The Il-96-400M is a wide-body long-range airliner which is created on the basis of the production Il-96 aircraft for the purpose of further development of this type of aircraft and increasing their transport capabilities due to the longer fuselage and more powerful PS-90A1 engines instead of PS-90A.
The Il-96-400M can carry up to 370 passengers. Large diameter of the fuselage provides modern day level of comfort for passengers during long flights. In terms of reliability, safety and effectiveness the Il-96-400M is on the level with world analogues.
Due to the usage of modern systems and “glass cockpit” the flight crew of the aircraft will consist of 3 people.
The aerodynamic configuration, design and aircraft systems employ state-of-the-art engineering solutions, which ensure high level of safety and effectiveness of aircraft operation. Modern materials used in the structure allow for decrease of aircraft weight, at the same time providing necessary integrity and stiffness. Wing aerodynamic ensures reliable and safe flight within the whole operational speed range.
Top thrust (SI system, H=0)4х17 400kgf
Maximum takeoff weight270tons
Flight altitude13 100m
Estimated technical characteristics
Dimensional characteristics Length, m 63,939 Height, m 15,717 Wingspan, m 60,105 Wing area, sq. m. 350 Fuselage diameter, m 6,08 Power plant parameters
Number x engine type 4 x turbojet engine Engine model PS-90A1 Top thrust (SI system, H=0), kgf 17 400 Compliance with ICAO standards Appendix 16, Chapter 4 Weight parameters
Maximum takeoff weight, tons 270 Maximum payload, tons 58 Fuel tank capacity, l 150 000 Aircraft performance Cruising speed, km/h 830-850 Flight altitude, m 9 100–13 100 Flight range with passengers, km 8 750 Takeoff distance, m 2 020 Landing distance, m 1 200 Number of seats
Crew, persons 3 Passengers, persons single-class configuration 370
Calendar operating life, years 20 Number of flights 20 000 Number of flight hours, hr. 60 000