KAI-1 Z.I.Itskovich

General Information
Type KAI-1
Function Passenger Trainer
Year 1934
Crew 1 3
Powerplant (2)
Type M-11
Power 100hp
Size
Length 7.9m
Wingspan 12.6m
Wing area (m2) 22.3 20.6
Weights and loads (kg)
Empty 780 855
Loaded 1310 1395
Wing Load (kg/m2) 58.7 67.7
Power load (kg/hp) 6.55 7.0
Speed
Maximum 218km/h
Cruising 190km/h
Landing 70km/h
Maneuverability
Turn time 20sec
Roll
Landing ?m
Takeoff ?m
Range
Practical 1000km
Flight Endurance 5h
Ceiling (m)
Practical 4800 ?
Climb (min)
1000m 3.5 3.5
2000m 7.2 -
3000m 12.5 16.0
Payload
Fuel 200kg
Cargo ?kg n/a
Seats 3 n/a
Drawing from "History of aircraft construction in the USSR", Vol.1 p.588

Low wing 2-engine passenger monoplane with fixed landing gear. Aircraft was designed to serve on short local airlines, but unusual location of one passenger (in the special nose cabin) exposed the fact that designers had in mind certain military applications as well.

KAI-1 was of wooden construction, fuselage - monocoque of elliptical cross-section. Skin - plywood 1.5 to 2.5mm. Wing of the first KAI-1 carried floating ailerons installed above the trailing edge. One of the first Soviet aircraft to be equipped with TsAP landing flap.

M-11 engines carried Taunend rings on the first aircraft. The second KAI-1 built was presented as a trainer-bomber. It differed by conventional ailerons, Taunend ring replaced by individual fairings on the engine cylinders.

Both civil and military variants were successfully tested at Kazan by pilot B.N.Kudrin and recommended for series production.

PredecessorsModifications
-
UPB
KAI-1 N°3
References
  • "History of aircraft construction in the USSR", Vol.1 p.558-559
  • "Самолет", 1935, 3, с. 25 (указан соавтор Б. Н. Езеров); 9, с. 15.
  • "Техника воздушного флота", 1935, 2, с. 56—62.
  • Links
  • Chapter from "History of aircraft construction in the USSR"
  • KAI website
  • KAI-1

  • Created September 9, 2001 Back to
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