Design and development
The M-14 features a single main rotor, a two-seats-in a tandem open cockpit with a windshield, tricycle landing gear with wheel pants and a four-cylinder, air and liquid-cooled, four-stroke, dual-ignition Rotax 912S engine in pusher configuration. The turbocharged Rotax 914 powerplant is optional. The aircraft fuselage is made from TIG-welded 4130 steel tubing, while the cockpit fairing is fibreglass. Its diameter composite rotor has a chord of and is manufactured in house by Magni Gyro. The propeller is a three-bladed carbon fibre, ground adjustable type. Electric trim is standard equipment, as is a Flydat digital engine monitor. The second seat is located right behind the pilot's seat without a separate cockpit, dual controls or windshield and is intended for occasional use to carry a passenger. The pilot's seat includes an integral fuel tank that provides three hours endurance. The aircraft has an empty weight of and a gross weight of , giving a useful load of .Specifications (M-14 Scout)
References
External links
* {{Portal bar, Italy, Companies, Aviation 2000s Italian sport aircraft Single-engined pusher autogyros Magni aircraft