The IL-96-400M aircraft is a modification of the IL-96-300 airliner and is designed to carry passengers, baggage and cargo on long-distance mainline airlines with intensive passenger traffic.
Main technical characteristics of the IL-96-400M aircraft
Geometric:
Length, m - 64,69; Height, m - 15,88; Wingspan, m - 60,105; Wing area, m² - 350; Fuselage diameter, m - 6,08
Characteristics of the power plant:
Number*type of engine - 4*TRDD; Engine - PS-90A1; Maximum thrust (MCA, H=0), kgf - 4*17400; Compliance with ICAO standards - app. 16, Ch.4
Mass characteristics:
Maximum take-off weight, tonnes - 270; Maximum payload, tonnes - 58; Fuel tank capacity, litres - 150000;
Flight characteristics:
Cruising speed, km/h - 830-850; Flight altitude, m - up to 13100; Range with maximum payload, km - 8750; Range, km / flight with 40t load,km - 10200; Run-up length, m - 2100; Run-down length, m - 950.
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