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49.035 Components for aerospace construction
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BS EN 2515:1990
Specification for rod ends, adjustable single fork and threaded shank. Dimensions and loads
Specification for rod ends, adjustable single fork and threaded shank. Dimensions and loads
Released: 1990-12-31
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BS EN 3285:1994
Bearings; airframe rolling. Rigid single row ball bearings in steel, cadmium plated. Diameter series 0 and 2. Normal clearance category. Dimensions and loads
Bearings; airframe rolling. Rigid single row ball bearings in steel, cadmium plated. Diameter series 0 and 2. Normal clearance category. Dimensions and loads
Released: 1994-08-15
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BS EN 3288:1994
Bearings, airframe rolling. Double row self-aligning ball bearings in steel, cadmium plated. Diameter series 2. Dimensions and loads
Bearings, airframe rolling. Double row self-aligning ball bearings in steel, cadmium plated. Diameter series 2. Dimensions and loads
Released: 1994-08-15
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BS ISO 10955:1999
End-fittings and turnbarrels for aircraft control wire rope. Technical specification
End-fittings and turnbarrels for aircraft control wire rope. Technical specification
Released: 1999-11-15
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BS T 77:1980
Specification for chromium-molybdenum steel tube (900 MPa) (weldable)
Specification for chromium-molybdenum steel tube (900 MPa) (weldable)
Released: 1980-02-29
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BS SP 21:1950
Specification for lubricating nipples for aircraft purposes
Specification for lubricating nipples for aircraft purposes
Released: 1950-04-28
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BS EN 4710-04:2015
Aerospace series. Quick release fastening systems for non-structural applications Spring clamp. One way tolerance compensation
Aerospace series. Quick release fastening systems for non-structural applications Spring clamp. One way tolerance compensation
Released: 2015-10-31
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BS ISO 9747:2000
Double shank ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads
Double shank ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads
Released: 2001-03-15
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BS T 79:1997+A1:2013
Specification for 2 ½% nickel-chromium-molybdenum steel tubes (1160 MPa)
Specification for 2 ½% nickel-chromium-molybdenum steel tubes (1160 MPa)
Released: 2013-04-30
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BS EN 2045:2001
Aerospace series. Square bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Thickness 6 mm ≤ a ≤ 50 mm. Dimensions
Aerospace series. Square bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Thickness 6 mm ≤ a ≤ 50 mm. Dimensions
Released: 2001-12-24
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BS EN 2046:2001
Hexagonal bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Width across flats 7 mm ≤ a ≤ 50 mm. Dimensions
Hexagonal bars, drawn, in aluminium and aluminium alloys. Tolerance class h 11. Width across flats 7 mm ≤ a ≤ 50 mm. Dimensions
Released: 2001-12-24
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BS EN 6098:2019
Aerospace series. Rod-end with bearing per EN 6097 in corrosion resisting steel, extra wide inner ring, external threaded shank. Dimensions and loads. Inch series
Aerospace series. Rod-end with bearing per EN 6097 in corrosion resisting steel, extra wide inner ring, external threaded shank. Dimensions and loads. Inch series
Released: 2019-05-10
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