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Tu-204СМ

Tu-204СМ

585/152

The aircraft meets Russian and international flight safety requirements, including newly introduced requirements of ICAO and Eurocontrol, and ETOPS-120 requirements. According to its performance, Tu-204СМ is highly competitive with its foreign analogues.
Tu-204СМ exceeds its predecessors of the Tu-204 family in navigational and flying performance, meets world's fuel efficiency, comfortability and maintenance performance requirements, including ICAO Chapter 4 perceivable noise requirements.
By the decision of the Aviation Register of the Interstate Aviation Committee, a Supplement to Type Certificate No СТ223-Ту-204-120CE/Д10 for Tu-204СМ aircraft was issued to "Tupolev" JSC on 31/05/2013.
The program of developing modernized Tu-204СМ aircraft includes the following:

 

Tu-204CM aircraft realizes the concept of significant extent of computerization of flight control processes on all flight phases: 

Passengers of Tu-204CM are provided with high level of individual comfort: spacious overhead compartments, sound absorbing structures, providing low noise level in the passenger cabin. The aircraft has audio and video systems for in-flight entertainment of passengers and solid-state lighting equipment.

Performance:

Flight crew size

2 pers.

Number of passengers

166-215 pers.

Maximum takeoff weight

108,000 kg

Maximum landing weight

89,500 kg

Maximum payload

23,000 kg

Maximum fuel weight

35,800 kg

Cruise speed

830-850 km/h

Cruise altitude

10,600-12,200 m

Range with maximum payload

4,200 km

Aerodrome class

B (code D ICAO)

Runway length

1,950 m

Landing category

IIIA

Perceivable noise

according to ICAO Chapter 4 Annex 16

Estimated service life

60,000 f.h.
45,000 flights
25 years

Payload-Range
Power plant PS-90A2
The engines PS-90A2, certified according to AP-33, are used as a power plant of Tu-204СМ.
The engine design includes a number of technical solutions, aimed at high operating economy and extended time between overhauls.
 The engine is certified in accordance with AP-33.
Service life of the main parts:
- cold portion, cycles - 20,000
- hot portion, cycles - 10,000
- increased time between overhauls
Engine start and operation on the ground can be performed at the altitude up to 4,500 m, and during flight - up to 12,000 m. Engine operation within specified performance is provided at an ambient temperature on the ground from -50°С to +45°С. Engine start is performed at an ambient temperature of -40°С and above.

Emergency thrust (repeatedly), kgf
(Н=0, V=0, ISA)

17,500

Specific fuel consumption, kg/kgf h

0.396

Bypass ratio

4.5

Engine weight (except pylon), kg

4,800

Maximum cruise thrust, kgf

3,500

Cruise specific fuel consumption, kg/kgf h

0.60

Proposed layout variants

 

Payload-Range