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Military and civil transport aircraft of similar type designed for the Soviet Air Force and Aeroflot respectively. Both aircraft carried the NATO reporting name Camp. The prototype of the former was exhibited at Tushino in 1956, powered by two 3,800kW Kuznetsov turboprop engines and with a cannon in a tail turret.
| CREW | 6 |
| PASSENGERS | 70 |
| ENGINE | 2 x turbo-prop AI-20D, 3810 kW |
| WEIGHTS |
| Take-off weight | 43400 kg | 95681 lb |
| Empty weight | 24400 kg | 53793 lb |
| DIMENSIONS |
| Wingspan | 37.0 m | 121 ft 5 in |
| Length | 30.7 m | 100 ft 9 in |
| Wing area | 117.2 m2 | 1261.53 sq ft |
| PERFORMANCE |
| Max. speed | 520 km/h | 323 mph |
| Cruise speed | 450 km/h | 280 mph |
| Ceiling | 9600 m | 31500 ft |
| Range w/max.fuel | 3900 km | 2423 miles |
| Range w/max.payload | 1000 km | 621 miles |
| ARMAMENT | 2 x 23mm machine-guns |
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