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 |