Kappa 77 KP 2U-SOVA
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The Kappa 77 KP 2U-SOVA is a two-seat civil utility aircraft designed in the Czech Republic and available in kit form for homebuilding. It is a conventional low-wing monoplane featuring all-metal construction and retractable tricycle undercarriage. It is marketed in the United States by Aero Adventure Aviation.
[edit] Specifications (KP 2U-SOVA)
General characteristics
- Crew: one pilot
- Capacity: one passenger
- Length: 7.17 m (23 ft 7 in)
- Wingspan: 9.90 m (32 ft 6 in)
- Height: 2.60 m (8 ft 7 in)
- Wing area: 11.9 m² (128 ft²)
- Empty weight: 285 kg (682 lb)
- Max takeoff weight: 450 kg (1,058 lb)
- Powerplant: 1× Rotax 912 , 80/100 hp (60/77 kW)
Performance
- Maximum speed: 260 km/h (160 mph)
- Range: 875 km (547 miles)
- Rate of climb: 450 m/min (1,475 ft/min)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.[edit] Related content
Designation sequence
KP 2 - KP-5
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