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)

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[edit] General characteristics

  • Crew: one pilot
  • Capacity: 1 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: 285 kg (682 lb)
  • Loaded: kg ( lb)
  • Maximum takeoff: 450 kg (1,058 lb)
  • Powerplant: Rotax 912, 80 hp (60 kW)

[edit] Performance

  • Maximum speed: 240 km/h (150 mph)
  • Range: 875 km (547 miles)
  • Service ceiling: m ( ft)
  • Rate of climb: 450 m/min (1,475 ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Power/Mass: kW/kg ( hp/lb)

[edit] Related content

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Comparable aircraft:

Designation sequence: KP 2 - KP-5

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