Kamov Ka-26 Hoodlum

Origin: Soviet Union / Russia
Prototype: maiden flight August 18, 1965
History:
  • produced since 1969
  • NATO reporting name : „Hoodlum“
  • transport, assault transport,
Crew: – two pilots
Powerplant: 2 x Vedenejev M-14 V-26 radial piston engines,   á 235 hj
Performance:
  • capacity: 6 passangers or 900-1100 kg
  • max speed 170 km/h
  • range 400 km/h
  • service ceiling 3,000 m
Weight: empty weight 1,97 t, max takeoff weight 3,25 t
Dimensions: length 7,75 m, rotor diameter 2 x 13 m, height 4,05 m; disc area 265 m2
Versions: number built 816
Operators: Russia + 6 other states

https://en.wikipedia.org/wiki/Kamov_Ka-26