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Tu-204-100Е/100В

Tu-204-100Е/100В

585/152

The aircraft completely fulfils modern and advanced ICAO and Eurocontrol requirements on ecology and airport noise.

Tu-204-100Е/100В are modern medium-range narrow-body twin-engine aircraft with high fuel efficiency and level of comfort.  Tu-204-100E/100B 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.

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.

Payload-Range

Interior

Tu-204-100Е/100В 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.

The aircraft Tu-204-100E/100B competitiveness, high efficiency in service and high flight performance characteristics are due to:

Performance:

Maximum takeoff weight, t

105

Maximum payload, t

21

Fuel weight, t

35.71

Passenger capacity, pers

190/172

Cruise speed, km/h

810-850

Cruise altitude, km

11.1-12.1

Takeoff distance, m
(t = 150, P = 760 mm. Hg)

1,780

2 turbofan engines

PS-90A

Landing category

II

Power plant
Tu-204-100Е/100В aircraft are equipped with up-to-date powerful 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-204-100Е/100В 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

3400

By-pass ratio at maximum thrust

4.7

By-pass 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

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