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Airline | Aircraft Type | In Service | On Order | Stored |
---|---|---|---|---|
Cairo Aviation | 3 x 204-120 2 x 204-120C | 2 | 0 | 3 |
Dalavia | 214 | 0 | 0 | 3 |
Airstars | 214 | 1 | 0 | 1 |
Orenair | 204-100 | 1 | 0 | 0 |
Air China Cargo | 204-120CE | 0 | 0 | 1 |
DHL Aviation | 204-100C | 1 | 0 | 1 |
China Cargo Airlines | 204-120CE | 0 | 2 | 0 |
Aviastar-TU Co. Ltd | 204 | 4 | 0 | 4 |
KMV | 204-100 | 2 | 0 | 0 |
KrasAir | 214 | 0 | 0 | 1 |
Palestinian Authority (government) | 204-100 | 0 | 1[31] | 0 |
Rossiya (commercial) | 204 | 0 | 0 | 2 |
Rossiya (government)[32] | 214 2 x 204–300 (order) | 6 | 6 | 0 |
Vladivostok Avia | 204–300 | 6 | 0 | 0 |
Cubana | 2 x 204-100CE 2 x 204-100E | 4 | 0 | 0 |
Air Koryo | x1 204–300 x1 204-100[33][34] | 2 | 2 | 0 |
Transaero | 214 | 3 | 7 | 0 |
Iran Air and Iran Airtour[35] | 204 | 0 | 30(−30)[36] | 0 |
Red Wings | 204-100/204SM | 8 | 1 /44 (−44)[37] | 0 |
Business Aero (for VTB) | 204–300A | 1[38] | 0 | 0 |
VIM | 204SM | 0 | 10 | 0 |
Syrianair | 204SM | 0 | 3[39] | 0 |
Total | 40 | 31 | 15 |
Year | 1989 | 1990 | 1991 | 1992 | 1993 | 1994 | 1995 | 1996 | 1997 | 1998 | 1999 | 2000 | 2001 | 2002 | 2003 | 2004 | 2005 | 2006 | 2007 | 2008 | 2009 | 2010 | 2011 |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Produced | 1 | 1 | 2 | 2 | 5 | 2 | 1 | 3 | 1 | 1 | 2 | 4 | 3 | 4 | 4 | 2 | 3 | 4 | 2 | 10 | 6 | 3 | 5 |
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) | |||
Seat pitch | 32 in (1-class, standard) 39 & 32 in (2-class, standard) | 32 in (1-class, standard) 41 & 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 | 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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