Rolled threads for bolts. Lead and runout requirements
Document status: Active
Specification for corrosion-resisting steel hexagonal nuts (B.A and B.S.F. threads) (ordinary, thin, slotted and castle) for aircraft
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General requirements for steel protruding-head bolts of tensile strength 1250 MPa (180000 lbf/in2) or greater. Specification
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Bolts, hexagonal head, close tolerance shank, UNJF threads, split pin & locking wire hole options, titanium alloy, various finishes. Classification: Rm 1 100-1 250 MPa (160 000-180 000 lbf/in2) at Ambient Temperature | +315°C
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Specification for corrosion-resisting steel hexagonal-headed bolts (B.A and B.S.F. threads) for aircraft
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Aerospace Series. Bolt, 100° Countersunk head, Hi-Torque speed drive recess, close tolerance shank, UNJF thread, split pin hole option, titanium alloy, various finishes. Classification: Rm 1100–1250 MPa (160 000–180 000 lbf/in2) at Ambient Temperature | +315 °C
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Spline drives. Wrenching configuration. Metric series
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Nuts, self-locking, with maximum operating temperature less than or equal to 425°C. Test methods
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Specification for steel hexagonal-headed shear bolts (B.S.F. threads) for aircraft
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Specification for aluminium alloy hexagonal headed bolts (B.A. and B.S.F. threads) for aircraft
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