Technical data
Type AIR-6
Function Prototype Passenger Ambulance
Year 1932 1933
Crew 1
Engines 1*100hp M-11
Length 8.0m
Wingspan 12.0m
Wing area 19.8m2
Empty weight 584kg 610kg 620kg
Loaded weight 843kg 900kg 1000kg
Wing Load (kg/m2) 42.0 47.3 50.5
Power load (kg/hp) 8.5 9.0 10.0
Speed at 0m 166km/h 162km/h 156km/h
Landing Speed 65km/h 68km/h 68km/h
Landing Roll 120m
13sec
120m
13sec
165m
15sec
Takeoff Roll 70m
7sec
90m
9sec
85m
8sec
Turn time 16sec 16sec 17sec
Range 650km
Flight Endurance 5h
Ceiling 4500m 4000m 3000m
Climb
1000m 6.9min 6.6min -
3000m 30min 29.3min -
Payload
Seats 2 to 3

AIR-6, Ya-6 by A.S.Yakovlev

AIR-5 52k drawing from "History of aircraft construction in the USSR", Vol.1 p.478;
Colors by Alexandre Savine

AIR-5 adaptation for domestic M-11 engine. It was ready in May 1932, flew on September 8 and passed all trials easily. Adopted as short range liaison aircraft.

In 1934 group of AIR-6 performed flight Moscow-Irkutsk-Moscow (with refuel landings), covering more than 10,000km.

During 1934-36 total 486 AIR-6 were built. Twenty of them were modified as ambulance with room for a stretcher and doctor.

PredecessorsModifications

AIR-5

AIR-6A
References
  • "History of aircraft construction in the USSR", Vol.1 p.478-479;
  • Links
  • AIR-6
  • Ya-6 (AIR-6) at Virtual Aircraft Museum

  • Modified February 9, 1998 Back to
    Main Gate