Tupolew / Tupolev Tu-124
Regional Airliner
The Tupolev Tu-124 is a twin-engined short- to medium-range jet airliner with a capacity of maximum 56 passengers developed by the Soviet Design Bureau OKB Tupolev.
| Propulsion | 2 Turbofan Engines |
| Engine Model | Soloviev D-20P |
| Engine Power (each) | 52,9 kN | 11892 lbf |
| Speed | 907 km/h | 490 kts
564 mph |
| Service Ceiling | 11.700 m | 38.386 ft |
| Range | 1.220 km | 659 NM
758 mi. |
| Empty Weight | 22.500 kg | 46.604 lbs |
| max. Takeoff Weight | 38.000 kg | 83.776 lbs |
| Wing Span | 25,55 m | 83 ft 10 in |
| Wing Area | 119,0 m² | 1281 ft² |
| Length | 30,58 m | 100 ft 4 in |
| Height | 8,08 m | 26 ft 6 in |
| First Flight | 24.03.1960 |
| Production Status | out of production |
| Total Production | 165 |
| NATO Code | Cookpot |
| Data for (Version) | Tupolev / Tupolew Tu-124V |
| Variants | Tu-124K, Tu-124K2, Tu-124W/V |
