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Aircraft type: Commercial airplane
Manufacturer: Tupolev
Maiden flight year: 1989
Tu-204-100 | Tu-204-120 | |
Dimensions | ||
---|---|---|
Length (m) | 46.2 | 46.2 |
Wingspan (m) | 42.0 | 42.0 |
Height (m) | 13.9 | 13.9 |
Wing area (m2) | 182.4 | 182.4 |
Weight | ||
Maximum take-off weight (kg) | 103 000 | 103 000 |
Maximum landing weight (kg) | 89 500 | 88 200 |
Operating empty weight (kg) | 56 920 | 59 300 |
Maximum zero fuel weight (kg) | 83 575 | 80 300 |
Maximum payload (kg) | 21 000 | 21 000 |
Standard fuel capacity (litres) | 30 812 | 30 812 |
Performance | ||
Maximum range (km) | 6 900 | 7 000 |
Range with max payload (km) | 4 400 | 4 500 |
Cruise speed (km/h) | 810 | 850 |
Maximum operating altitude (m) | 12 500 | 12 500 |
Take-off field length (m) | 2 150 | |
Landing field length (m) | 2 130 | |
Engines | PS-90A, 2 x 35250 lb | Rolls-Royce RB211-535E4B, 2 x 43070 lb |
Fuel efficiency (g/pass*km) | 19.6 | 19.1 |
Fuel flow rate (kg/h) | 3 460 | 3 420 |
Cabin Data | ||
Passengers (1-class) | 214 | 214 |
Passengers (2-class) | 196 | 196 |
Passengers (3-class) | 190 | 190 |
Economy seat pitch (cm) | 81 | 81 |
Cabin width (m) | 3.57 | 3.57 |
62% | 23% | 15% |