More about Ansat helicopters


Ansat — light multipurpose helicopter developed by the design Bureau of JSC “Kazan helicopter plant”. The first prototype of the helicopter was assembled in April 2004. The Ansat helicopter can carry 1300 pounds of payload in the cabin.

Ansat is translated from the Tatar language means “simple”, “simple”.

Lead designer of the program “Ansat” for fifteen years, from 1993 to 2007, was Valeriy V. Dvoeglazov. At Kazan helicopter plant he came with KNPP “Helicopters “Mi” in 1993. At this time, LSC has begun work on “Anatom”. A young professional who wanted students to develop a new light helicopter, hit, as they say, at the right place at the right time.

General characteristics

Crew: 1 or 2
Capacity: 9 or 10 passengers or 2 stretchers and 3 attendants
Length: 13.76 m (45 ft 2 in)
Height: 3.40 m (11 ft 2 in)
Empty weight: 1,900 kg (4,189 lb)
Gross weight: 3,000 kg (6,614 lb)
Max takeoff weight: 3,300 kg (7,275 lb)
Powerplant: 2 × Pratt & Whitney Canada PW207K turboshaft, 470 kW (630 hp) each
Main rotor diameter: 11.50 m (37 ft 9 in)
Main rotor area: 103.87 m2 (1,118.0 sq ft)


Maximum speed: 275 km/h (171 mph; 148 kn)
Cruising speed: 250 km/h (155 mph; 135 kn)
Never exceed speed: 285 km/h (177 mph; 154 kn)
Range: 540 km (336 mi; 292 nmi)
Endurance: 3 hr 20 min
Service ceiling: 4,500 m (14,764 ft)
Rate of climb: 21.5 m/s (4,230 ft/min)

The first helicopter was assembled in may 199. The first flight was made in 1999. In 2011 began the process of certification of civil helicopters. In August 2013 received the type certificate of Aviation register of Interstate aviation Committee. In 2013, 6 helicopters “Ansat-U” was transferred to the air force Academy for training cadets.

The helicopter’s spacious cargo-passenger cabin, which is being converted into different versions of the task use.

The machine can be used to resolve a wide scope of tasks: delivery of goods, passenger transport, patrolling, rescue and search operations, medical emergency, administrative, transportation, primary education.

A variation of the helicopter increased comfort (VIP) is available for the transportation of senior passengers.
The closest analogue abroad is a EC145 helicopter of the Airbus ‘Eurocopter’ group.

The Ansat is powered by two turboshaft engines PW 207K capacity of 630 HP Pratt & Whitney Canada c digital engine control system (FADEC), providing a continued takeoff with one engine failed.

Flight navigation system and on-Board equipment of the helicopter “Ansat” include on-Board information system, multi-function indicators and warning system about the failure.

In “Ansate” applied all-metal fuselage design, composite materials in non-force elements and fiberglass blades. The hingeless main rotor hub provides a high level of manageability and significant reduction in operating costs.

Trainer variant of the Ansat with the SIC-And has quadruple redundant fly-by-wire integrated digital control system.

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