page_title: Villiers XXIV
section_title: Specifications
hierarchical_section_title: Villiers XXIV / Specifications
caption_attribution_description: English: Villiers XXIV C.2 3-view drawing from L'Air June 1,1928
context_page_description: The Villiers XXIV or Villiers 24 CAN2 was a French army night fighter most notable as the first French military aircraft to be fitted with leading edge slats.
context_section_description: Data from NACA (November 1928) unless indicated otherwise
  General characteristics
  Crew: two
  Length: 8.75 m (28 ft 8 in)
  Upper wingspan: 13 m (42 ft 8 in)
  Lower wingspan: 9.00 m (29 ft 6 in)
  Height: 3.30 m (10 ft 10 in)
  Wing area: 42 m² (450 sq ft)
  Airfoil: upper wing R.A.F.31, lower wing Göttingen 436
  Empty weight: 1,469 kg (3,239 lb)
  Gross weight: 2,219 kg (4,892 lb)
  Fuel capacity: 300 kg (660 lb)
  Powerplant: 1 × Lorraine 12Eb Courlis water-cooled W-12 engine, 340 kW (450 hp)
  Propellers: 2-bladed
  Performance
  Maximum speed: 212 km/h (132 mph; 114 kn) at sea level; 200 km/h (120 mph; 110 kn) at 5,000 m (16,000 ft)
  Minimum control speed: 70 km/h (43 mph; 38 kn) with slots open, 101 km/h (63 mph; 55 kn) slots closed
  Endurance: 3 hrs with normal tankage; provision for an extra tank to add 1 hr
  Time to altitude: 50 min to 6,000 m (20,000 ft)
  Armament
  Guns: 
  2x fixed forward firing 7.7 mm (0.303 in) Vickers machine guns
  and
  2x 7.7 mm (0.303 in) Lewis machine guns on a flexible mount in the rear cockpit
caption: Villiers XXIV C.2 3-view drawing from L'Air June 1,1928
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