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HISTORICAL
1960-11-01
Standard
AMS5352A
This specification covers a corrosion-resistant steel in the form of investment castings. These castings have been used typically for parts requiring hardness up to 58 HRC and having resistance to corrosion and to wear, but usage is not limited to such applications. Optimum corrosion resistance is obtained by hardening from 1850 to 1950 °F (1010 to 1066 °C) and tempering at not higher than 800 °F (427 °C).
HISTORICAL
1960-11-01
Standard
AMS5526C
This specification covers a corrosion and heat resistant steel in the form of sheet, strip, and plate.
HISTORICAL
1960-11-01
Standard
AMS5754C
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
HISTORICAL
1960-11-01
Standard
AMS5665F
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.
1960-10-01
Magazine
HISTORICAL
1960-10-01
Standard
AMS5585
This specification covers a corrosion and heat resistant alloy in the form of welded and drawn tubing.
1960-09-01
Magazine
HISTORICAL
1960-06-30
Standard
AMS6444
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1960-06-30
Standard
AMS6458
This specification covers a low-alloy steel in the form of welding wire. This wire has been used typically for use as filler metal for gas-tungsten-arc and gas-metal-arc welding of low-alloy steels of similar composition where the weld area is required to have strength comparable to that of the parent metal, but usage is not limited to such applications.
HISTORICAL
1960-06-30
Standard
AMS6461A
This specification covers a low-alloy steel in the form of welding wire.
HISTORICAL
1960-06-30
Standard
AMS6462
This specification covers a low-alloy steel in the form of welding wire.
HISTORICAL
1960-06-30
Standard
AMS6276
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1960-06-30
Standard
AMS4778A
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder and procured in inch/pound units.
HISTORICAL
1960-06-30
Standard
AMS6429
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1960-06-30
Standard
AMS6406
Primarily for heat treated parts and structures that may require welding during fabrication and may be through-hardened to a minimum tensile strength of 270,000 psi (1862 MPa) in sections of 2 in. (50 mm) or less in nominal thickness. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of April 1, 1987. It is recommended that this specification not be specified for new designs.
HISTORICAL
1960-06-30
Standard
AMS6407A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1960-06-30
Standard
AMS2261D
This specification covers established manufacturing tolerances applicable to bars, rods, and wire of nickel, nickel alloy, and cobalt alloys ordered to inch-pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" is used to apply only to the higher figure of a specified range. Where the terms “nickel”, “nickel-copper”, “nickel-chromium”, “nickel-molybdenum”, “nickel-molybdenum-chromium”, and “cobalt” are used without qualification, they refer to both non-heat-treatable and heat-treatable alloys as applicable, unless otherwise noted.
HISTORICAL
1960-06-30
Standard
AMS5355A
This specification covers a corrosion resistant steel in the form of investment castings. These castings have been used typically for parts requiring good corrosion resistance and strength up to 600 °F (316 °C), but usage is not limited to such applications (See 8.3). Certain processing procedures and service conditions may cause these castings to become subject to stress-corrosion cracking; ARP1110 recommends practices to minimize such conditions. Where stress-corrosion is considered to be a factor, precipitation heat treatment should be performed at a temperature not lower than 1000 °F (538 °C).
HISTORICAL
1960-06-30
Standard
AMS6435
This specification covers a premium aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
HISTORICAL
1960-06-30
Standard
AMS4779
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder. This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. This filler metal may also be used as a corrosion and oxidation resistant hard coating.
HISTORICAL
1960-06-01
Standard
AMS2550
This specification covers the enginering requirements for a treatment to provide enhanced corrosion resistance to sheet metal parts, such as brackets, spacers, and washers, fabricated from martensitic corrosion-resistant steels, usually AMS 5504 or AMS 5508 and having hardness not higher than 40 HRC, or ferritic corrosion-resistant steels, usually AMS 5506. The treatment is not recommended for use on parts subject to impact in service.
HISTORICAL
1960-06-01
Standard
AMS5391
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.
HISTORICAL
1960-06-01
Standard
AMS5396
This specification covers a corrosion and heat-resistant nickel alloy in the form of investment castings.
HISTORICAL
1960-06-01
Standard
AMS5769
This specification covers a corrosion and heat resistant alloy in the form of bars, forgings, flash welded rings, and stock for forging, flash welded rings, or heading. These products have been used typically for parts, such as turbine rotors, shafts, blades, and bolts, requiring high strength up to 1350 degrees F (732 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C), but usage is not limited to such applications.
HISTORICAL
1960-06-01
Standard
AMS5768D
This specification covers a corrosion and heat-resistant iron-chromium-nickel-cobalt alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging, flash welded rings, or heading.
HISTORICAL
1960-06-01
Standard
AMS5552
This specification covers a corrosion and heat-resistant alloy in the form of sheet, strip, and plate.
HISTORICAL
1960-06-01
Standard
AMS5746
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, and stock for forging or heading. These products have been used for parts such as turbine rotors, shafts, blades, bolts, dowels, and fittings, requiring high strength up to 1600°F (871°C) and oxidation resistance up to 1800°F (982°C).
HISTORICAL
1960-06-01
Standard
AMS7849
This specification covers tantalum in the form of sheet, strip, plate, and foil.
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