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HISTORICAL
1939-12-04
Standard
AMS6250
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1939-12-04
Standard
AMS6292
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
1939-12-04
Standard
AMS5050
This specification covers a low-carbon steel in the form of seamless tubing.
HISTORICAL
1939-12-04
Standard
AMS6330
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1939-12-04
Standard
AMS5685
This specification covers a corrosion-resistant steel in the form of wire.
HISTORICAL
1939-12-04
Standard
AMS6317
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
HISTORICAL
1939-12-04
Standard
AMS6352
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
1939-12-04
Standard
AMS6290
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. These products have been used typically for carburized parts which require low minimum core hardness and allow a wide hardness range in sections 0.375 in. (9.50 mm) and under in nominal thickness, but usage is not limited to such applications. The core may or may not be machinable after hardening.
HISTORICAL
1939-12-04
Standard
AMS6470
This specification covers an aircraft quality nitriding grade low alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1939-12-04
Standard
AMS6294
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
HISTORICAL
1939-12-04
Standard
AMS5688
This specification covers a corrosion-resistant steel in the form of wire. This wire has been used typically for springs requiring corrosion and heat resistance up to 500 degrees F (260 degrees C), but usage is not limited to such applications. Alloy: 30302 UNS Number: S30200
HISTORICAL
1939-12-04
Standard
AMS6370
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
1939-12-04
Standard
AMS6440
This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1939-12-04
Standard
AMS6382
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
1939-12-04
Standard
AMS5510
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
HISTORICAL
1939-12-04
Standard
AMS5610
This specification covers two types of free-machining, corrosion and moderate heat resistant steel in the form of bars, wire, forgings, and forging stock.
HISTORICAL
1939-12-01
Standard
AMS7220
HISTORICAL
1939-12-01
Standard
AMS5680
This specification covers a corrosion and heat resistant steel in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-arc or gas-metal-arc welding of corrosion and heat resistant steels and alloys, but usage is not limited to such applications.
HISTORICAL
1939-12-01
Standard
AMS5690
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
1939-12-01
Standard
AMS5110
This specification covers a carbon steel in the form of wire supplied as coils of wire or as finished springs.
HISTORICAL
1939-12-01
Standard
AMS4135
This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled rings, and stock for forgings on rolled rings. Primarily for applications, such as aircraft structural members, requiring material with moderately high strength. Certain design and processing procedures may cause these forgings to become susceptible to stress corrosion cracking; ARP 823 recommends practices to minimize such conditions.
HISTORICAL
1939-12-01
Standard
AMS4118
This specification covers an aluminum alloy in the form of bars, rods, and wire.
HISTORICAL
1939-12-01
Standard
AMS4125
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.
HISTORICAL
1939-12-01
Standard
AMS4290
This specification covers an aluminum alloy in the form of die castings.
HISTORICAL
1939-12-01
Standard
AMS4000
This specification covers aluminum in the form of sheet and plate.
HISTORICAL
1939-12-01
Standard
AMS5112
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
1939-12-01
Standard
AMS4016
This specification covers an aluminum alloy in the form of sheet and plate.
HISTORICAL
1939-12-01
Standard
AMS5580
This specification covers a corrosion and heat-resistant nickel alloy in the form of seamless tubing.
HISTORICAL
1939-12-01
Standard
AMS4003
This specification covers an aluminum alloy in the form of sheet and plate 1 .000 inch (25.40 mm) and under in nominal thickness.
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