Commercial Aircraft Directory - Aircraft Specification

Antonov - An-24

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: Apr 1960  
Certification date:  
Launch customer(s): Aeroflot-Russian Airlines
 

PRINCIPAL DIMENSIONS

Fuselage width: 2.9 m 
Fuselage height: 8.32 m 
Fuselage length: 23.53 m 
Cabin length: 9.69 m 
Cabin width: 2.76 m 
Cabin height: 1.91 m 
Cabin volume: 52 m3 
Hold volume:  

WEIGHTS

Empty operating: 13,300 kg 
Max zero fuel:  
MTOW: 21,000 kg 
MLW:  
Standard fuel capacity:  
Max fuel capacity:  

SPEEDS

Normal cruise:  
Max cruise: 452 km/h 

PERFORMANCE

Long Range Cruise alt:  
Max ceiling: 8,999 m 
Take off field length: 500 m 
Landing field length: 590 m 
Max Payload Range: 520 m 
Range notes:  
Max passengers: 50  
Typical passengers: 50  

POWERPLANT

Category: Turboprop  
Manufacturer: Motor Sich / Ivchenko Progress  
Model/Submodel: AI-24 T/VT  
Thrust: 0 kN  

POWERPLANT

Category: Turboprop  
Manufacturer: Motor Sich / Ivchenko Progress  
Model/Submodel: AI-244  
Thrust: 0 kN  

POWERPLANT

Category: Turboprop  
Manufacturer: Motor Sich / Ivchenko Progress  
Model/Submodel: AI-24 T/VT  
Thrust: 0 kN  

POWERPLANT

Category: Turboprop  
Manufacturer: Motor Sich / Ivchenko Progress  
Model/Submodel: AI-244  
Thrust: 0 kN  

MAINTENANCE PROVIDERS

Aircraft Maintenance Base Domodedovo (AMB)
Aviation Technical Centre
Joint Stock Company Rostov Civil Aviation Factory N 412
Kiev Aviaremont N410
Volga-Dnepr Gulf (Sharjah, UAE)