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Fleet

Ilyushin IL-76TD

The IL-76 (Candid) was designed to meet a Soviet Air force requirement for a medium to long range jet transport aircraft, having ability to operate from short, unprepared runways and airports with undeveloped infrastructure. To achieve a large, easy to load/unload cargo compartment, the IL-76 was built as a high-wing monoplane with a T-tail and rear-loading ramp. The cargo area is fully pressurized and has a titanium floor, which can accept a large variety of self-loading wheeled or tracked vehicles. A mechanical handling system, which is rated at 10 metric ton, provides loading/offloading or palletized or containerized cargo/module. Currently IL76 is available for retrofitting with PS-90 engines to meet newly implemented noise and pollution limitations.

Wing span 165 ft 7 in 50.5 m

Length 152 ft 9 in 46.6 m

Height 48 ft 43 in 14.76 m

Empty weight 202 825 lb 92 000 kg

Max take-off weight 418 878 lb 190 000 kg

Max landing weight 334 000 lb 151 500 kg

Powerplant Solovyov D-30KP 4 x 12 000 ehp 4 x 11 770 kN

Structural payload 103 617 lb 47 000 kg

Structural volume 180 cub.m 180 cub.m

Min runway required 7 875 ft 2 400 m

Average cruise speed 405 knots 750 km/h

Fuel capacity (density 0.8) 110 000 L
194 007 lb
29 060 usg
88 000 kg

Average fuel consumption 2 972 usg/h 9 000 kg/h

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