Commercial Aircraft Directory - Aircraft Specification

Tupolev - Tu-214

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: 21 Mar 1996  
Certification date: Apr 1997  

PRINCIPAL DIMENSIONS

Fuselage width:  
Fuselage height: 13.9 m 
Fuselage length: 46 m 
Cabin length: 30.18 m 
Cabin width: 3.8 m 
Cabin height: 4.1 m 
Cabin volume:  
Hold volume: 26 m3 

WEIGHTS

Empty operating: 59,000 kg 
Max zero fuel: 84,200 kg 
MTOW: 110,750 kg 
MLW: 93,000 kg 
Standard fuel capacity: 40,730 kg 
Max fuel capacity: 40,730 kg 

SPEEDS

Normal cruise: 808 km/h 
Max cruise: 850 km/h 

PERFORMANCE

Long Range Cruise alt:  
Max ceiling: 12,101 m 
Take off field length:  
Landing field length:  
Max Payload Range: 4,340 m 
Range notes:  
Max passengers: 212  
Typical passengers: 184  

POWERPLANT

Category: Turbofan  
Manufacturer: KMPO  
Model/Submodel: NK-93  
Thrust: 176 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: Perm / Aviadvigatel  
Model/Submodel: PS-90 A2  
Thrust: 157 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: Perm / Aviadvigatel  
Model/Submodel: PS-90 A  
Thrust: 156 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: Perm / Aviadvigatel  
Model/Submodel: PS-90 A2  
Thrust: 157 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: Perm / Aviadvigatel  
Model/Submodel: PS-90 A  
Thrust: 156 kN