Technoavia SM-94

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.

SM-94
Technoavia SM-2000P
Role General aviation aircraft
Manufacturer Technoavia
Number built limited number of prototypes
Developed from Yakovlev Yak-18T

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
Technoavia SM-94

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
Wikimedia Commons has media related to Tehnoavia SM-94.
Notes
  1. "Technoavia SM-94". ruslet.webnode.cz. Retrieved 16 September 2015.
Bibliography
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