page_title: Buscaylet-de Monge 5/2
section_title: Specification
hierarchical_section_title: Buscaylet-de Monge 5/2 / Specification
caption_attribution_description: English: Buscaylet-de Monge 5/2 3-view drawing from L'Aéronautique December,1922
context_page_description: The Buscaylet-de Monge 5/2 was a 1920s French single-seat, parasol-wing fighter prototype designed by Louis de Monge for the Buscaylet et Cie company.
context_section_description: Data from The Illustrated Encyclopedia of Aircraft, Jane's all the World's Aircraft 1924
  General characteristics
  Crew: 1
  Length: 7.15 m (23 ft 5 in)
  Wingspan: 10.90 m (35 ft 9 in)
  Height: 2.70 m (8 ft 10 in)
  Wing area: 24.00 m² (258.3 sq ft)
  Gross weight: 1,392 kg (3,069 lb)
  Powerplant: 1 × Hispano-Suiza 8Fb 8-cylinder inline piston, 220 kW (300 hp)
  Propellers: 2-bladed fixed-pitch propeller, 2.25 m (7 ft 5 in) diameter
  Performance
  Maximum speed: 270 km/h (168 mph; 146 kn) at sea level; 250 km/h (160 mph; 130 kn) at 4,000 m (13,000 ft)
  Service ceiling: 7,500 m (24,600 ft)
  Wing loading: 58 kg/m² (12 lb/sq ft)
  Power/mass: 0.161 kW/kg (0.098 hp/lb)
  Armament
  Guns: two forward-firing synchronised 0.303 in (7.70 mm) machine-guns (intended)
caption: Buscaylet-de Monge 5/2 3-view drawing from L'Aéronautique December,1922
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