The Mi-2 helicopter is an all metal structure, with a single main rotor and tail design. Powered by two GTD-350 turbo-shaft engines with a combined 800 shp.

This helicopter is generally found an Agricultural and Medavac services. Other options for civilian and military configurations are available.

General characteristics
Crew: One
Capacity: 8 passengers or 700 kg (1,540 lb) internal, 800 kg (1,760 lb) external cargo
Length: 11.9 m (39 ft 4 in)
Rotor diameter: 14.6 m (47 ft 11 in)
Height: 3.7 m (12 ft 2 in)
Empty weight: 2,372 kg (5,218 lb)
Loaded weight: 3,550 kg (7,810 lb)
Max takeoff weight: 3,700 kg (8,140 lb)
Powerplant: 2 Ea. PZL GTD-350 Turbo-shafts, 298 kW (400shp) each

Performance
Maximum speed: 220 km/h (138 mph)
Range: 340 km (212 mi)
Service ceiling: 4,000 m (13,120 ft)
Rate of climb: 4.5 m/s (886 ft/min)
Disc loading: 21 kg/met (4.3 lb/ft)
Power/mass: 170 W/kg (0.10 hp/lb)

There are numerous avionics, configuration, engine modification and upgrade packages available.

Contact us for further information concerning sales and parts assistance.

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