Commercial Aircraft Directory - Aircraft Specification

Ilyushin - Il-76

The Il-76 was developed as a jet transport for the Soviet air force, capable of delivering cargo, troops or vehicles to austere airfields with short runways, and capable of operating in extreme conditions. To enable this, the Il-76 has relatively powerful engines, extensive high lift devices, a high flotation landing gear, APU and comprehensive cargo handling equipment. In addition the Il-76 can self refuel/defuel. For civilian operators involved in such tasks as mineral exploitation and infrastructure development in isolated locations; such attributes and capabilities are valuable and as such Aeroflot received one hundred and fifty aircraft. Civilian versions of the IL-76 are the 76T and 76TD; the 76T featuring additional fuel tankage in the wing centre section. The 76TD in addition features uprated Soloviev D-30KP-1 engines which give improved performance in ‘hot and high’ take offs. Civilian Il-76s do not feature the rear gun position of military variants although ex military aircraft are seen in civilian service and vice versa. A total of fifty four Il-76Ts have been built delivery taking place between July 1972 and January 1990. During the period February 1978 to April 2005 one hundred and ninety five IL-76TDs were delivered mainly to Aeroflot. Including military versions; eight hundred and ninety nine IL-76s have been delivered to operators In August 1995 the first IL-76MF a stretched military version with PS-90AN engines rated at 156.9 kn flew; the aircraft has been stretched by two plugs fore and aft of the wings increasing length to 53.19m. Range with a 40.000 kg payload is 5200km and operating economics are said to be improved by 30% in comparison with the IL-76TD.Hold volume is increased to 400m³ The civil version of this aircraft is designated IL-76TF . A PS-90 powered version of the standard airframe the IL-76-90VD flew in September 2005.

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: 25 Mar 1971  
Certification date:  

PRINCIPAL DIMENSIONS

Fuselage width: 4.8 m 
Fuselage height: 50.5 m 
Fuselage length: 46.5 m 
Cabin length: 24.5 m 
Cabin width: 3.4 m 
Cabin height: 3.46 m 
Cabin volume: 235 m3 
Hold volume:  

WEIGHTS

Empty operating: 89,000 kg 
Max zero fuel: 136,000 kg 
MTOW: 170,000 kg 
MLW: 155,000 kg 
Standard fuel capacity: 81,830 kg 
Max fuel capacity: 81,830 kg 

SPEEDS

Normal cruise: 750 km/h 
Max cruise: 850 km/h 

PERFORMANCE

Long Range Cruise alt: 11,887 m 
Max ceiling: 13,716 m 
Take off field length: 1,700 m 
Landing field length: 900 m 
Max Payload Range: 2,986 m 
Range notes: Data refers to IL-76T  
Max passengers: 90  
Typical passengers: 0  

POWERPLANT

Category: Turbofan  
Manufacturer: Aviadvigatel / NPO Saturn  
Model/Submodel: D-30 KU 1 series  
Thrust: 108 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: Aviadvigatel / NPO Saturn  
Model/Submodel: D-30 KU 1 series  
Thrust: 108 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: NPO Saturn  
Model/Submodel: D-30 KP 3 Burlak  
Thrust: 127 kN  

MAINTENANCE PROVIDERS

Aircraft Maintenance Base Domodedovo (AMB)
Aviation Technical Centre
Volga-Dnepr Gulf (Sharjah, UAE)