Il-96-400T
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Performance
General Data
The Il-96-400T airplane is a freight modification of the Il-96-300 developed with consideration of comments from air carriers and meeting all modern requirements both in Russia and in the global sphere.Fuselage length of Il-96-400T is extended by 9,35 m, in comparison with the baseline aircraft Il-96-300. It is fitted with Russian equipment including the four fan-type engines PS-90A1 with thrust of 17,4 tons each.
The main distinction of the freight plane Il-96-400T from its passenger version is that the passenger cabin has been reconstructed into the cargo compartment, with a reinforced bottom section and installation of additional rails for mounting floor-based mechanical gear, meant for handling of international aircraft pallets and containers. Configuration of cargo deck in the Il-96-400T allows for the use of various patterns of loading and palletizing when placing the cargo. Maximum commercial load is 92 tons.
The aircraft has two cargo decks, an upper and a lower deck.Maximum takeoff weight is 270 tons. The aircraft complies with requirements of Appendix 16 Chapter 4 ICAO on noise emissions.
Top thrust (SI system, H=0)
4х17400kgfMaximum takeoff weight
270tonsMaximum flight altitude
13 100m
Another figureMain 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
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 92 Fuel tank capacity, l 150 000 Number of seats
Crew, persons 6 Freight compartment parameters (upper deck) Length x Width x Height, m 44,9x4,8x3,3 Volume, cubic meters 776 Specified life
Calendar operating life, years 20 Number of flights 3 000 Number of flight hours, hr. 22 000