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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