IL-76 Technical specification
- Maximum take-off weight: 195 tons
- Maximum load: 50 tons
- Flying range by maximum load: 4 000 km
- Cargo cabin size: 3,4 х 3,45 х 20 meters
Aircraft specifications and loading equipment:
| Il-76TD-90VD | |
|---|---|
| ENGINE TYPE | 4x PS-90A-76 |
| ENGINE TAKE-OFF THRUST | 4x 16,000 kg f Σ= 64,000 |
| MAXIMUM TAKE-OFF WEIGHT | 195,000 kg |
| OPERATING EMPTY WEIGHT | 97, 243 kg |
| MAXIMUM PAYLOAD INCL.LOADING EQUIPMENT | 50,000 kg |
| MAXIMUM LANDING WEIGHT | 155,000 kg |
| MAXIMUM ZERO FUEL WEIGHT | 144,800 kg |
| CRUISING SPEED | 750 km/h |
| FLIGHT LEVEL (TYPICAL) | 9,100 m – 10,600 m |
| RANGE | 4 500 km |
| CAPABILITY OF ONBOARD CRANE SYSTEM | 12,000 kg |
| ENGINEERING CREW | 4 crew members |
| FLIGHT CREW | 4 crew members |
LOADING EQUIPMENT
- Internal Crane System – The onboard system of overhead cranes consists of 4 electric hoists with 3-tonne lifting capacity each, they are capable of lifting single items of up to 12,000kgs
- The freighter is equipped with 2 onboard electric winches of 3-tonne hauling capacity each
- Loading of wheeled vehicles, trailers and tracked vehicles
- Ramp enables wheeled vehicles to be loaded using their own power
- Extension ramp can be applied for the loading of long and high vehicles
- Loading of heavy and outsize cargo
- Use of special Volga-Dnepr Airlines‘ loading equipment for loading of heavy and outsize cargo subject to usage of mobile crane(s) and additional trailers
