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MAGNI M-22 VOYAGER - TECHNICAL SPEFIFICATIONS:

Length x width x height 4,7 m x 1,8 m x 2,7 m
Rotor diameter 8.23 or 8.54 m
Cruising speed 145 km/h
Maximum speed 185 km/h
Rate of climb 5 m/s
Max takeoff weight 450 kg
Empty weight 280 kg
Engine Rotax 912 ULS (100 hp) or Rotax 914 UL2 (Turbo with 115 hp)


SERIAL EQUIPMENT AUTOGYRO MAGNI M-22 VOYAGER:

- Open 2-seat factory built gyroplane
- AIRFRAME: Chrome-alloy aeronautical 4130 steel, tig welded. Fiberglass fuselage, wheels and rudder pedals
- SEAT With integral 80 litre fuel tank manufactured in epoxy resin reinforced with fiberglass
- INSTRUMENTS: Rotor rev counter, altimeter, air-speed indicator, Flydat and fuel level and pressure gauge
- ENGINE: Turbo Rotax 914 (115 HP), 4 cylinders, 4-stroke, water-cooled, with electric starter and mechanical pre-rotator
- PROPELLER: Three-bladed propeller, carbon fibre with ground adjustable pitch
- ROTOR: Two-bladed, composite materials manufactured by Magni Gyro, 27-28 ft diameter
- CONTROLS: Single
- ELECTRIC TRIM

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