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Viewing 241 to 270 of 37721
2014-09-25
WIP Standard
AMS2241S
This specification covers established manufacturing tolerances applicable to corrosion and heat-resistant steel, iron alloy, titanium, and titanium alloy bars and wire. These tolerances apply to all conditions, unless otherwise noted. The term "excl " is used to apply only to the higher figure of the specified range.
2014-09-25
Standard
J2399_201409
Adaptive cruise control (ACC) is an enhancement of conventional cruise control systems that allows the ACC-equipped vehicle to follow a forward vehicle at a pre-selected time gap, up to a driver selected speed, by controlling the engine, power train, and/or service brakes. This SAE Standard focuses on specifying the minimum requirements for ACC system operating characteristics and elements of the user interface. This document applies to original equipment and aftermarket ACC systems for passenger vehicles (including motorcycles). This document does not apply to heavy vehicles (GVWR > 10,000 lbs. or 4,536 kg). Furthermore, this document does not address other variations on ACC, such as "stop & go" ACC, that can bring the equipped vehicle to a stop and reaccelerate. Future revisions of this document should consider enhanced versions of ACC, as well as the integration of ACC with Forward Vehicle Collision Warning Systems (FVCWS).
2014-09-25
WIP Standard
AMS5355K
This specification covers a corrosion-resistant steel in the form of investment castings.

These castings have been used typically for parts requiring good corrosion resistance and strength up to 600 °F (316 °C), but usage is not limited to such applications.

Certain processing procedures and service conditions may cause these castings to become subject to stress-corrosion cracking; ARP1110 recommends practices to minimize such conditions. Where stress-corrosion is considered to be a factor, precipitation heat treatment should be performed at a temperature not lower than 1000 °F (538 °C).

2014-09-25
WIP Standard
AMS5513K
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate. These products have been used typically for formed and drawn parts requiring corrosion resistance up to 800 °F (427 °C), but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 °F (427 °C) during fabrication may impair corrosion resistance.
2014-09-25
WIP Standard
ARP1313D
This SAE Aerospace Recommended Practice (ARP) describes procedures for the determination of trace elements listed in AMS2280 for Nickel, Cobalt, and Iron-based high temperature alloys. While the materials, methods, applications and processes described or referenced in this procedure may involve the use of hazardous materials, this document does not address the hazards which may be involved in such use. It is the sole responsibility of the user to ensure familiarity with the safe and proper use of any hazardous materials and to take necessary precautionary measures to ensure the health and safety of all personnel involved.
2014-09-25
WIP Standard
AMS5759M
This specification covers a corrosion and heat-resistant cobalt alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts requiring high strength up to 1500 °F (816 °C) and oxidation resistance up to 2000 °F (1093 °C), but usage is not limited to such applications.
2014-09-24
WIP Standard
AMS4773G
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.

2014-09-24
WIP Standard
AMS4774G
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.

2014-09-24
WIP Standard
AMS4771J
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.

2014-09-24
WIP Standard
AMS4772K
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.

2014-09-24
WIP Standard
AMS4766H
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.

2014-09-24
WIP Standard
AMS4765F
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.

2014-09-24
WIP Standard
AMS4769G
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.

2014-09-24
WIP Standard
AMS4768J
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.

2014-09-24
WIP Standard
AMS4767G
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.

2014-09-24
WIP Standard
AMS4770L
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.

2014-09-24
WIP Standard
AMS4788B
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.

2014-09-24
WIP Standard
AMS4860G
This specification covers a leaded red brass alloy in the form of sand and centrifugal castings. These castings have been used typically for parts, such as fittings in fluid conducting lines, where soundness of castings is of prime importance, but usage is not limited to such applications.
2014-09-24
WIP Standard
AMS4855H
This specification covers a leaded red brass alloy in the form of sand and centrifugal castings. These castings have been used typically for parts, such as fittings in fluid conducting lines, where soundness of castings is of prime importance, but usage is not limited to such applications.
2014-09-24
WIP Standard
AMS4822G
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of January 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 ".
2014-09-24
WIP Standard
AMS4824E
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of January 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 ".
2014-09-24
WIP Standard
AMS4156L
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 requiring good surface finish and for hollow, partially enclosed, intricate profiles for which an alloy having good extruding characteristics is required, but usage is not limited to such applications.

2014-09-24
WIP Standard
AMS4070N
This specification covers an aluminum alloy in the form of drawn, round seamless tubing. This tubing has been used typically for ducts requiring small radius bends, but usage is not limited to such applications.
2014-09-24
WIP Standard
AMS4069F
This specification covers an aluminum alloy in the form of drawn, round seamless tubing. This tubing has been used typically for ducts requiring small radius bends, but usage is not limited to such applications.
2014-09-24
WIP Standard
AMS4117K
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire, of flash welded rings, and of 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.
2014-09-24
WIP Standard
AMS4116J
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire, of flash welded rings, and of 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.
2014-09-24
WIP Standard
AMS4115J
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire, of flash welded rings, and of 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.
2014-09-24
WIP Standard
AMS4140K
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.
2014-09-24
WIP Standard
AMS4125L
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.
2014-09-24
WIP Standard
AMS4130N
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.
Viewing 241 to 270 of 37721