Iljuschin / Ilyushin Il-12
Airliner / Transport Aircraft
The Ilyushin Il-12 is a twin-engined short-range airliner for max. 32 passengers and transport aircraft developed by the Soviet design bureau Ilyushin OKB.
Propulsion | 2 Radial Engines |
Engine Model | Shvetsov ASh-82FN |
Engine Power (each) | 1360 kW | 1824 hp |
Speed | 376 km/h | 203 kts 234 mph |
Service Ceiling | 6.700 m | 21.982 ft |
Range | 2.000 km | 1.080 NM 1.243 mi. |
Empty Weight | 9.000 kg | 19.842 lbs |
max. Takeoff Weight | 17.000 kg | 37.479 lbs |
Wing Span | 31,70 m | 104 ft 0 in |
Wing Area | 100,0 m² | 1076 ft² |
Length | 21,30 m | 69 ft 11 in |
Height | 8,07 m | 26 ft 6 in |
First Flight | 07. Jan. 1946 |
Production Status | out of production |
Total Production | ca. 3000 |
Developed from | Lisunow / Lisunov Li-2 (Douglas DC-3) |
NATO Code | Coach |
Data for (Version) | Iljuschin / Ilyushin Il-12 |