Iljuschin / Ilyushin Il-103
Trainer / Touring Aircraft
The Ilyushin Il-103 is a single-engine four-seat touring and trainer aircraft developed by the Russian manufacturer JSC Ilyushin Aviation Complex.
| Propulsion | 1 Piston Engine |
| Engine Model | Continental IO-360-ES |
| Engine Power | 149 kW | 200 hp |
| Speed | 220 km/h | 119 kts 137 mph |
| Service Ceiling | 2.999 m | 9.840 ft |
| Rate of climb | 190 m/min | 623 ft/min |
| Range | 1.070 km | 578 NM 665 mi. |
| Empty Weight | 915 kg | 2.017 lbs |
| max. Takeoff Weight | 1.285 kg | 2.833 lbs |
| Wing Span | 10,56 m | 34 ft 8 in |
| Wing Area | 14,7 m² | 158 ft² |
| Length | 8,00 m | 26 ft 3 in |
| Height | 3,14 m | 10 ft 4 in |
| First Flight | 17.05.1994 |
| Production Status | in production |
| ICAO Code | I103 |
| Data for (Version) | Iljuschin / Ilyushin Il-103 |