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In 1990, the development efforts at ALCOA's Massena Operations began with the objective to create a free machining alloy that would be comparable to a lead bearing alloy, 6262, in strength, machinability, corrosion resistance, anodizing, brazing, and welding responses while eliminating the health and environmental concerns associated with lead. The results from years of controlled experimentation was a 1996 patented and registered 6020 alloy (nominal 1.1% Sn addition) which proved all of the objectives were met and the machinability performance was enhanced over the “B” rated 6262 product. Proclaimed as the fastest growing new product in automotive and miscellaneous applications the full cold finished product line in T8, T9 and T651 tempers excel in markets where 6262, 6061, 2011 aluminum alloys and 12L14 steels are used today. The automotive applications include ABS manifolds, brake parts, A/C components, transmission valves and transmission sleeves.

This specification covers a corrosion-resistant nickel-copper alloy in the form of bars, forgings, and forging stock.

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading.

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of Januray 1990.

This specification has been "CANCELLED" by the Aerospace Materials, Division, SAE, as of July 1, 1993.

This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of July 1, 1993.

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. Primarily for parts, such as turbine blades, bolts, and fittings, requiring high strength up to 1600 degrees F (870 degrees Centigrade) and oxidation resistance up to 1800 degrees F (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.

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.

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.

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.

This specification covers a corrosion and heat resistant nickel-base alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.

This specification covers a corrosion and heat resistant nickel-base alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.

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.

This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and flash welded rings up to 4.000 inch (101.6 mm), inclusive, in nominal thickness or distance between parallel sides, and stock of any size for forging or flash welded rings (see 8.6).

This specification covers a corrosion and heat resistant nickel alloy powder-metallurgy product in the form of billets and preforms for forgings. Primarily for parts requiring high strength up to 1500 degrees F (815 degrees C) and corrosion and oxidation resistance up to 1700 degrees F (925 degrees C). This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of October 16, 1986. It is recommended that this specification not be specified for new designs.

This specification covers a corrosion and heat resistant nickel alloy in the form of centrifugal castings.