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Viewing 9931 to 9960 of 10147
HISTORICAL
1943-10-01
Standard
AMS5112B
This specification covers a carbon steel in the form of wire supplied as coils, spools, or cut lengths. This wire has been used typically for springs subject to high stress or requiring good fatigue properties up to 200 °F (93 °C), but usage is not limited to such applications.
HISTORICAL
1943-10-01
Standard
AMS6440A
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1943-07-01
Standard
AMS5843A
This specification covers a high strength, corrosion and heat resistant cobalt-chromium-nickel alloy in the form of bars.
HISTORICAL
1943-04-01
Standard
AMS3072A
This specification covers a blend of corrosion-preventive compound concentrate and petroleum-base aircraft-engine lubricating oil in the form of a ready-to-use liquid.
HISTORICAL
1943-04-01
Standard
AMS6550
Primarily for general use is light wall-thickness sections where minimum tensile strength up to 160,000 psi (1105 MPa) is required and parts may be welded during fabrication. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of April 19, 1988. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1943-04-01
Standard
AMS5036
This specification covers a low-carbon steel in the form of sheet and strip coated on both faces with aluminum-silicon alloy by the hot-dip process. Primarily for low-stressed parts, such as brackets, clips, and sheathing, requiring corrosion resistance and oxidation resistance up to 1200F degrees (650C degrees).
HISTORICAL
1943-04-01
Standard
AMS6272A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1943-04-01
Standard
AMS6270A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1943-04-01
Standard
AMS6300
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
HISTORICAL
1943-04-01
Standard
AMS6325A
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
HISTORICAL
1943-04-01
Standard
AMS3075
This specification covers a stable, nonvolatile, petroleum-base compound in a form suitable for application by dipping at 170 to 210 °F (77 to 99 °C).
HISTORICAL
1943-04-01
Standard
AMS6322A
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
1943-04-01
Standard
AMS6327A
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
HISTORICAL
1943-04-01
Standard
AMS6320A
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
1943-04-01
Standard
AMS6274A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
1943-03-01
Standard
AMS6310A
No scope available.
CURRENT
1942-12-01
Standard
AMS5033
HISTORICAL
1942-12-01
Standard
AMS6253C
HISTORICAL
1942-12-01
Standard
AMS6254C
CURRENT
1942-12-01
Standard
AMS7212
HISTORICAL
1942-12-01
Standard
AMS6250C
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1942-12-01
Standard
AMS6413
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
HISTORICAL
1942-12-01
Standard
AMS5044
This specification covers a carbon steel in the form of sheet and strip.
HISTORICAL
1942-12-01
Standard
AMS5042B
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 specifications which have previously been widely used 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.
HISTORICAL
1942-12-01
Standard
AMS5575B
This specification covers a corrosion and heat-resistant steel in the form of welded tubing.
HISTORICAL
1942-12-01
Standard
AMS2400B
This specification covers the requirements for electrodeposited cadmium on metal parts.
HISTORICAL
1942-12-01
Standard
AMS6381
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
HISTORICAL
1942-12-01
Standard
AMS6352A
This specification covers an aircraft quality, low alloy steel in the form of sheet, strip, and plate. These products have been used typically for heat treated parts and structures that may require welding during fabrication, but usage is not limited to such applications. It may be through-hardened to a minimum tensile strength of 180 ksi (1241 MPa) in sections 0.125 inch (3.18 mm) and under in nominal thickness and proportionately lower strength in heavier section thicknesses.
HISTORICAL
1942-12-01
Standard
AMS6470A
This specification covers an aircraft quality nitriding grade low alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1942-12-01
Standard
AMS6359
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
Viewing 9931 to 9960 of 10147