Manoeuvrable, Sports, aerobatic certified

MICROVOLT EVOLUTION

Directly derived from the MCR SPORTSTER EVOLUTION, the MCR MICROVOLT EVOLUTION is the two-seater aerobatic aircraft in the MCR range

Equipped with a lift stiffened by shrouds, doubled carbon wing spars and a reinforced fuselage, the MCR MICROVOLT EVOLUTION‘s airframe is very robust to benefit from 4 hours of aerobatic autonomy.

Certified by the DGAC in aerobatic categories A1 and A2, with limitations set at +7/-3.5 G solo and +6/-3 G two-up, the MCR MICROVOLT EVOLUTION is also ideal for travel; safe and comfortable thanks to the electric flap system and its structural parachute.

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Wingspan 6.63 m

Length 5.53 m

Wing area 5.20 m²

Cabin width 1.12 m

Aerobatic certified

2-seater light aircraft for traveling

Fast

Economical

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

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

Carbon and glass fiber blades for main landing gear and sandowfor nose landing gear
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 light
Fuel tanks: 80L or 120L or 200L
Cowling flap
Ground anchor loops

172

kt
TAS at FL120

3400

km
of range

225

kg
payload

250

m
take-off distance

MCR MICROVOLT EVOLUTION

Rotax engine 912 ULS

Power 100 hp
Speed 265 km/h
MTOW 490 kg
Capacity 80 L - 200 L
Consumption 20 L/h