| Technical data | |
|---|---|
| Type | Tu-214 |
| Function | Passenger Transport |
| Year | 1996? |
| Crew | 3 |
| Engines | 2*16000kg PS-90A |
| Length | 46.0m |
| Height | 13.9m |
| Wingspan | 42.0m |
| Wing area | 182.4m2 |
| Empty weight | 50000kg |
| Empty equipped | 59000kg |
| Loaded weight (max) | 110750kg |
| Landing weight (max) | 89500kg |
| Wing Load (kg/m2) | 607 |
| Thrust to Weight |
0.28 |
| Cruise Speed | 830km/h |
| Landing Strip (sea level) | 2000m |
| Range (maximum load) | 6500km |
| Cruise Ceiling | 7200m |
| Service Ceiling | 12100m |
| Payload | |
| Maximum Load (total) | 50000kg |
| Fuel | 32000l |
| Cabin size LxWxH | 30.18x 3.57x 2.16 m3 |
| Seats (economy only) | 210 |
| Seats (economy+ business) | 196 |
| Seats (economy+ business+ first) | 168 |
Tu-214 (Tu-204-200) by Tupolev KB
 |
(From 's Gallery
Version of the Tu-204 (Tu-204-200) with extended range and increased payload. Aircraft has strengthened airframe and additional fuel tank. It is designed to transport cargo/passengers on the medium or long-range routes. Tu-214 can carry up to 210 passengers or 18 cargo containers. Configurations include 6 containers and 130 passengers, 16 containers and 30 passengers.
Electronic and navigation equipment identical to the Tu-204, with provision for SAT-906 satellite communication set and TCAS collision preventing system.
Capabilities of the Kazan Aviation Industrial Association (KAPO) allow to roll out up to 24 aircraft per year. Five pre-series aircraft assembly started in second half of 1994. Aircraft is in series production since 1996.
| Predecessors | Modifications |
|---|---|
 Tu-204 |
 Tu-204-200S |
| References | Links |
|---|---|
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