Aerospace series. Titanium alloy TI-P64003. Cold worked and stress relieved. Seamless tube for pressure systems. 4 mm = D = 51 mm. 690 MPa = Rm = 1 030 MPa
€165.00
Aircraft. Minimum airworthiness requirements and test conditions for certified air cargo unit load devices
Stud-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads
Turnbarrels, for aircraft control wire rope. Dimensions and loads
Eye-ends, in corrosion-resistant steel, threaded, for aircraft control wire rope. Dimensions and loads
Double shank ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads
Eye-ends, in corrosion resisting steel, swaged on aircraft control wire rope. Dimensions and loads
End-fittings and turnbarrels for aircraft control wire rope. Technical specification
€193.00
Ball-ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads
Fork-ends, in corrosion-resistant steel, threaded, for aircraft control wire rope turnbarrels. Dimensions and loads
Fork-ends, in corrosion-resistant steel, threaded, for rolling bearings, for aircraft control wire rope. Dimensions and loads
Fork ends, in corrosion-resistant steel, swaged on aircraft control wire rope. Dimensions and loads
Locking clips, in corrosion-resistant steel, for aircraft control wire rope turnbuckles. Dimensions
Aircraft control wire rope assemblies. Dimensions and end-fitting combinations
Nuts, barrel, self-locking, floating, with MJ threads, classifications. 900 MPa (at ambient temperature)/235°C, 1100 MPa (at ambient temperature)/235°C, 1250 MPa (at ambient temperature)/235°C, 1550 MPa (at ambient temperature)/235°C. Dimensions
