page_title: Kamov Ka-126
section_title: Variants
hierarchical_section_title: Kamov Ka-126 / Variants
caption_attribution_description: Kamov Ka-226T
context_page_description: The Kamov Ka-126 is a Soviet light utility helicopter with co-axial rotors.
  Evolved from Ka-26 with engine pods removed from stub wings, fitted with one TVO-100 turboshaft engine positioned on top of fuselage, modified rotor blades, new fuel system.
context_section_description: Ka-126 Hoodlum-B
  One or two crew utility light helicopter, powered by a 720-shp (537-kW) (Glushenkov) OMKB TVD-100 turboshaft engines. First flown in 1986, and built under licence by IAR in Romania. 2 prototypes and 15 series helicopter built.
  Ka-128
  One prototype, powered by a 722-shp (538-kW) Turbomeca Arriel 1D1 turboshaft engine.
  Kamov Ka-226
  Powered by two 450-shp (335-kW) Rolls-Royce 250-C20R/2 turboshaft engines.
caption: Kamov Ka-226
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