SOVA
SOVA selective trainer and utility aircraft
A single-engine, low-wing, four-seat aircraft of semi-monocoque metal construction with fixed landing gear, intended for initial training and pilot selection, sport flying and tourism, and optionally for reconnaissance, aerial photography or carriage of weapons.
Enlarge SOVA selective trainer and utility aircraft
Specification
| Maximum take-off mass | 1200 kg |
|---|---|
| Equipped empty mass | 750 kg |
| Wing surface area | 15.10 m2 |
| Wing span | 9.80 m |
| Overall length | 7.11 m |
| Height | 3.15 m |
| Wheel base | 1.94 m |
| Wheel track | 2.58 m |
| Maximum horizontal speed at sea level | 230 km/h |
| Stall speed, flaps up, idle | 105 km/h |
| Stall speed, flaps down, idle | 95 km/h |
| Best-climb speed | 150 km/h |
| Maximum rate of climb at sea level | 5 m/s |
| Service ceiling | 3200 m |
| Take-off distance over 15 m | 665 m |
| Landing distance from 15 m | 440 m |
| Endurance at economy speed | 4.2 hours |
| Flying range | 675 km |
| Engine | Lycoming IO-390-A3 A6 |
| Engine configuration | Four-cylinder boxer, air cooled, direct injection |
| Maximum continuous power | 154.40 kW (210 hp) |
| Cruise power | 75%; 115.80 kW (157.50 hp) |
| Economy power | 65%; 110.40 kW (136.50 hp) |
| Propeller | Two-blade all-metal constant-speed Hartzell HC-C2YR-1BFP/F7894 |
| Maximum propeller speed | 2700 rpm |
| Propeller diameter | 1.98 m |
All data provided for information purposes; final specification is defined per contract.