The aircraft is combination of primary classic anti-corrosion all-metal construction which is riveted and bonded and composite parts to achieve elegant external contours. The DV-1 aircraft is designed to be used for flight training, glider towing and recreational flights. Pilots will appreciate not only the roomy cockpit space and comfortable ergonomic seats but also the precise aerodynamics of the aircraft.
The aircraft meets the requirements of ASTM, FAA and is certified under Czech LAA and German DULV. Operation of the aircraft is assumed only during the day under VFR rules under VMC conditions.
Modern technology, precise design, maximum emphasis placed on safety and passion for flying. All this manifests our aircrafts.
To see the complete price list of DV-1 Skylark and its components and to find out more about the aircraft, click here.
|Empty weight||287 kg||290 kg|
|Maximum take-off weight||450 kg (472.5 kg w/rescue system)||600 kg|
|Useful load||163 kg||310 kg|
|Fuel tanks capacity||90 l||90 l|
|Maximum baggage weight||20 kg||20 kg|
|Load factors in g’s||(+4, -2)||(+4, -2)|
|Stall speed without flaps||78 km/h||83 km/h|
|Stall speed with flaps||64 km/h||68 km/h|
|Never exceeded speed||267 km/h||267 km/h|
|Maximum horizontal flight speed||230 km/h||230 km/h|
|Travel speed||210 km/h||210 km/h|
|Climb rate||6 m/s||5.9 m/s|
|Ceiling||3650 m||3650 m|
|Range (30 min. reserve)||1000 km||900 km|
|Wing span||8.14 m|
|Aircraft lenght||6.62 m|
|Aircraft height||2.28 m|
|Cabin width||1.09 m|
|Wing area||9.44 m2|
|Horizontal tailplane surface||1,48 m2|
|Vertical tailplane surface||0.9 m2|
|Cruise speed at 3000 ft with 75 % of power||210 km/h|
|Maximum horizontal flight speed||230 km/h|
|Take-off distance to 50 ft (15 m): concrete||265 m|
|Take-off distance to 50 ft (15 m): grass||280 m|
|Braking distance||153 m|
|Range (30 min. reserve)||1000 km|
|Fuel capacity||90 l|
|Average fuel consumption||15 l/h|