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Homepage>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.035 Components for aerospace construction

49.035 Components for aerospace construction

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233 results
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BS 4T 45:1972+A2:2015
Specification for carbon manganese steel tube (700 MPa) (Tube 12.5 mm outside diameter and greater) (Weldable)
Released: 2015-09-30
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BS EN 3727:2006
Aerospace series. Bearings, airframe rolling rigid with flanged alignment housing. Technical specification
Released: 2006-06-30
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BS EN 3291:1994
Bearings, airframe rolling. Single row self-aligning roller bearings in steel, cadmium plated. Diameter series 3 and 4. Dimensions and loads
Released: 1994-08-15
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BS 3F 65:1991
Specification for flexible corrugated oxygen and air tubes for aircraft (natural or synthetic polyisoprene)
Released: 1991-05-31
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BS EN 2498:1990
Specification for rod ends, adjustable self-aligning plain bearing, with self-lubricating liner and threaded shank. Dimensions and loads
Released: 1990-12-31
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BS ISO 9749:2000
Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads
Released: 2001-03-15
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BS EN 2792:1991
Rod ends, adjustable, double fork and threaded shank with engagement: 1.5 thread diameter. Dimensions and loads
Released: 1991-08-30
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BS EN 3290:1994
Bearings, airframe rolling. Single row self-aligning roller bearings in steel. Diameter series 3 and 4. Dimensions and loads
Released: 1994-09-15
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BS EN 4041:2006
Aerospace series. Bearings, airframe rolling. Rigid single row ball bearings in corrosion resisting steel, with extended inner ring and flanged alignment bush. Dimensions and loads
Released: 2006-06-30
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BS EN 3060:2007
Aerospace series. Bearings, airframe rolling. Rigid single row ball bearings in steel, cadmium plated, with flanged alignment housing, cadmium plated. Dimensions and loads
Released: 2007-07-31
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BS L 117:1975
Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: not tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
Released: 1975-05-30
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BS L 118:1975
Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
Released: 1975-05-30
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233 results
First page123...111315...181920Last page