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Dyn'Aero MCR R180




The design of the MCR R180 incorporates a carbon fuselage derived from the MCR 4S (four-seater with more than 130 sold), a Lycoming O-360 of 180 hp, and a canopy offering a visibility on 180°. Options include a roller of tow cable and a ballistic parachute.

The MCR R180 is certificated for kits under CNSK 2 category allowing kits.

Engine: Lycoming O-360, 180 hp
Propeller: Sensenich or 4-blade Hoffman
Max propeller diameter: 1.94m
Wing span; 8.72 m
Wing area; 8.31 sq.m
Length; 9.2 m
Cabin width; 1.20 m
Fuel capacity; 2 x 65 lt
Empty weight initial version; 450 kg
Equipped weight; 750 kg
MTOW aerotowing; 600 kg
Wing loading aerotowing; 72 kg/sq.m
Stall @ MAUW; 83 km/h
Stall 600 kg; 74 km/h
Manoeuvring speed (Va); 219 km/h
Never exceed (Vne); 270 km/h
Turbulent air max (Vno); 243 km/h
Load factors; +3.8/-1.5 g
Flap extension (Vfe); 160 km/h
Best towing speed; 90 - 150 km/h
ROC w/tow 350 kg: 7.27 m/s
ROC w/tow 550 kg: 5.73 m/s
ROC w/tow 750 kg: 4.67 m/s


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