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Tu-204-300

Tu-204-300

585/152

Aircraft Tu-204-300 is an up-to-date twin-engine airliner of high fuel efficiency and comfort level.

Tu-204-300 is the first state-of-the-art Russian aircraft that can fly for long distances without intermediate stops for refueling. That means for passengers to be able to get to Moscow from Vladivostok in 9 hours only, and for the airline companies, to significantly reduce costs, including fuel expenses.

Tu-204-300 passenger aircraft manufactured by CJSC “Aviastar-SP” as well as engines PS-90A are certified by AR IAC and fully comply with international requirements regarding perceivable noise and emission.

The aircraft Tu-204-300 competitiveness, high efficiency in service and high flight performance characteristics are due to:

Performance:

Maximum takeoff weight, t

107.0 (105.0)

Maximum payload, t

18

Fuel weight, t

36

Passenger capacity, pers

 

Economy-class

156

Economy- + business-class

142

Cruise speed, km/h

830-850

Cruise altitude, km

10.1-12.1

(t = 15°С, P = 760 mm. Hg)

1,870

2 turbofan engines

PS-90A

Landing category

II

Power plant PS-90A

Tu-204-300 aircraft are equipped with up-to-date and efficient PS-90A engines.

The PS-90A is a turbofan high by-pass ratio exhaust mixing engine with a common exhaust nozzle and a thrust reverser.

The engine design includes a number of technical solutions, aimed at providing high economy efficiency and weight perfection.

Aircraft Tu-204-300 powered with engines PS-90A fully complies with ICAO Chapter 4 Appendix 16 perceivable noise requirements as well as those of ICAO Appendix 16 (volume 2) concerning emission due to perfection of the engine design structure and selected noise absorbing devices.

PS-90A performance:

Takeoff thrust (ISA, H=0), kgf

16,000

Maximum cruise thrust (ISA + 10°С, Н=11 km, М=0.8), kgf

3,400

By-pass ratio at maximum thrust

4.7

Pressure ratio at maximum thrust

31.1

Air consumption, kg/s

485

Cruise specific fuel consumption, kg/kgf h

0.595

Fan diameter, m

1.90

Engine length with air intake, mm

5,530

Engine weight, kg

4,800

Layout variants

Interior

  • High level of individual comfort for passengers
  • Spacious overhead compartments and large cargo compartments under passenger cabin.
  • Multilevel lighting system
  • Sound absorbing structures, providing low noise level
  • Audio and video systems for in-flight entertainment
  • All materials, used in the passenger cabin interior, meet fireworthiness, smoke emission and toxicity standards

Cockpit

The cockpit is developed on the basis of up-to-date ergonomic and design solutions based on using electronic indication and flight control automation means.

 

 

 

Tu-204-300 has got a Perceivable Noise Certificate. This certificate confirms compliance of the aircraft being delivered with the requirements of Chapter 4 Appendix 16 ICAO Convention (volume 1) as well as those of Aviation Rules Part 34, 2008.

Payload-Range

Airplane maintenance

Estimated service life, life time

> 

45,000 flight hours

25,000 flights

20 years

It is possible to extend service life and life time up to

> 

60,000 flight hours

40,000 flights

25 years

The aircraft functional systems and airborne equipment are operated by on-condition basis.

The aircraft is certified in accordance with Russian standards AP-25. Tu-204-300 is being successfully operated in a 142 passenger seats version in the Vladivostok Avia airlines company.