Suchoi / Sukhoi Su-26
Aerobatic Aircraft
The Sukhoi Su-26 is a single-engine single-seat aerobatic aircraft developed by the Soviet Design Bureau Sukhoi, today Sukhoi JSC (Russia).
| Propulsion | 1 Radial Engine |
| Engine Model | Vedeneyev M-14P |
| Engine Power | 268 kW | 359 hp |
| max. Cruise Speed | 309 km/h | 167 kts
192 mph |
| max. Speed (vne) | 450 km/h | 243 kts
280 mph |
| Service Ceiling | 4.000 m | 13.123 ft |
| Range | 895 km | 483 NM
556 mi. |
| Empty Weight | 700 kg | 1.543 lbs |
| max. Takeoff Weight | 962 kg | 2.121 lbs |
| Wing Span | 7,80 m | 25 ft 7 in |
| Wing Area | 11,8 m² | 127 ft² |
| Length | 6,83 m | 22 ft 5 in |
| Height | 2,89 m | 9 ft 6 in |
| First Flight | 30.06.1984 |
| Production Status | out of production |
| Total Production | >50 |
| ICAO Code | SU26 |
| Data for (Version) | Sukhoi / Suchoi Su-26M |
| Variants | Su-26M, Su-26MKh, Su-26M2 |
