Browse Topic: Corrosion resistant alloys
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.
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide the aerospace industry with recommendations concerning the minimization of stress corrosion cracking in wrought heat-treatable carbon and low-alloy steels and in austenitic, precipitation hardenable, and martensitic corrosion-resistant steels and alloys. The detailed recommendations are based on laboratory and field experience and reflect those design practices and fabrication procedures which should avoid in-service stress corrosion cracking.
This specification covers steel cleanliness requirements for aircraft-quality ferromagnetic steels, other than hardenable corrosion-resistant steels (refer to AMS2303), by magnetic particle inspection methods. This specification contains sampling, specimen preparation, inspection procedures, and cleanliness rating criteria (see 8.2).
This specification covers steel cleanliness requirements for special aircraft-quality ferromagnetic steels, including hardenable corrosion-resistant steels, by magnetic particle inspection methods. This specification contains sampling, sample preparation, inspection procedures, and cleanliness rating criteria (see 8.2).
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable material specifications of corrosion- and heat-resistant steel and alloy forgings.
This specification covers a corrosion-resistant steel product in the solution and precipitation heat-treated (H1025) condition, 4 inches (102 mm) and under in nominal thickness.
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
This specification covers a heat-treatable, corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, and stock for forging or heading.
This specification covers a corrosion-resistant steel in the form of investment castings homogenized and solution and precipitation heat treated to 130 ksi (895 MPa) tensile strength.
This specification covers a corrosion-resistant steel in the form of investment castings homogenized and solution and precipitation heat treated to 180 ksi (1241 MPa) tensile strength.
This specification covers a titanium alloy in the form of sheet, strip, and plate up to 4.000 inches (101.60 mm), inclusive (see 8.6).
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate 0.015 to 1.5 inches (0.38 to 38 mm) in nominal thickness.
This specification covers a corrosion- and heat-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness.
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate.
This specification covers a corrosion-resistant steel in the form of investment castings, solution and precipitation heat treated to 180 ksi (1241 MPa) tensile strength.
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.
This specification covers a corrosion- and heat-resistant nickel-iron alloy in the form of bars and forgings 5 inches (127 mm) and under in nominal diameter or least distance between parallel sides and forging stock of any size.
This specification covers quality assurance sampling and testing procedures used to determine conformance to applicable material specification requirements of wrought corrosion- and heat-resistant steel and alloy products and of forging stock.
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, flash-welded rings, and extrusions up to 12 inches (305 mm) in nominal diameter or least distance between parallel sides (thickness) in the solution heat-treated condition (see 8.4) and stock of any size for forging, flash-welded rings, or extrusions.
This specification covers a corrosion-resistant steel in the form of investment castings homogenized, solution, and precipitation heat treated to 150 ksi (1034 MPa) minimum tensile strength.
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.
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, wire, forgings, flash-welded rings, and extrusions 4 inches (102 mm) and under in nominal diameter or least distance between parallel sides and stock for forging or flash-welded rings.
This specification covers established manufacturing tolerances applicable to sheet, strip, and plate of corrosion- and heat-resistant steels, iron alloys, titanium, and titanium alloys. These tolerances apply to all conditions, unless otherwise noted. The term “excl” is used to apply only to the higher figure of the specified range.
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet and strip 0.080 inch (2.03 mm) and under in nominal thickness.
This specification covers a corrosion- and heat-resistant steel in the form of sheet, strip, and plate.
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
This specification covers a corrosion-resistant steel in the form of laminated sheet.
This specification covers a free-machining, corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings.
This specification covers flash welded rings made of corrosion and heat-resistant austenitic steels and austenitic-type iron, nickel, or cobalt alloys, or precipitation-hardenable alloys.
This specification covers flash welded rings made of ferritic and martensitic corrosion-resistant steels.
This specification covers a corrosion-resistant steel product 12 inches (305 mm) and under in nominal diameter, thickness, or for hexagons, least distance between parallel sides in the solution and precipitation heat treated (H950) condition.
This specification covers a corrosion-resistant steel product 8 inches (203 mm) and under in nominal diameter, thickness, or for hexagons least distance between parallel sides in the solution and precipitation heat-treated (H925) condition.
This specification covers a corrosion-resistant steel product 8 inches (203 mm) and under in nominal diameter, thickness, or for hexagons least distance between parallel sides in the solution and precipitation heat-treated (H900) condition.
This specification covers a corrosion- and heat-resistant steel in the form of welding wire.
This specification covers a free-machining, corrosion-resistant steel in the form of bars, forgings, and forging stock.
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
This specification covers a carbon steel in the form of bars up through 3.000 inches (76.20 mm) and forgings and forging stock of any size.
This specification covers an iron-nickel alloy in the form of strip 0.020 to 0.250 inch (0.51 to 6.35 mm), inclusive, in thickness.
This specification covers a corrosion- and heat-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness.
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of investment castings.
This specification covers a corrosion- and heat-resistant nickel alloy in the form of investment castings.
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of investment castings.
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of investment castings.
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate 0.002 inch (0.05 mm) and above in nominal thickness.
This specification covers a corrosion- and heat-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness.
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of welding rods or wrought wire.
This specification covers a corrosion- and heat-resistant iron alloy in the form of investment castings.
This SAE Aerospace Standard (AS) establishes the requirements for 24° cone flareless fluid connection fittings and nuts and bite type flareless sleeves (see Section 6) for use in aircraft fluid systems at an operating pressure of 5000 psi for the fittings and nuts and 3000 psi for the bite type sleeves.
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