MAGNUS FUSION 212
Two-seat light aircraft — localisation programme
A programme with Hungary’s Magnus Aircraft to set up large-assembly production in Kazakhstan.
- 600 kg
- MTOW
- 1,100 km
- range
- 240 km/h
- max speed
- +6 / −3 G
- load factor
The Fusion 212 is the flagship of Magnus Aircraft Corporation: a highly manoeuvrable two-seater in carbon composite, stressed to +6 / −3 G. With 800–1,100 km of range and a 120–130 m take-off run, it suits regional aviation and pilot training.
QAZDRON is an official partner of the company. Negotiations are under way on localising joint production of the Fusion 212 and Fusion 213 in the Republic of Kazakhstan, with large-assembly manufacturing as the core objective.
Applications
- Ab-initio pilot training
- Regional light aviation
- Patrol and monitoring
- Aero clubs and sport flying
Technical specifications
| Parameter | Value |
|---|---|
| Length | 6,620 mm |
| Wingspan | 8,440 mm |
| Cabin height | 1,170 mm |
| Seats | 2 |
| MTOW | 600 kg |
| Fuel | 90 L (AI-95 petrol) |
| Fuel consumption | 16–21 L/h |
| Landing speed | 80 km/h |
| Take-off run | 120–130 m |
| Landing roll | 150–200 m |
| Range | 800–1,100 km |
| Load factor | +6 / −3 G |
| Cruise speed | 200–210 km/h |
| Maximum speed | 240 km/h |
| Service ceiling | 3,650 m |
Gallery
MAGNUS FUSION 212
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