There are 3 images added on 24 February 2007
Initial Operational Capability (IOC): 4 July 2001
Maiden Flight: 21 March 1996
Total Production: ?
Also Known As: Tu-204-214 and Tu-214ON
Origin: Russia
Corporations: Aviastar-SP, KAPO Gorbunov and PSC Tupolev
Parent System: Tu-204
Initial Operational Capability (IOC): 1994
Total Production: ?
Family Members: Tu-204-120, Tu-204-300 and Tu-204C
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Description: The Tu-204 is a twin-engine, medium range family of aircraft capable of carrying from 164 to 210 passengers and/or cargo at ranges from 4,100 km to 5,800 km. Provided with state-of-the-art equipment, the Tu-204 aircraft family outstands by its compliance with western standards for low operating costs, cabin comfort, low noise level and low fuel consumption. The aircraft is fully compliant with Russian and European airworthiness standards. Originally, it was intended as a replacement for Soviet Tu-154 airliners but political turmoil and program slow run have doomed these plans.

The Tu-204 aircraft family includes the Tu-204-100/120 airliner; the Tu-204C freighter; the Tu-214 jetliner featuring increased maximum take off weight, payload and range over its predecessors; and the longer range Tu-204-300 airliner with decreased seating capacity, shortened fuselage and a maximum range of 5,800 kilometers. Production of the Tu-204/214 aircraft family is being carried out at Russian aircraft plants in Ulianovsk (Aviastar-SP) and Kazan. The first Tu-204-100 aircraft was certified by Russian authorities in 1994 and the Tu-204-120 powered by Rolls Royce engines was certified three years later.

The Tu-214 is an improved version of Tu-204 with increased takeoff weight, fuel load, payload and slightly longer range (4,340 km vs. 4,300 km on the Tu-204-100). The Tu-214 was certified according to Russian standards AP-25. The Tu-214ON is used by Russia for international aerial inspections under the Open Skies Treaty.

Tu-214 Applications

Support Aircraft Tu-214R Tu-214SR

Tu-214 Specifications

Number of Engines: 2
Passengers: 210
Wing Area: 184 square meter
Fuselage Diameter: 4.10 meter
Height: 13.9 meter
Length: 46 meter
Wingspan: 42 meter
Max Range: 4,340 kilometer (2,343 nautical mile)
Take Off Run Distance: 2,250 meter
Cruise Speed: 850 kph (0.71 mach)
Fuel Load: 35.7 ton
Max Takeoff Weight: 111 ton (244,158 pound)
Payload: 25.2 ton
Thrust: 70,000 pound
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Tu-214 News

There are 6 news between
28 Nov 2008 and 9 Jul 2018
Monday, July 9, 2018Russian Air Force Developing New Porubshchik-2 Electronic Warfare Aircraft
Monday, June 2, 2014Russian Air Force Unveils 2014 Weapons Procurement Plan
Thursday, August 18, 2011Russia to Get Second Tu-214ON Aircraft for Open Skies Inspections in 2012
Saturday, October 17, 2009First Flight for PS-90A2 Engine Test-bed
Monday, June 1, 2009First Two Tu-214SR Jets Delivered to the Administration of the President of Russian Federation
Friday, November 28, 2008Transaero Takes Delivery of Second Tu-214 Jet

Operators & Related Equipment

Ordered by Dalavia, GTK Russia, KrasAir and TransAero (10). Russia also operates two Tu-214ON for international aerial inspections under the Open Skies Treaty.

Grand Total ?1
Propulsion Systems
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