Tupolev Tu-204

· Tupolev · 2 × Aviadvigatel PS-90

Airplanes

Length

46.14 m

Flat Wing Span

41.8 m

Height

13.9 m

Max Seating

172

Max Ceiling

12100 m

Number of Engines

Aircraft Engine

First Flight

1989-01-02

Entry Into service

1996-02-23

Number Built

Maximum Take-Off Weight

105 t (paragliders: kg)

Maximum Range

4300 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Tupolev Tu-204	105	4300

Name	Family	Aircraft Engine	Length (m)	Flat Wing Span (m)	Two Class Typical Seating	Max Seating
Airbus CC-150 Polaris			46.66	43.9		194	Compare
757-200		Pratt & Whitney PW2000	47.3	38			Compare
Boeing C-32		Pratt & Whitney PW2000	47.244	37.7952			Compare
Beriev A-40		Soloviev D-30	43.84	41.62			Compare
A321-251N	A320	LEAP-1A35A/33/33B2/32/30	44.51	35.8	206	244	Compare
Boeing YC-14		General Electric CF6	40.14	39.32		150	Compare

All data (23 fields)

Name: Tupolev Tu-204
Manufacturer: Tupolev
Description: The Tupolev Tu-204 () is a twin-engined medium-range narrow-body jet airliner capable of carrying 210 passengers, designed by Tupolev and produced by Aviastar-SP and Kazan Aircraft Production Association.
ICAO Code: T204
First Flight: 1989-01-02
Entry Into service: 1996-02-23
Designer: Tupolev
Type: Narrow-body jet airliner
Length (m): 46.14
Height (m): 13.9
Max Seating: 172
Max Ceiling (m): 12100
Capacity Description: 172–210
National Origin: Soviet Union
Number Built: 89
Powerplant Description: -100: Aviadvigatel PS-90A, -120: Rolls-Royce RB211-535E4B
Primary Users: Russian Air Force, Red Wings Airlines, Cubana de Aviación, Air Koryo
Status: In service, in production
Wikipedia Article (URL): en.wikipedia.org/wiki/Tupolev_Tu-204
Flat Wing Span (m): 41.8
Wake Category: M
Aircraft Engine: Aviadvigatel PS-90
Number of Engines: 2