page_title: Caudron C.67
section_title: Specifications
hierarchical_section_title: Caudron C.67 / Specifications
caption_attribution_description: English: Caudron C.67 3-view drawing from Les Ailes May 25,1922
context_page_description: The Caudron C.67 was a simple single seat biplane with a low powered engine. It was built and flown in France in 1922.
context_section_description: Data from Hauet (2001)
  General characteristics
  Crew: One
  Length: 5.80 m (19 ft 0 in)
  Wingspan: 7.30 m (23 ft 11 in)
  Height: 2.40 m (7 ft 10 in)
  Wing area: 14.00 m² (150.7 sq ft)
  Empty weight: 210 kg (463 lb)
  Gross weight: 324 kg (714 lb)
  Fuel capacity: 34 kg (75 lb)
  Powerplant: 1 × Anzani 3-cylinder air-cooled inverted Y or radial, 19 kW (25 hp)
  Propellers: 2-bladed
  Performance
  Maximum speed: 95 km/h (59 mph; 51 kn)
  Service ceiling: 1,300 m (4,300 ft)
caption: Caudron C.67 3-view drawing from Les Ailes May 25,1922
exif: {}