An-74

 Àn-74ÒÊ-200 UR-74026 Aircraft:

Aircraft description
 ÀN-74ÒÊ-200 Aircraft The aircraft is developed for operation over the routes, where transportation of the passengers to one end and cargo on return is required or the kinds of transpiration change from time to time. The aircraft can be converted from a passenger to a cargo aircraft and vice versa.Àn-74ÒÊ-200 provides for transportation of 52 passengers or 10 tones of cargo. The aircraft can be converted from a cargo aircraft to a passenger aircraft and vice versa by the crew for less than 2 hou
Technical characteristics
FLIGHT PERFORMANCE: Year of manufacture 1992 Crew 6 Maximum takeoff weight, t 36,5 Maximum payload, t10,0 Maximum range, km3800 Maximum fuel, kg 13500 Maximum flight rate, km/h 750 Cruising rate, km/h 650 Operating ceiling, m10100 Takeoff roll, m620 Landing run, m420 Required runway length, m1200 POWER PLANT: Engine operating modes: Takeoff: - thrust, kgf (N)6500 (63765) - specific fuel consumption, kg/kgf*h 0,350 Cruising: - thrust, kgf (N)1600 (15696) - specific fuel consumption, kg/kgf*h0,630