Specification for 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 550 N/mm2) (weldable)
€165.00
Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 800 MPa) (weldable)
Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (titanium stabilized: 800 N/mm2) (weldable)
€77.00
Specification for chromium-molybdenum steel tube (770 MPa) (weldable)
Specification for chromium-molybdenum steel tube (900 MPa) (weldable)
Specification for aircraft material. Preformed corrosion-resisting steel wire rope
Specification for tube of 99% aluminium (cold drawn: seamless: tested hydraulically) (not exceeding 12 mm wall thickness)
Specification for tube of aluminium-2¼% magnesium alloy (temper designation-O) (seamless: tested hydraulically) (not exceeding 12 mm wall thickness)
Specification for bearings - airframe rolling single row self aligning roller bearings in corrosion resisting steel diameter series 3 and 4. Dimensions and loads
Specification for bearings - airframe rolling double row, self aligning ball bearings in steel diameter series 2. Dimensions and loads
Specification for bearings - airframe rolling single row, self aligning roller bearings in steel diameter series 3 and 4. Dimensions and loads
Specification for bearings. Airframe rolling rigid single row ball bearings in corrosion resisting steel diameter series 8 and 9.Dimensions and loads
Specification for bearings - airframe rolling rigid, single row ball bearings in steel diameter series 0 and 2. Dimensions and loads
Specification for bearings - airframe rolling double row self aligning ball bearings in corrosion resisting steel diameter series 2. Dimensions and loads
Specification for bearings. Airframe rolling rigid single row ball bearings in corrosion resisting steel diameter series 0 and 2.Dimensions and loads
