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Initial Operational Capability (IOC):
Also Known As: Aktay
Parent System: Aktai
Initial Operational Capability (IOC): 2009
Total Production: ?
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Description: The Kazan Helicopters Aktai is a light, single-engine, three-seat multi-purpose helicopter developed to suit a wide spectrum of duties in the commercial range. A single VAZ-3265 piston engine rated at 270-hp at takeoff drives a three-bladed main rotor allowing the aircraft to achieve a maximum airspeed of 190 kph. The cabin flexibility allows to accommodate up to four passengers including the pilot, one pilot and two passengers or one pilot and up to 300 kg of cargo in the rear compartment.
The Aktai design focuses on simplicity and low operating costs. Currently, Aktai is undergoing flight tests with the first helicopter rolling off the production line at Kazan Helicopters planned for 2009.
Main Rotor Blades: 3
Number of Engines: 1
Cabin Height: 1.32 meter (52 inch)
Cargo Compartment Length: 1.20 meter
Cargo Compartment Width: 1 meter
Ceiling: 4,700 meter (15,420 foot)
Hovering Ceiling: 1,300 meter (4,265 foot)
Max Range: 400 kilometer (216 nautical mile)
Max Power at TakeOff: 270 hp (201 kW)
Cruise Speed: 155 kph (84 KTAS)
Top Speed at High Altitude: 190 kph (103 KTAS)
Cargo Hook Capacity: 240 kilogram (529 pound)
Max Takeoff Weight: 1,150 kilogram (2,535 pound)
Payload: 300 kilogram (661 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)
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on 14 Sep 2010
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