MCR M

MCR M EVOLUTION is derived from MCR ULC EVOLUTION. It is the same model but it is an aircraft and not an ultralight.

MCR M EVOLUTION existes in 2 versions.
The tricyle landing gear version and taildraggers. Both have a 544kg MTOW with a payload at 290kg.

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WIngspan 8.66 m

Lenght 5.53 m

Wing area 8.31 m²

Cabin width 1.12 m

Fast 2 seats

Economical

Large payload

Tricyle landing gear or Tricylelanding gearor taildragger

Caractéristiques | MCR M

MT Propeller electric or hydraulic variable pitch, two or three blades
MT Propeller fixed pitch two blades

Carbon fiber construction ensuring resistance, lightness and absence of corrosion
Heating and ventilation
Electric elevator trim and electric fin trim controlled from the stick

Oleo-pneumatic tricycle landing gear with wheel hull
Or taildraggerwith wheel hull
Hydraulic brakes: controlled by hand or toe-brakes

Cell parachute
Personalized avionics: GPS, radio, TCAS, autopilot … (AvMap, Dynon, Garmin)
Landing light, strobe light and navigation lights
Fuel tanks: 80L or 120L or 200L
Cowling flap
Ground anchor loops
Glider towing possible (Tricycle gear only)

133

kt
TAS at FL65

3400

km
range

225

kg
payload

250

m
take-off distance

MCR M

Rotax engine 912 UL

Power 80 cv
Speed 240 km/h
MTOW 544 kg
Capacity 150 L

MCR M

Rotax engine 912 ULS

Power 100 hp
Speed 246 km/h
MTOW 544 kg
Capacity 150 L

MCR M

Rotax engine 914 UL

Power 115 hp
Speed 252 km/h
MTOW 544 kg
Capacity 150 L

Brochure MCR M English