Blériot-SPAD S.70

The Blériot-SPAD S.70 was a French fighter aircraft developed in the late 1920s. It was the second prototype of the S.60, a two-seat biplane fighter of all-wood construction with a canvas coating and a monocoque fuselage. The specification lists a length of 7.5 m, a wingspan of 11.3 m, a wing area of 36.6 square metres, an empty weight of 1,331 kg, a gross weight of 1,893 kg and a maximum speed of 210 km/h from one 340 kW Lorraine 12Ed Courlis water-cooled W-12 piston engine driving a two-bladed fixed-pitch propeller. The article lists the crew as one although its text calls the type a two-seater.