Specification for low pressure oxygen hose for aeronautical purposes
€165.00
Power take-off, squared shaft drive. Four stud flange without oil seal gasket.
€28.00
Power take-off, squared shaft drive. Two stud flange without oil seal gasket.
Ball joints for small controls. Threaded end and undercut
Specification for hose for aviation fuel and engine lubricating oil for aeronautical purposes
Specification for chromium-molybdenum steel tube (700 MPa) (outside diameter not less than 12.5 mm) (weldable)
Specification for chromium-molybdenum steel tube (1150 MPa) (maximum thickness 8 mm)
Specification for 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 550 MPa) (weldable)
€95.00
Specification for cold drawn 18/10 chromium-nickel corrosion-resisting steel tube (niobium stabilized: 800 MPa) (weldable)
Specification for chromium-molybdenum steel tube (900 MPa) (weldable)
Aluminium alloy rod body for flight control and aircraft structure.technical specification.
€0.00
Assembly and spot stamping of ball bearings and spherical plain bearings. Spot stamping with six notches.
Assembly and spot stamping of ball bearings and spherical plain bearings. Spot stamping by spherical indentations with 2 mm diameter ball.
Assembly and spot stamping of ball bearings and spherical plain bearings. Spot stamping by spherical indentations with 4 mm diameter ball.
Specification for chromium-molybdenum steel tube (770 MPa) (weldable)
