Tupolev Tu-204
Specifications
Sources: United Aircraft Corporation, Tupolev, 204SM.

Tupolev Tu-204

Section Title: Specifications
Table Section Text: Sources: United Aircraft Corporation, Tupolev, 204SM.

204-100	204-120	214	204-300	204SM

Cockpit crew	Three	Two

Seating capacity	190 (1-class, standard) 172 (2-class, standard) 210 (maximum)	210 (1-class, standard) 180 (2-class, standard)	156 (1-class, standard) 142 (2-class, standard)	194 (1-class, standard) 176 (2-class, standard) 215 (maximum)

Seat pitch	32 in (1-class, standard) 47 & 32 in (2-class, standard)	32 in (1-class, standard) 39 & 32 in (2-class, standard)	32 in (1-class, standard) 46 & 32 in (2-class, standard)	32 in (1-class, standard) 38 & 32 in (2-class, standard)

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	105,000 kilograms (231,000 lb)	103,000 kilograms (227,000 lb)	110,750 kilograms (244,160 lb)	107,000 kilograms (236,000 lb)	108,000 kilograms (238,000 lb)

Maximum landing weight	88,000 kilograms (194,000 lb)	93,000 kilograms (205,000 lb)	88,000 kilograms (194,000 lb)	89,500 kilograms (197,300 lb)

Maximum payload	21,000 kilograms (46,000 lb)	25,200 kilograms (55,600 lb)	18,000 kilograms (40,000 lb)	23,000 kilograms (51,000 lb)

Takeoff run at MTOW	1,780 metres (5,840 ft)	2,030 metres (6,660 ft)	1,870 metres (6,140 ft)	1,950 metres (6,400 ft)

Service ceiling	12,100 metres (39,700 ft)	12,200 metres (40,000 ft)

Cruising speed	810 to 850 km/h (500 to 530 mph)

Maximum speed	900 km/h (560 mph)

Range (Max payload)	4,300 kilometres (2,700 mi)	4,100 kilometres (2,500 mi)	4,340 kilometres (2,700 mi)	5,800 kilometres (3,600 mi)	4,200 kilometres (2,600 mi)

Maximum fuel capacity	35,700 kilograms (78,700 lb)	36,000 kilograms (79,000 lb)	35,800 kilograms (78,900 lb)

Engine (x 2)	Aviadvigatel PS-90A	Rolls-Royce RB211-535E4B	Aviadvigatel PS-90A	Aviadvigatel PS-90A2

Max. thrust (x 2)	157 kN 16,000 Kgf; 35,274 lbf	192 kN 19,000 Kgf; 43,100 lbf	158.2 kN 16,140 Kgf; 35,582 lbf	171.6 kN 17,500 Kgf; 38,581 lbf

Sentence(s)

The Tu-204-120 variant has Rolls-Royce RB211-535E4 engine.
The Tu-204-120 variant, with Rolls-Royce RB211-535E4 engines.

final_sentence: The Tu-204-120 variant has Rolls-Royce RB211-535E4 engine.
final_sentence: The Tu-204-120 variant, with Rolls-Royce RB211-535E4 engines.