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Technical data of the MT-03
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Short technical description
The MT-03 is a two-seat tandem autogyro with dual controls. The airframe and ancillaries are made from high-grade stainless steel. The certified Rotax 912 ULS 100 HP engine is equipped with a 1:2.43 reduction gearbox, slipper clutch as standard and a High-grade stainless steel exhaust system. Cockpit, seats, landing gear, propeller and tail unit are fabricated from composite materials. There is no additional weight due to the hydraulic main wheel disc brakes with parking brake. The pneumatic trim and rotor brake are getting air supplied by a compressor. Plastic fuel tank with integrated drain catches 34 litres of fuel. The Air Copter aluminium rotor system complies with the stringent 8H12 NACA aerofoil standards. Alternatively to the classic mechanic pre-rotator a comfortable pneumatic pre-rotator is offered.
Technical data
- Rotax engine 100 PS
- Empty weight 239 kg
- Max. take-off weight 450 kg
- Payload 211 kg
- VNE 163 km/h
- Cruise Speed 130 km/h
- V/min 30 km/h
- Rate of climb 5 m/s
- Take-off distance 10-70 m
- Landing distance 0-15 m
- Fuel capacity 68 l
- Range appr. 400 km
Instruments
- Airspeed indicator
- Altimeter
- Compass
- Engine rpm
- Rotor rpm
- Oil temperature
- Oil pressure
- Oil pressure warning
- Air intake temperature
- Cylinder head temperature
- Trim position indicator
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