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TU-204C |
Presented to your attention cargo Tu-204C aircraft, manufactured by Ulyanovsk Aviation Industrial Complex ‘Aviastar-SP’, is an up-to-date two-engine aircraft, equipped with domestic PS-90A engines. The aircraft and engines are certified by AR IAC and fully meet international noise level and toxic emission requirements. Maximum aircraft payload is 27 tons.
| Total capacity of cargo cabin, m3 | 170 |
| Total capacity of baggage compartment, m3 | 44,5 |
| Front baggage compartment, m3 | 16 |
| Rear baggage compartment, m3 | 28,5 |
| Engines | 2 x PS-90A |
| Take-off thrust, kgf | 16000 |
| Maximum fuel capacity, t | 32,895 |
| Maximum take-off weight, t | 103,0 |
| Maximum landing weight, t | 89,5 |
| Maximum payload, t | 27,0 |
| Maximum flight range, km | |
| at maximum payload | 3120 |
| at maximum fuel capacity and payload of 13,5 t | 7000 |
| Cruising speed, km/h | 810-850 |
| Range of cruising altitude, km | 10,1-12,1 |
| Required runway length, m | |
| at take-off (take-off run) | 2150 |
| at landing (landing run) | 2140 |
| Landing category | II |
| Aerodrome code | B |
| Crew, persons | 3 |
| Outside air temperature by the ground, C | +/-45 |
| Arranged service life of the aircraft- years/flights/hours | 20/25000/45000 |
| The present stage of serving out of projected service life- years/flights/hours | 12/3000/9000 |
| Scheduled maintenance check intervals, f/h: | |
| Form F1 | 600 |
| Form F2 | 3000 |
| Basic dimensions: | |
| Aircraft length, m | 46,14 |
| Aircraft height, m | 13,87 |
| Wing span, m | 40,88 |
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Modern cargo handling system installed at Tu-204C aircraft lessens work time and decreases expenses connected with aircraft ground time, and this increases flight profitableness. The aircraft is equipped with modern, high-powered, efficient PS-90A engines of Russian manufacture, which provides on-condition maintenance concept. The engine is removed from the aircraft only by completion of the assigned service life or detection of critical condition by the built-in test system and fault diagnosis. |
After-sale support of the aircraft is assured by the conditions to be agreed by the parties including technical assistance, maintenance, performance of service bulletins, repair, supply of spare parts as within warranty period so as during post-warranty period. More detailed information on the system of after-sale support can be found in Clause "After-sale support"
More detailed technical information about the aircraft can be received from the following sources:
Basic technical data. Tu-204C cargo aircraft
Aircraft
Tu-204 is equipped with cargo handling system ‘ANCRA’ (USA), which makes
it possible to operate with 4 type size pallets and containers.. Over-adjustment of
the system for any of these pallets and containers is carried out within
30 minutes and it shortens the period of cargo handling works and decreases
the expenses on aircraft outage in the airport. Cargo handling system
provides transportation of containers and pallets with cargo inside the
fuselage and their fixation. The basic side cargo door is located on the
left side of the fuselage between frames 16-23, opens outside
upwards at an angle of 73 degrees, and is of size of 3408 x 2080 mm with step down height of 3,89 m.
The Tu-204
cockpit is designed on the basis of modern ergonomic and design solutions
connected with implementation of electronic indication and means of
automation of the aircraft control, on aircraft MSN 64024 are installed the
newest multifunctional liquid crystalloid displays. 
Aircraft
Tu-204 are equipped with efficient turbofan trishaft PS-90A engines of JSC 'Perm
motor plant' manufacture with high bypass ratio, mixing of airflow and gas
stream, general jet nozzle and reverse thrust. 
