Commercial Aircraft Directory - Aircraft Specification

Airbus - A310-200

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: 3 Apr 1982  
Certification date: 11 Mar 1983  
Launch customer(s): Swissair
 

PRINCIPAL DIMENSIONS

Fuselage width: 5.64 m 
Fuselage height: 7.56 m 
Fuselage length: 45.89 m 
Cabin length: 33.24 m 
Cabin width: 5.28 m 
Cabin height: 2.54 m 
Cabin volume:  
Hold volume: 79 m3 

WEIGHTS

Empty operating: 79,450 kg 
Max zero fuel: 113,000 kg 
MTOW: 142,000 kg 
MLW: 123,500 kg 
Standard fuel capacity: 54,920 kg 
Max fuel capacity: 54,920 kg 

SPEEDS

Normal cruise: 838 km/h 
Max cruise: 895 km/h 

PERFORMANCE

Long Range Cruise alt: 11,278 m 
Max ceiling: 12,192 m 
Take off field length: 1,550 m 
Landing field length: 1,150 m 
Max Payload Range: 6,667 m 
Range notes:  
Max passengers: 275  
Typical passengers: 220  

POWERPLANT

Category: Turbofan  
Manufacturer: GE  
Model/Submodel: CF6 80C2  
Thrust: 282 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: GE  
Model/Submodel: CF680C2A8  
Thrust: 262 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: GE  
Model/Submodel: CF6 80C2A2  
Thrust: 238 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: GE  
Model/Submodel: CF6 80A2  
Thrust: 222 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: GE  
Model/Submodel: CF680A3  
Thrust: 222 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: Pratt & Whitney  
Model/Submodel: PW4000-94 PW4152  
Thrust: 231 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: Pratt & Whitney  
Model/Submodel: JT9D7R4E  
Thrust: 222 kN  

MAINTENANCE PROVIDERS

Air Transat
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S7 Airlines
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