Back Magni M 19 Shark
2002

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.

DESIGN FEATURES: Generally ās for M 20 Talon. M 16 Tandem Trainer can be upgraded to M 19 standard.

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

*     *     *

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

Comments 
shoes, e-mail, 19.09.2011

I am from IRAN.
Is there a plans available , how much?

polo, e-mail, 16.06.2011

Fuel in integral cockpit seat/tank of epoxy/glass fibre,

FARDIN, e-mail, 23.07.2007

I am from IRAN.
Is there a plans available , how much?
my email is engfardin@yahoo.com
tanks.
FARDIN

Do you have any comments concerning this aircraft ?

Name   E-mail


All the World's Rotorcraft


Virtual Aircraft Museum


Back AVIATION TOP 100 - www.avitop.com Avitop.com