Material Specifications - SAE Mobilus
This specification covers a corrosion- and heat-resistant nickel alloy in the form of bars, forgings, and flash-welded rings 4.00 inches (101.6 mm) and under in diameter or least nominal cross-sectional dimension and stock of any size for forging or flash-welded rings.
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire and of flash-welded rings conforming to the dimensions listed in Table 2 (see 8.6).
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross-sectional area of 32 square inches (206 cm2) maximum (see 8.6).
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing produced with cross-sectional area of 32 square inches (206 cm2), maximum (see 8.6).
This specification covers a corrosion- and heat-resistant cobalt alloy in the form of strip up to 0.100-inch (2.54-mm) thick.
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) produced with a cross-sectional area of 24 square inches (155 cm2), maximum, and a circumscribing circle (see 2.4.1) diameter (circle size) of 10.5 inches (267 mm), maximum, with a nominal thickness up to 3.000 inch (76.20 mm), inclusive (see 8.6).
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness.
This specification covers a titanium alloy in the form of sheet and strip up to and including 0.125 inch (3.18 mm) in nominal thickness.
This specification covers an aluminum alloy in the form of rolled or cold-finished bars, rods, and wire up to 6.000 inches (152.40 mm) in nominal diameter or least nominal dimension (see 8.6).
This specification covers a magnetic nickel-iron alloy in the form of sheet and strip.
This specification covers a magnetically soft nickel-iron alloy in the form of bars, rods, forgings, mechanical tubing, and forging stock.
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles.
This specification covers an aluminum alloy in the form of sheet and plate alclad two sides, over 0.187 to 1.000 inch (over 4.750 to 25.40 mm) in nominal thickness, supplied in the -T3/-T351 temper (see 8.5).
This specification covers an aluminum alloy in the form of seamless round tubing with wall thickness from 0.025 to 0.500 inch (0.64 to 12.70 mm), inclusive (see 8.6).
This specification covers the requirements for a low-electrical-resistance chemical conversion coating on aluminum and aluminum alloy parts.
This specification covers a nickel alloy in the form of wire, rod, strip, foil, tape, and powder and a viscous mixture (paste) of the powder in a suitable binder.
This specification covers an aluminum alloy in the form of plate 1.500 to 6.000 inches (38.10 to 152.40 mm) in nominal thickness (see 8.6).
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form (see 8.5).
This specification covers a magnetically soft nickel-iron alloy in the form of sheet and strip.
This specification covers requirements for a coating consisting of finely powdered molybdenum disulfide in a heat-resistant inorganic binder applied to parts.
This specification covers the engineering requirements for applying coatings to parts by the plasma spray process and the properties of such coatings.
This specification covers a corrosion- and heat-resistant nickel alloy in the form of sheet, strip, and plate.
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 aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
This specification covers an aluminum alloy in the form of alclad sheet 0.040 to 0.187 inch (1.02 to 4.75 mm), inclusive, in nominal thickness (see 8.6).
This specification covers a free-machining, low-alloy steel in the form of round bars 3.50 inches (88.9 mm) and under in nominal diameter produced by a die-drawing process.
This specification covers a corrosion- and heat-resistant iron-nickel alloy in the form of sheet, strip, and plate.
This specification covers an aircraft-quality, low-alloy steel in the form of heat-treated bars and forgings.
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate over 0.005 inch (0.13 mm) in nominal thickness.
This specification defines limits of variation for determining acceptability of the composition of cast or wrought titanium and titanium alloy parts and material acquired from a producer.
This specification covers an aluminum alloy in the form of plate from 1.000 to 6.000 inches (25.40 to 152.40 mm) in thickness (see 8.6).
This specification covers established manufacturing tolerances applicable to low-alloy steel bars ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term “exclusive” is used to apply only to the higher figure of the specified range.
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot-pressed powder.
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, and drawn shapes 4.000 inches (101.60 mm) and under and stock for forging, heading, or flash-welded rings of any size (see 8.6).
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) produced with thicknesses 0.040 to 2.500 inches (1.02 to 38.10 mm), inclusive, having a maximum cross-sectional area of 23 square inches (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 16 inches (406 mm) (see 2.4.1 and 8.7).
This specification covers beryllium in the form of bars, rods, tubing, and machined shapes fabricated from vacuum hot-pressed powder.
This specification covers a titanium alloy in the form of bars, wire, forgings, flash-welded rings, drawn shapes 5.000 inches (127.00 mm) and under, and stock for forging or flash-welded rings of any size (see 8.6).
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate up to and including 1.500 inches (38.10 mm) in thickness.
This specification covers a titanium alloy in the form of sheet, strip, and plate up through 2.000 inches (50.80 mm), inclusive (see 8.6)
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing 0.040 to 4.499 inches (1.01 to 114.27 mm), inclusive, in nominal diameter or least thickness and with areas up to 32 square inches (206 cm2), inclusive (see 8.6).
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