page_title: Dova DV-1 Skylark
section_title: Specifications (DV-1 Skylark)
hierarchical_section_title: Dova DV-1 Skylark / Specifications (DV-1 Skylark)
caption_attribution_description: Deutsch: Dova DV-1 Skylark auf dem Flugplatz Uetersen
context_page_description: The Dova DV-1 Skylark is a Czech ultralight and light-sport aircraft produced by Dova Aircraft of Paskov. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.
context_section_description: Data from Bayerl and manufacturer
  General characteristics
  Crew: one
  Capacity: one passenger
  Length: 6.62 m (21 ft 9 in)
  Wingspan: 8.14 m (26 ft 8 in)
  Height: 2.23 m (7 ft 4 in)
  Wing area: 9.44 m² (101.6 sq ft)
  Empty weight: 297 kg (655 lb)
  Gross weight: 472.5 kg (1,042 lb)
  Fuel capacity: 90 litres (20 imp gal; 24 US gal)
  Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
  Performance
  Maximum speed: 240 km/h (150 mph, 130 kn)
  Cruise speed: 210 km/h (130 mph, 110 kn)
  Stall speed: 64 km/h (40 mph, 35 kn) flaps down
  Never exceed speed: 280 km/h (170 mph, 150 kn)
  Range: 1,000 km (620 mi, 540 nmi)
  Service ceiling: 3,650 m (11,980 ft)
  g limits: +4/-2
  Rate of climb: 8 m/s (1,600 ft/min)
  Wing loading: 50.1 kg/m² (10.3 lb/sq ft)
caption: Dova DV-1 Skylark
exif: {}