Blériot-SPAD S.XXIV

The Blériot-SPAD S.XXIV was a prototype fighter built by SPAD at the end of the First World War. It was a single-seat biplane fighter of all-wood construction with a canvas coating and a monocoque fuselage. The specification, given for a variant, lists a crew of one, a length of 6.48 m, a wingspan of 9.8 m, a height of 2.56 m, a wing area of 26.2 square metres and an empty weight of 650 kg, with one 160 kW Hispano-Suiza 8Bc water-cooled V-8 piston engine. The article gives no gross weight or performance figures, and it shares the same dimensions and empty weight as the S.XXII.