, wherever applicable, on construction and industrial machinery to ease serviceability. Designers, in their efforts to determine the proper fastener for heavy equipment, sometimes overlook the practical aspects of serviceability. When a particular component requires frequent service, it is much faster and easier for the serviceman to work with common size, easily distinguished bolts and capscrews which require a minimum of tools. Section 4 lists eight diameters of recommended bolts and capscrews, some of which can be found in any hardware store, require only standard tools, are easy to distinguish, and at the same time cover proof loads from 1043 kg (2300 lb) on up at convenient intervals. While some applications may require other sizes and/or fine threaded fasteners for greater camping forces and/or area restrictions, the convenience of UNC threads in the sizes indicated is preferred wherever possible.
1968-11-01
Standard
J853A_196811
This SAE Standard has been established to provide direction for the design and installation of a Vehicle Identification Number assigned to a passenger car or truck. In adhering to these standards, facility of application in factory production and appearance are matters for manufacturer control.
1968-11-01
Standard
AMS5588B
This specification covers a corrosion and heat-resistant nickel alloy in the form of welded and drawn tubing.
1968-11-01
Standard
AMS4166
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These products have been used typically for parts requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such applications.
1968-11-01
Standard
AMS2673A
This specification covers the engineering requirements for producing brazed joints of aluminum and aluminum alloys by immersion in molten flux bath.
1968-11-01
Standard
AMS2813B
This specification covers spooling and packaging of bare welding wire to ensure cleanliness but with minimum environmental protection, spool sizes and weights of spooled wire, and package weights of cut lengths.
1968-11-01
Standard
AMS2816E
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
1968-11-01
Standard
AMS7273
This specification covers a fluorosilicone (FVMQ) rubber in the form of molded rings.
1968-11-01
Standard
AMS7498C
This specification covers flash welded rings made of titanium and selected titanium alloys.
1968-11-01
Standard
AMS5047A
This specification covers an aluminum-killed carbon steel in the form of sheet and strip.
1968-11-01
Standard
AMS4071G
This specification covers an aluminum alloy in the form of drawn, round seamless tubing. This tubing has been used typically for parts, such as hydraulic systems and fuel and oil lines, but usage is not limited to such applications.
1968-11-01
Standard
AMS4031B
This specification covers an aluminum alloy in the form of sheet and plate supplied in the annealed (O) condition. When specified, product shall be supplied in the "as fabricated" (F) temper.
1968-11-01
Standard
AMS2510C
1968-11-01
Standard
AMS4784
This specification covers a gold-palladium-nickel alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, chips, preforms, and a viscous mixture (paste) of the powder in a suitable binder.
1968-11-01
Standard
AMS4169D
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These extrusions have been used typically for parts subject to excessive warpage during machining 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; SAE ARP 823 recommends practices to minimize such conditions.
1968-11-01
Standard
AMS4041J
This specification covers an aluminum alloy in the form of sheet and plate clad on both sides with a different aluminum alloy.
1968-11-01
Standard
AMS5754F
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.
1968-11-01
Standard
AMS4083F
This specification covers an aluminum alloy in the form of seamless round tubing.
1968-11-01
Standard
AMS5587B
This specification covers a corrosion and heat resistant nickel alloy in the form of seamless tubing.
1968-11-01
Standard
AMS6427D
This specification covers an aircraft quality, low alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts requiring a combination of high tensile strength and good ductility with relatively high impact strength and hardness, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment. ARP1110 recommends practices to minimize such conditions.
1968-11-01
Standard
AMS2350L
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.
1968-11-01
Standard
AMS6277A
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.