There are 27 images added between 18 February 2007 and 22 May 2015
1  2  3  4  
Ka-226  
Initial Operational Capability (IOC): 2003
Total Production: 269
Also Known As: Hoodlum, Ka-226A, Ka-226T and Ka-226TG
Origin: Russia
Corporations: Kamov and Kumertau Aviation Production Enterprise
Parent System: Ka-226
Initial Operational Capability (IOC):
Total Production: 269
Reviews
There are no reviews so far

Description: The Kamov Ka-226 is a small, twin-engine, light utility helicopter provided with a dismountable mission-specific module located behind the cockpit. The mission-specific module permits Ka-226 to meet a wide range of roles such as search and rescue, emergency medical evacuation, gas/oil-field servicing, cargo and passenger transport, flying crane, fire-fighting, police and training helicopter. Ka-226 is based on the Ka-26 helicopter also from Kamov. The aircraft has been certified by Russian aviation authorities and is compliant with FAR A and B standards. The Ka-226 can be powered alternatively by either Allison 250-C20B or Turbomeca Arrius 2G turboshaft engines.

In addition to the central compartment module, Ka-226 features Kamov's two coaxial rotors with a diameter of approx. 13-meter each, modular design and a modern avionics package including western avionics for export models. The lack of tail rotor provides the Ka-226 with outstanding maneuverability in enclosed environments and in turbulent atmosphere. Kamov is currently developing several variant equipped with medical equipment, gun pods, imaging systems, loudspeaker pods, etc. to meet the requirements of Russian and foreign customers.

Ka-226 Specifications

Crew: 1
Main Rotor Blades: 6
Number of Engines: 2
Passengers: 9
Dimensions
Cargo Compartment Height: 1.40 meter
Cargo Compartment Length: 2.35 meter
Cargo Compartment Width: 1.54 meter
Main Rotor Diameter: 13 meter (512 inch)
Performance
Ceiling: 6,200 meter (20,341 foot)
Hovering Ceiling: 2,500 meter (8,202 foot)
Max Range: 600 kilometer (324 nautical mile)
Speed
Cruise Speed: 195 kph (105 KTAS)
Top Speed at High Altitude: 205 kph (111 KTAS)
Weight
Max Takeoff Weight: 3,400 kilogram (7,496 pound)
Payload: 1,400 kilogram (3,086 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Ka-226 News

There are 16 news between
11 Aug 2011 and 19 Jun 2017
1  2  
Monday, June 19, 2017Joint Venture for the Production of Ka-226T Helicopters is Registered in India
Wednesday, May 3, 2017India, Russia Set Up Joint Venture to Make Kamov Ka-226 Multi-Role Helicopters
Friday, April 28, 2017Russia, India Agree on Production of 200 Ka-226 Helicopters
Saturday, February 18, 2017Indian Air Force Upgraded Super Sukhoi Multirole Fighters to Get Al-41F1S Engines
Saturday, October 15, 2016India Signs Agreement with Russia on Deliveries of S-400 Air Defense Systems
Russia and India Sign Agreement to Jointly Produce Ka-226T Light Helicopters
Monday, July 20, 2015Indian Armed Forces to Buy 200 Ka-226 Helicopters
Thursday, May 21, 2015Russian Helicopters' Ansat and Ka-226T Enter the Russian Commercial Market
Thursday, May 14, 2015India to Buy 200 Russian Kamov Ka-226T Helicopters
Monday, April 27, 2015Ka-226T Helicopter with KRET Avionics successfully Certified

Operators & Related Equipment


OperatorsItems
India200
India bought 200 Ka-226T helicopters in July 2015 to be manufactured locally
Kazakhstan1
Aircraft ordered by Almaty Rescue Service (1)
Russia68
Russian Navy plans call for the procurment of 20 Ka-226 search and rescue helicopters. Russian Air Force ordered 30 Ka-226 trainers in May 2011. NefteGazAeroCosmos ordered 18 Ka-226TG in September 2012.
YearHoldings
202050Russian Air Force (30) and Navy (20)
201410Russian Air Force

Grand Total 2694
Propulsion Systems
AI-450x2
Arrius 2G1x2
Model 250-C20Bx2
Copyright © 2003-2017 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.