Engineering:Technoavia SM-94
| SM-94 | |
|---|---|
| |
| Technoavia SM-2000P | |
| Role | General aviation aircraft |
| Manufacturer | Technoavia |
| Number built | limited number of prototypes |
| Developed from | Yakovlev Yak-18T |
The Technoavia SM-94 series was developed in the early 1990s as a six-seat version of the Yakovlev Yak-18T, incorporating upgraded, modern avionics and aerodynamic refinements.
Design and development
The main changes in the Technoavia SM-94 series, besides the increase in fuselage capacity, were including all-metal wings and empennage with all surfaces re-profiled to give a squarer appearance, a three-blade propeller, increased tankage and two-piece windscreen replacing the original multipane design.
Operational history
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In 1997, the SM94-1 development aircraft (RA-44486) was shown at MAKS, Moscow, but series production was subsequently halted by financial concerns.
The Technoavia SM-94 was further developed into the SM-2000 series. The prototype SM-2000P made first flight 21 March 2002 and was displayed at MAKS '03.
Designation SM-2000P differentiates it from the further developed SM-2000 turboprop, that became a separate variant. Since 2006, no further developments have been announced.
Specifications (SM-94)
Data from [1]
General characteristics
- Length: 8.35 m (27 ft 5 in)
- Wingspan: 11.6 m (38 ft 1 in)
- Empty weight: 1,100 kg (2,425 lb)
- Max takeoff weight: 1,870 kg (4,123 lb)
Performance
- Maximum speed: 300 km/h (190 mph, 160 kn)
- Range: 1,350 km (840 mi, 730 nmi)
- Service ceiling: 5,500 m (18,000 ft)
References
- Notes
- ↑ "Technoavia SM-94". http://ruslet.webnode.cz/technika/ruska-technika/letecka-technika/technoavia/sm-94/. Retrieved 16 September 2015.
- Bibliography
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