Technical data
Type IT-6
Function Trainer
Year 1929
Crew 2
Engines 1*60hp Cirrus
Length 6.7m
Wingspan 10.6m
Wing area 16.0m2
Empty weight 430kg
Loaded weight 650kg
Wing Load (kg/m2) 40.6
Power load (kg/hp) 10.9
Speed at 0m 160km/h
Fuel+Oil 60kg

IT-6 by I.P.Tolstyh

20k b/w "History of aircraft construction in the USSR", Vol.1 p.425

Parasol trainer with 60hp 'Cirrus' engine. Plywood skin of the aircraft wing and fuselage provided very clean airdynamic for penalty of minor overweight. Series of successful flights were performed in 1929- 1930, but complete trials never took place.

  • "Samoliot" 2, 1930, p18;
  • "Samoliot" 5, 1930, p9;
  • "History of aircraft construction in the USSR", Vol.1 p.424;
  • None

  • Created February 19, 1999 Back to
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