Yakovlev Yak-112
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| Yak-112 | |
|---|---|
| Yak-112 prototype at Zhukovski, 1997 | |
| Role | Trainer / Gider tug |
| National origin | USSR |
| Manufacturer | Yakovlev |
| Designer | Vladimir Mitkin |
| First flight | 20 October 1992 |
The Yakovlev Yak-112 is a Russian/Soviet civil utility aircraft that first flew in early 1990s. It is ready for serial production as of 2008 (50..70 "firm" orders awaited to begin). It is an all-metal high-wing braced monoplane with a non-retractable tricycle landing gear and a heavily glazed[disambiguation needed 
] cabin.
[edit] Specifications (Yak-112)
Data from The Osprey Encyclopaedia of Russian Aircraft 1875 – 1995[1]
General characteristics
- Crew: 1
- Capacity: 2 PAX
- Length: 6.96 m (22 ft 10 in)
- Wingspan: 10.25 m (33 ft 8 in)
- Height: 2.9 m (9 ft 6 in)
- Wing area: 16.96 m2 (182.6 sq ft)
- Empty weight: 950 kg (2,094 lb)
- Gross weight: 1,300 kg (2,866 lb)
- Max takeoff weight: 1,520 kg (3,351 lb)
- Powerplant: 1 × Lycoming IO-540 6-cyl. horizontally opposed air-cooled piston engine, 191 kW (256 hp) or Continental IO-550
- Propellers: 3-bladed Hartzell
Performance
- Maximum speed: 230 km/h (140 mph; 120 kn)
- Cruising speed: 193 km/h (120 mph; 104 kn)
- Range: 1,000 km (621 mi; 540 nmi)
- Service ceiling: 4,000 m (13,123 ft)
[edit] References
- ^ Gunston, Bill (1995). The Osprey Encyclopaedia of Russian Aircraft 1875 – 1995. London: Osprey. pp. 497. ISBN 1 85532 405 9.
- Gunston, Bill (1995). The Osprey Encyclopaedia of Russian Aircraft 1875 – 1995. London: Osprey. pp. 497. ISBN 1 85532 405 9.
[edit] External links
The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.
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