BASIC TECHNICAL DATA

 

Tu-204-300 passenger aircraft

Herewith we present to your attention the Tu-204-300 aircraft, a modification of Tu-204-100 aircraft with 6 m shortened fuselage, lesser passenger carrying capacity and increased flight range.

Tu-204-300 aircraft are equipped with Russian engines of PS-90A type.

Up-to-date, powerful and fuel-efficient engines support the on-condition maintenance concept. Engine is to be removed from the aircraft only if the service life is served out or the critical condition is detected by the engine monitoring and crew alert system.

 

PS-90A engines are certified by Aviation Register of Interstate Aviation Committee and fully meet international noise level and toxic emission requirements.

Tu-204-300 passenger aircraft makes it possible to carry up to 162 passengers on air routes of 500 to 8,500 km range with 1.5 times lesser fuel consumption compared with its obsolete domestic analogues.

Passenger service units are installed on overhead baggage bins in accordance with the pitch of passenger seats. To improve comfortability and ecological safety of passengers and crew the air conditioning system incorporates Engelhard ozone converters, air humidifying system in the cockpit, and filters for cleaning off smoke and microbiological components from air. The aircraft can have installed galley equipment of domestic and foreign production. Lavatories are equipped with smoke detection systems and built-in fire extinguishers. Baggage compartments are equipped for carrying cargo “in bulk”.

Up-to-date digital Integrated Flight and Navigation Complex with foreign laser gyro inertial navigation systems and radio communication equipment installed on the aircraft complies with all effective ICAO regulations for flights on international routes and assures the following:

•                     vertical separation of 1000 ft (300 m) between flight levels 290-410 (RVSM);

•                     ICAO Category II automatic approach;

•                     VHF/FM-immunity of short-range navigation and landing systems ILS, VOR;

•                     Automated construction of flight plan using standard procedures for departure (SID) and arrival (STAR);

•                     Automatic loading of air navigation information onboard the aircraft;

•                     Vertical navigation mode provided by Navigation Computer System;

•                     Automatic modes “Reaching the flight level (H specified)”, Indicated Air Speed hold and M Number hold in climb and cruise, and vertical speed Vy hold provided by Automatic Flight Director System and Thrust Management System.

At the customer’s option, the aircraft can be equipped with inertial systems Litton LTN-101 or Honeywell HG 1150, Inertial Reference System ‘ÁÈÍÑ-85’ integrated with satellite navigation systems GPS LTN-2001 or ‘ÑÍÑ-2’ operating in the systems ÃËÎÍÀÑÑ (Global Satellite Navigation System) / NAVSTAR. This allows to meet RNP-5 requirements for BRNAV area navigation with further stage-by-stage modification to RNP-1 requirements.

The integrated flight and navigation complex may incorporate Honeywell (USA) traffic collision avoidance system TCAS-II with Mode S transponder.

To comply with ICAO requirements the radio communication equipment includes VHF radio stations with 8,33/25kHz channel spacing.

To provide for the flights on air routes with the breaks in FM-communication of more than one hour the second SW-radio station is installed.

Tu-204-300 aircraft have air-heat protection of slats against icing in flight conditions.

Airborne flight data recorders are equipped with underwater locator beacons.

Product support of the aircraft is assured by the conditions to be agreed by the parties, covering technical assistance, maintenance, performance of service bulletins, repair, supply of spare parts as within warranty period so as during post-warranty period.

 MAIN PERFORMANCE OF TU-204-300 AIRCRAFT

 

Item

Performance

Tu-204-300

1.       

Aircraft length

40.19 m

2.       

Maximum takeoff weight

103 t

3.       

Fuel quantity

35 t

4.       

Power
plant

Engine type x No. of engines

2õPS-90À

5.       

Cruising speed

830-850 km/hr

6.       

Cruising altitude

10100 ¸12100 m

7.       

Maximum payload

18 t

8.       

Actual
flight range

with maximum payload

with maximum pax seats occupied

5600 km

6500 km

 

 

with 100 pax seats occupied

8500 km

9.       

Crew

3 persons

10.   

Passenger-carrying
capacity in economy class

number of passengers

162

11.   

Aerodrome code letter

Â/Á

12.   

Landing category

II

13.   

Field length required, m

2000

14.   

Outside air temperature at the ground, TH

±45°Ñ

15.   

Friction factor

0.3  m

16.   

Aerodrome altitude, not more than

2000 m

17.   

Certified to comply with

AP-25

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