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Technical Data

 

MODELS

K209M – retractable gear

K209MF – skids

Category & type of aircraftRotorcraft Helicopter
Kit manufacturerFamà Helicopters s.r.l. / Italy
SeatsPilot + 1

ROTOR SYSTEMS

Main rotor & anti-torque rotorSemi-rigid (2 blade carbon)
Drive system3 fold double V-belt

POWER PLANT

ModelFamà turboshaft gas turbine
Power rating162 HP (120 kW) at 60,000 RPM
Engine-ManagementFADEC

UNDERCARRIAGE

SystemElectro-hydraulic retractable landing gearskids

FUEL

Tank capacity145 litres or 116 kg (38 USG or 256 lbs)
Type of fuelJet A-1
Consumption at 65% PWR40 litres/h or 32 kg/h (11 USG or 70 lbs)
RangeMaximum 300 NM (555 km) (no reserve)

SPEEDS

Cruise speed100 kts (185 km/h)90 kts (185 km/h)
Never exceed speed (VNE)116 kts (215 km/h)
Maximum rate of climb2,165 ft/min. (11 m/sek.)

HEIGHT LIMITATIONS

Hover ceiling in ground effect (IGE)10,000 ft (3,000 m)
Hover ceiling out of ground effect (OGE)8,000 ft (2,400 m)
Service ceiling12,500 ft (3,800 m)

WEIGHTS

Empty weightNormal-/experimental category: 340 kg (750 lbs)Normal-/experimental category: 310 kg (683 lbs)
Maximum take-off weight700 kg (1,543 lbs)

DIMENSIONS

Cockpit Inner width1,250 mm (49.21 inch)
Cockpit Inner height1,280 mm (50.39 inch)
Baggage compartment980 x 530 x 300 mm (38.58 x 20.86 x 11.81 inch)

For assembly support, please contact our customer service. Technical specifications and price changes without notice.

Date of issue: September 1, 2012

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