Iljuschin / Ilyushin Il-12
Photo ©: Francisco José Jurado Ariza (Photos at airliners.net)
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.
| Crew | 3 | |
| Passengers | 18-32 | |
| Propulsion | 2 Radial Engines | |
| Engine Model | Schwetsow / 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 | 104,0 ft |
| Wing Area | 100,0 m² | 1076 ft² |
| Length | 21,30 m | 69,9 ft |
| Height | 8,07 m | 26,5 ft |
| 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 | |
Remarks
The Il-12 is based on the Lisunov Li-2, a modified copy of the Douglas DC-3.
| Extras | |
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