Il-76MD-90 military transport aircraftis based on the Il-76MD series productionmilitary transport aircraftand is designed for landing and parachuting of military personnel, equipment and various cargos.
The aircraft has more powerful and economic PS-90A-76 engines, which meet ICAO requirements for noise and harmful emissions. Installation of new engines allowed for increasing cost efficiency of the aircraft significantly, due to reduced average fuel consumption in cruise flight, increasingflying range and commercial load, and reducing direct operational costs.
Top thrust (SI system, H=0)4х16000kgf
Maximum takeoff weight195tons
Maximum flight altitude12 100m
Main technical characteristics
Dimensional characteristics Length, m 46,6 Height, m 14,76 Wingspan, m 50,5 Wing area, sq. m. 300 Fuselage diameter, m 4,8 Power plant parameters
Number x engine type 4 x turbojet engine Engine
PS-90A-76 Top thrust (SI system, H=0), kgf 16 000 Weight parameters
Maximum takeoff weight, tons 195 Maximum payload, tons 50 Fuel tank capacity, l 109 500 Aircraft performance Cruising speed, km/h 750–800 Flight altitude, m 9 100–12 100 Flight range with payload of 40 tons, km 5 400 Takeoff distance, m 1 300 Landing distance, m 930 Number of seats
Crew, persons 6 Passengers, persons single-deck version:
145 military personnel
225 military personnel
Freight compartment parameters Length x Width x Height, m 24,54x3,45x3,4 Volume, cubic meters 321 Specified life
Calendar operating life, years 30 Number of flights 4 000 Number of flight hours, hr. 6 000