Specifications
| 204-100 | 204-120 | 204SM | 214 | 204–300 | |
|---|---|---|---|---|---|
| Cockpit crew | Three | Two | Three | ||
| Seating capacity | 210 (1-class, standard) 175 (2-class, standard) |
164 (1-class, standard) 142 (2-class, standard) |
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| Seat pitch | 32 in (1-class, standard) 39 & 32 in (2-class, standard) |
32 in (1-class, standard) 41 & 32 in (2-class, standard) |
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| Length | 46.14 metres (151 ft 5 in) | 40.19 metres (131 ft 10 in) | |||
| Wingspan | 41.8 metres (137 ft 2 in) | ||||
| Wing area | 184.2 square metres (1,983 sq ft) | ||||
| Height | 13.9 metres (45 ft 7 in) | ||||
| Fuselage width | 3.8 metres (12 ft 6 in) | ||||
| Fuselage height | 4.1 metres (13 ft 5 in) | ||||
| Cabin width | 3.57 metres (11 ft 9 in) | ||||
| Cabin height | 2.16 metres (7 ft 1 in) | ||||
| Maximum take-off weight | 103,000 kilograms (230,000 lb) | 105,000 kilograms (230,000 lb) | 110,750 kilograms (244,200 lb) | 107,500 kilograms (237,000 lb) | |
| Maximum landing weight | 88,000 kilograms (190,000 lb) | 89,500 kilograms (197,000 lb) | 93,000 kilograms (210,000 lb) | 88,000 kilograms (190,000 lb) | |
| Maximum payload | 21,000 kilograms (46,000 lb) | 23,000 kilograms (51,000 lb) | 25,200 kilograms (56,000 lb) | 18,000 kilograms (40,000 lb) | |
| Takeoff run at MTOW | 2,250 metres (7,380 ft) | 1,800 metres (5,900 ft) | 2,250 metres (7,380 ft) | 2,500 metres (8,200 ft) | |
| Service ceiling | 12,600 metres (41,300 ft) | 12,100 metres (39,700 ft) | |||
| Cruising speed | 810 km/h to 850 km/h (503 mph to 528 mph) | ||||
| Maximum speed | 900 km/h (560 mph) | ||||
| Range fully loaded | 4,300 kilometres (2,700 mi) | 4,100 kilometres (2,500 mi) | 4,000 kilometres (2,500 mi) | 4,340 kilometres (2,700 mi) | 5,800 kilometres (3,600 mi) |
| Maximum fuel capacity | 41,000 L (9,000 imp gal; 11,000 US gal) | 35,700 kilograms (79,000 lb) | 44,600 L (9,800 imp gal; 11,800 US gal) | 45,000 L (9,900 imp gal; 12,000 US gal) | |
| Engine (x 2) | Aviadvigatel PS-90A | Rolls-Royce RB211-535E4 | Aviadvigatel PS-90A2 | Aviadvigatel PS-90A | |
| Max. thrust (x 2) | 157 kN 16,000 Kgf; 35,274 lbf |
186.3 kN 19,000 Kgf; 41,887 lbf |
157 kN 16,000 Kgf; 35,274 lbf |
158.2 kN 16,140 Kgf; 35,582 lbf |
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Sources: United Aircraft Corporation, Tupolev, 204SM.
Read more about this topic: Tupolev Tu-204