|Magni M 19 Shark|
TYPE: Two-seat autogyro ultralight.
PROGRAMME: Three built for trials by 2002. However, not placed in production and development and marketing effort switched to M 21.
STRUCTURE: Generally as for M 20 Talon.
LANDING GEAR: Fixed tricycle type.
POWER PLANT: One turbocharged 84.6kW Rotax 914 UL flat-four with electric starter, driving a ground-adjustable pitch, three-blade, carbon fibre pusher propeller. Fuel in integral cockpit seat/tank of epoxy/glass fibre, capacity 74 litres.
Jane's All the World's Aircraft, 2004-2005
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Technical data for Magni M 19 Shark
Rotor diameter: 8.23m, overall length: 4.80m, overall width: 1.85m, overall height: 2.60m, propeller diameter: 1.70m, weight empty: 280kg, max take-off weight: 550kg, max level speed: 185km/h, cruising speed: 145km/h, rate of climb at sea level: 300m/min, service ceiling: 3500m, take-off run: 90m, landing run: up to 30m, range, no reserves: 481km, endurance: 4h 30min