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Viewing 9751 to 9780 of 9991
HISTORICAL
1944-08-01
Standard
AMS6292C
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Primarily for carburized parts which require intermediate minimum core hardness and allow wide hardness range in sections 0.25 in. (6 mm) and under in nominal thickness. The core may or may not be machinable after hardening. Alloy: 4617 UNS Number: G46170
HISTORICAL
1944-08-01
Standard
AMS6272B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1944-06-01
Standard
AMS2400C
This specification covers the requirements for electrodeposited cadmium on metal parts.
HISTORICAL
1944-05-01
Standard
AMS5040C
This specification covers a carbon steel in the form of sheet and strip.
HISTORICAL
1944-05-01
Standard
AMS5310
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.
HISTORICAL
1944-05-01
Standard
AMS6253D
HISTORICAL
1944-05-01
Standard
AMS6260A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1944-05-01
Standard
AMS6264A
This specification covers an aircraft quality, low alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1944-05-01
Standard
AMS6263A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
1944-04-01
Standard
AMS6353
No scope available.
HISTORICAL
1944-03-01
Standard
AMS5690B
This specification covers a corrosion and heat resistant steel in the form of wire. This wire has been used typically in woven wire screening, but usage is not limited to such application. The former requirements of this specification for use as welding wire are embodied in AMS 5692. When AMS 5690 is specified for welding wire, use AMS 5692.
HISTORICAL
1944-03-01
Standard
AMS5610B
This specification covers two types of free-machining, corrosion and moderate heat resistant steel in the form of bars, wire, forgings, and forging stock.
CURRENT
1943-12-01
Standard
AMS6252C
No scope available.
HISTORICAL
1943-10-01
Standard
AMS5032
This specification covers a low-carbon steel in the form of wire supplied as coils of wire or, when specified, as straight lengths.
HISTORICAL
1943-10-01
Standard
AMS5115A
This specification covers a carbon steel in the form of wire supplied as coils of wire or as finished springs. Primarily for springs, such as valve springs, subject to moderate stresses and requiring good fatigue properties.
HISTORICAL
1943-10-01
Standard
AMS5050A
This specification covers a low-carbon steel in the form of seamless tubing. This tubing has been used typically for oil lines and other parts requiring high-quality tubing suitable for severe forming and for welding or brazing, but usage is not limited to such applications.
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
1943-10-01
Standard
AMS6280A
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
1943-10-01
Standard
AMS6358
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
HISTORICAL
1943-10-01
Standard
AMS6357A
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
HISTORICAL
1943-10-01
Standard
AMS6535A
Primarily for use where welding and moderate tensile properties are required. May be used where minimum tensile strength up to 180,000 psi (1240 MPa) is required for wall thicknesses up to 0.125 in. (3 mm) and proportionately lower strength is required in heavier thicknesses. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of 19 April 1988. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1943-10-01
Standard
AMS6550A
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
1943-07-01
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
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
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
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.
Viewing 9751 to 9780 of 9991