General Information
Type S-202
Function Light hydroplane
Year 1995
Crew 1+1
Powerplant (2)
Type RMZ-640 Rotax 503-1 V
Power 30hp 45hp
Size (m)
Length 7.0
Wingspan 12.0
Wing area ?m2
Weights (kg) and loads
Empty 330 330
Takeoff 550 580
Wing Load (kg/m2) ?
Power load (kg/hp) 9.17 6.44
Speed (km/h)
Maximum 135 160
Cruising 110 130
Landing 60 60
Takeoff (m)
Water 250 150
Land 150 100
Range (km)
Maximum 450 600
Maneuverability
g-Load +4.5 -2.25
Other
Airframe resource 3000h

D.Suslakov (OKB LA)


S-202
S-202 in flight, OKB LA

Light 2-seater hydroplane, designed and tested at Experimental Design Bureau of Flying Vehicles of the Samara Aerospace University (former KuAI). From the very beginning project was developed in compliance with the International Airworthiness Standards for light aircraft.


S-202
S-202 on land, OKB LA

If necessary, wheel or ski landing gear may be installed. Possible applications are:

Picture used for the background, found at the OKB LA site
PredecessorsModifications
- S-302
References
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  • Links
  • S-202
  • S-202
  • S-202

  • Created February 22, 2002 Back to
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