TU-204-300

Presented to your attention Tu-204-300 aircraft is a modification of Tu-204-100 aircraft and differs from its prototype by 6m-shortened fuselage, reduced passenger capacity and increased fuel tank capacity. The aircraft and engines are certified by AR IAC and fully meet international noise level and toxic emission requirements. Passenger Tu-204-300 aircraft supports transportation of up to 162 passengers on air routes of 500 to 9000 km at 1,5 time less fuel consumption in comparison with obsolete domestic analogues.

PASSENGER CABIN

The basic criteria of Tu-204-300 passenger cabin layout   such as flexibility, functionality, full compliance with safety requirements, ergonomics and convenience of operation- fully meet passengers’ and airlines’ needs. Passenger cabin layout can be designed in the economy class variant for 157  seats or in the mixed variant: business (24 passenger seats) and economy class ( 112 passenger seats). The interior of Tu-204-300 aircraft provides high-level comfort for passengers in each class: high ceiling and relatively straight contour of cabin sidewalls; wide enough center aisle and large baggage bins; comfortable passenger seats and conveniently located PSU panels; efficient air-conditioning and ventilation system and low noise level throughout the cabin.

INTERIOR

Tu-204-300 aircraft interior provides high level of comfort for passengers in each class: high ceiling and relatively straight contour of cabin sidewalls; wide enough center aisle and large baggage bins; comfortable seats and conveniently located PSU panels; efficient air-conditioning and ventilation system; low noise level throughout the cabin.

PROFIT-MAKING CAPACITY

Economic analysis and marketing studies of Tu-204-300 aircraft have shown that:

  • Operational efficiency of Tu-204-300 aircraft compared with its domestic analogues is 18% higher by reduced operating costs.
  • Profitability of the aircraft operation on current routes will reach 30 to 40%.
  • Recoupment period of the aircraft on routes it is currently operated with current fares will be 4 to 5 years.
  • To recoup the flight of Tu-204-300 aircraft 78 passenger seats are to be occupied, while under other equal conditions IL-62M requires 105 passengers for a flight recoupment, B-757-200-126 passengers, and IL-96-300-140 passengers.

MAIN PERFORMANCE OF TU-204-300 AIRCRAFT

Passenger cabin  
Standard single-class layout (seat peach 810 mm) 155/157
Standard single-class layout (seat peach 840 mm) 142
Standard two-class layout 136
Baggage compartment capacity at bulky cargo transportation, m3 24,45
Engines 2 x PS-90A
Maximum flight thrust, kgf 16 000
Engine setting take-off at derating setting is possibly
Maximum fuel capacity, t 35,535
Weight performance:  
Maximum take-off weight, t 103,0
Maximum landing weight, t 88,0
Maximum payload, t 18
Maximum flight range, km 9000
Cruising speed, km/h 830-850
Cruising height, m 10100-12100
Required RW length, m 2000
Landing category II
Aerodrome code B
Crew, persons 3
Outside air temperature by the ground, Co +/-45
Certification basis АП-25
The basic dimensions:  
Aircraft length, m 40,19
Aircraft height, m 13,87
Wing span, m 40, 88

More detailed information about Tu-204-300 aircraft can be received from the following sources:

Basic technical data. Tu-204-300 passenger aircraft

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