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Viewing 163861 to 163890 of 190966
HISTORICAL
1974-12-15
Standard
AMS6299B
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 to be carburized requiring high minimum core hardness with wide range in sections 0.375 inch (9.5 mm) and under in thickness, but usage is not limited to such applications. The core may or may not be machinable after hardening.
HISTORICAL
1974-12-15
Standard
AMS6485C
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
HISTORICAL
1974-12-15
Standard
AMS4223
This specification covers an aluminum alloy in the form of castings.
HISTORICAL
1974-12-15
Standard
AMS6487D
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
HISTORICAL
1974-12-15
Standard
AMS4218C
This specification covers an aluminum alloy in the form of sand, permanent mold, composite mold, and investment castings.
HISTORICAL
1974-12-15
Standard
AMS6448D
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1974-12-15
Standard
AMS6526A
This specification covers a premium aircraft-quality, high-strength, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1974-12-15
Standard
AMS4941A
This specification covers one grade of commercially pure titanium in the form of welded tubing.
HISTORICAL
1974-12-15
Standard
AMS6466B
This specification covers a low-alloy steel in the form of welding wire. Primarily for use as filler metal for gas-tungsten-arc and gas-metal-arc welding of low-alloy steels where response to heat treatment is required in the weld.
HISTORICAL
1974-12-15
Standard
AMS6382H
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1974-12-15
Standard
AMS4982
The specification covers a titanium alloy in the form of wire.
HISTORICAL
1974-12-15
Standard
AMS2259A
This specification defines limits of variation for determining acceptability of the composition of wrought low-alloy and carbon steel parts and material acquired from a producer.
HISTORICAL
1974-12-15
Standard
AMS6490C
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
1974-12-04
Standard
RS729-1
No scope available.
CURRENT
1974-12-02
Standard
ARIC573-7
This standard provides design guidance for the development and installation of an expandable Flight Data Acquisition and Recording System. The functions defined include flight data acquisition through suitable electrical interfaces, conversion of analog input signals into a standard serial data output and the capability for expansion to permit increased data handling capacity.
HISTORICAL
1974-12-01
Standard
AMS3598B
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1995.
HISTORICAL
1974-12-01
Standard
AMS5223B
This specification covers an iron-nickel alloy in the form of strip.
HISTORICAL
1974-12-01
Standard
AMS3712
This specification covers expanded honeycomb core made of glass cloth impregnated with polyimide resin and supplied in the form of blocks, slices, and ordered shapes. This core has been used typically for bonded sandwich structures requiring high strength and corrosion resistance for long-term service up to 450 degrees F (232 degrees C) and short duration up to 700 degrees F (371 degrees C), but usage is not limited to such applications.
HISTORICAL
1974-12-01
Standard
AMS3380B
This specification covers polytetrafluoroethylene resin in the form of extruded and sintered flexible hose reinforced with wire braid.
HISTORICAL
1974-12-01
Standard
AMS7269
This specification covers a special, low-outgassing silicone rubber compound in the form of molded rings.
HISTORICAL
1974-12-01
Standard
J211B_197412
This SAE Recommended Practice outlines a series of performance recommendations which concern the whole data channel. These recommendations are not subject to any variation and all of them should be adhered to by any agency conducting tests to this practice. However, the method of demonstrating compliance with the recommendations is flexible and can be adapted to suit the needs of the particular equipment the agency is using. It is not intended that each recommendation be taken in a literal sense, as necessitating a single test to demonstrate that the recommendation is met. Rather, it is intended that any agency proposing to conduct tests to this document should be able to demonstrate that if such a single test could be and were carried out, then their equipment would meet the recommendations. This demonstration should be undertaken on the basis of reasonable deductions from evidence in their possession, such as the results of partial tests.
HISTORICAL
1974-12-01
Standard
AMS5593B
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring heat and oxidation resistance up to 2150 degrees F (1177 degrees C), particularly where such parts may require welding during fabrication, but usage is not limited to such applications.
HISTORICAL
1974-12-01
Standard
AMS5603A
This specification covers a corrosion-resistant, precipitation-hardenable steel in the form of sheet and strip.
HISTORICAL
1974-12-01
Standard
AMS5634A
This specification covers a corrosion and heat resistant, iron-nickel alloy in the form of bars, wire, forgings, and forging stock.
HISTORICAL
1974-12-01
Standard
AMS5633B
This specification has been "CANCELLED" by the Aerospace Materials, Division, SAE, as of July 1, 1993.
HISTORICAL
1974-12-01
Standard
AMS5673C
This specification covers a corrosion and heat resistant steel in the form of spring-temper wire.
HISTORICAL
1974-12-01
Standard
AMS5751B
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. Primarily for parts, such as turbine components, requiring high strength up to 1600 degrees F (870 degrees C) and oxidation resistance up to 1800 degrees Farenheit (980 degrees C). This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of October 16, 1987. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1974-12-01
Standard
AMS5740A
This specification covers a corrosion and moderate heat resistant steel in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings.

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