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This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire.
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 4.500 inches (1.02 to 114.30 mm), inclusive, in thickness produced with maximum cross sectional area of 56.1 square inches (36199 mm2) and a maximum circumscribing circle diameter (circle size) of 24.4 inches (620 mm) (see 2.4.1 and 8.6).
This specification covers a copper alloy (brass) in the form of seamless tubing with nominal OD of 0.405 inch (10.29 mm) to 10.75 inches (273.05 mm) and nominal weight of 0.253 lb/ft (0.38 kg/m) to 66.142 lb/ft (98.43 kg/m) (see 8.6).
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 titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm), inclusive.
This specification covers a titanium alloy in the form of welding wire.
This specification covers a Methyl Vinyl Silicone (MVQ) rubber in the form of molded rings for aeronautical and aerospace applications. For sheet, strip, tubing, extrusions, and molded shapes it is the responsibility of the user to determine suitability.
This specification covers an acrylonitrile-butadiene rubber in the form of molded rings, compression seals, O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applications.
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
This specification covers a petroleum-based reference oil.
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness (see 8.6).
This specification covers a corrosion-resistant steel in the form of sheet and strip over 0.005 inch (0.13 mm) in nominal thickness (see 8.6).
This specification covers a titanium alloy in the form of forgings up through 4.0 inches (102 mm) and under in nominal diameter or least distance between parallel sides and 16 square inches (103 cm2) and under in cross-sectional area and stock of any size for forging (see 8.6).
This specification covers an aluminum alloy in the form of plate with nominal thickness from 1.000 to 5.000 inches (25.40 to 127.00 mm), inclusive (see 8.5).
This specification covers one type of copper in the form of bars, rods, and shapes. Requirements are provided for bar and rods up to 3.000 inches (mm) in nominal diameter, squares and rectangles with up to 4.000 inches (mm) least distance between parallel sides and shapes of any size (see 8.6).
This specification covers a copper-zinc alloy (brass) in the form of wire.
This specification covers an aluminum alloy in the form of plate 0.500 to 2.250 inches (12.70 to 57.15 mm), inclusive, in nominal thickness (see 8.6).
This specification covers an aluminum alloy in the form of plate 0.750 to 1.500 inch (19.05 to 38.10 mm), inclusive, in nominal thickness (see 8.5).
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 4.500 inches (1.02 to 114.30 mm), inclusive, in thickness produced with maximum cross sectional area of 56.1 square inches (36193 mm2) and a maximum circumscribing circle diameter (circle size) of 20.2 inches (513 mm) (see 2.4.1).
This specification covers an aluminum alloy in the form of sheet and plate from 0.020 to 5.000 inches (0.51 to 127.00 mm), inclusive, in nominal thickness (see 8.5).
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
This specification covers a corrosion-resistant nickel-copper alloy in the form of bars 0.093 to 4.000 inches (2.35 to 100.00 mm) in diameter or distance between parallel sides, and forgings and forging stock of any size.
This specification covers the engineering requirements for producing brazed joints in parts fabricated from steels, iron alloys, nickel alloys, cobalt alloys, and copper alloys by use of silver alloys, and the properties of such joints.
This specification covers a maraging steel in the form of rolled or forged plate 0.375 inches through 8.000 inches (9.52 mm through 203.20 mm).
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate up to 2.000 inches (50.80 mm), inclusive, in nominal thickness.
This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock for forging or flash welded rings of any size (see 8.6).
This specification covers discontinuously reinforced aluminum alloy (DRA) metal matrix composites (MMC) in the form of sheet.
This specification covers a titanium alloy in the form of bars up through 7.000 inches (177.80 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 7.000 inches (177.80 mm), inclusive, and stock for forging of any size.
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.6).
This specification covers aluminum alloy rolled or forged rings up to 6 inches (152 mm) which are produced and shipped in the –T351 or –T352 temper and are artificially aged to the –T82 temper prior to being put into service.
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
This specification covers an aluminum alloy in the form of extruded profiles such as angles, channels, tees, zees, I-beams, and H-beams.
This specification covers an aluminum alloy in the form of die forgings up to 6.000 inches (152.40 mm), inclusive, in nominal thickness and forging stock of any size (see 8.6).
This specification establishes the engineering requirements for producing anodic coatings on magnesium and magnesium alloys, from an alkaline electrolyte, and the properties of those coatings.
This specification covers an aluminum alloy in the form of drawn, round, seamless hydraulic tubing with nominal wall thickness of 0.018 to 0.500 inch (0.46 to 12.70 mm) (see 8.6).
This specification covers a titanium alloy in the form of sheet in nominal thicknesses 0.016 through 0.1874 inch (0.41 through 4.760 mm).
This specification covers an aluminum alloy in the form of plate 0.500 to 2.000 inches (12.70 to 50.80 mm), inclusive, in thickness (see 8.6).
This specification covers an aluminum alloy in the form of plate 0.250 to 0.300 inch (6.35 to 7.62 mm), inclusive, in thickness (see 8.8).
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm), inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (see 8.6).
This specification covers the requirements for producing brazed joints of aluminum and aluminum alloys by immersion in a molten flux bath.
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