Ilyushin Il-112
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| Il-112 | |
|---|---|
| Type | light military transport |
| Manufacturer | Tashkent Aviation Production Association |
| Designed by | Ilyushin |
| Primary user | Russian Air Force |
The Ilyushin Il-112V is a light military transport aircraft developed by Ilyushin for air landing and airdrop of military cargoes, equipment and personnel. The IL-112V is equipped with the avionics combining the entire equipment complexes and systems into an integrated complex – the on board equipment integrated complex. The IL-112V can fulfill the assigned missions in any geographic and weather conditions, day and night, standard or adverse weather conditions.
[edit] Specifications
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.Data from ilyushin.org[1]
General characteristics
- Crew: 2
- Length: 23.14 m (75 ft 11 in)
- Wingspan: 25.74 m (84 ft 5 in)
- Height: 8.87 m (29 ft 1 in)
- Wing area: 300.0 m² ()
- Useful load: 6000 kg (13,000 lb)
- Max takeoff weight: 20,000 kg (44,000 lb)
- Powerplant: 2× Klimov TV7-117ST turboprops, 2800 hp (2100 kW) each
Performance
- Cruise speed: 550-580 km/h (340-260 mph)
- Range: 5000 km with 2 tonne load; 1000 km with max load (3100 mi with 2 ton load; 600 mi with max load)
- Service ceiling 9000 m (30,000 ft)
[edit] References
- ^ Light transport aircraft Il-112T. Official Ilyushin Il-112T page (in Russian).
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