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JSC Kamov Design 
Ka-226 Sergei 




A Ka-226 of the Police of Russia
General information
Type Light utility
National origin Russia
Manufacturer Kamov
Status Active
Primary user Russian Aerospace Forces
Syrian Arab Air Force
Number built 269 
History
Manufactured 1996 - Present
Introduction date 2002
First flight 4 September 1997
Developed from Kamov Ka-126
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History JSC Kamov Design Bureau
Kamov Ka-226 Sergei (NATO reporting name: Hoodlum)
  • Design

    The design is a refinement of the proven Ka-26, featuring interchangeable mission pods. The aircraft is fitted with a new rotor system, increased visibility nose, and new passenger cabin design. The Ka-226 also features a new transmission system and is made largely from composite materials.

    The aircraft is fitted with trademark Kamov coaxial rotors, of advanced composite design, making the Ka-226 highly manoeuvrable and eliminating the need for a tail rotor.

    Variants

    The Kamov Ka-226 is available in the following variants; Search and Rescue, medevac, disaster relief and patrol variants have been developed for the Russian Emergency Ministry. Air ambulance, police and fire fighting variants have been developed for the Russian government.

    Ka-226T
    Instead of Rolls-Royce 250C engines, this variant is fitted with the more powerful Turbomeca Arrius 2G1. Each engine provides 670 shp, increasing the service ceiling to around 7,000 m, providing improved high altitude and high temperature operation. Helicopter has new avionics with multifunctional displays, automatic control system, navigation system, radar. It can be equipped with hoist system, helicopter sling, searchlight, additional external fuel tank. For search and rescue missions helicopter can be equipped with medical module.
    Ka-226TG
    Gazprom specific variant based on Ka-226T model.
    • A Russian Aerospace Forces Ka-226
    • Kamov Ka-226T at the MAKS 2009 International Aviation and Space Salon
    • Gazprom Ka-226TG

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JSC Kamov Design Bureau Kamov Ka-226 (NATO reporting name: Hoodlum)

JSC Kamov Design Bureau
Kamov Ka-226 Sergei (NATO reporting name: Hoodlum)

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General characteristics

  • Crew: 1-2
  • Capacity:
    • Passengers: 7
    • Cargo: 1,050 kg internally, or 1,100 kg on an external sling
  • Length: 8.1 m (25 ft 7 in)
  • Height: 4.15 m (13 ft 7 in)
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Powerplant

  • Powerplant: 2 × Turbomeca Arrius 2G1 , 435 kW (580 hp) each
  • Main rotor diameter: 2 × 13 m
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Specifications

  • Maximum speed: 250 km/h 
  • Cruise speed: 220 km/h 
  • Range: 600 km (373 mi, 324 nmi)
  • Service ceiling: 6,200 m (20,300 ft)
  • Hover ceiling: (4600 m, 15,000 ft)
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Armament

Special Links JSC Kamov Design Bureau Ka-226 Sergei. NATO reporting name 'Hoodlum'

Links to Youtube & Others

Kamov announced the development of the Ka-226 Sergei light multipurpose helicopter in 1990. The helicopter was developed to meet the requirements of the TSENTROSPAS Russian Emergency Ministry, the Moscow City Government and Gazpromavia Airlines. The Ka-226 underwent its maiden flight in September 1997.

Kamov Design Bureau Kamov Ka-226 Sergei

In November 2007, Kamov secured a $25m contract from the Royal Jordan Air Force for six Ka-226 light utility helicopters.

interior

Youtube Link

The cabin is lightly pressurised, with ventilation and warm air heating.

interior
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