The lightest ultralight for fast trips

ULC EVOLUTION

MCR ULC EVOLUTION is the most efficient ultralight of the MCR.

Thank to its flaps Fowler type and its meticulous aerodynamics, MCR ULC Evolution can fly from 68km/h to 250km/h awith a 100hp engine.

The accuracy of Michel Colomban’s calculations and the widespread use of composite materials make the MCR ULC Evolution the only high-performance multi-axis ULM to offer a large payload (250kg), exceptional climb speeds and low operating costs.

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Wingspan 8.66 m

Lenght 5.53 m

Wing area 8.31 m²

Cabin width 1.12 m

2525 km de range (with 150L wing fuel tanks)

Fast

Large payload

Safe Ultralight with BRS parachute

MT Propeller electric or hydraulic variable pitch, two or three blades
MT Propeller or E-props fixed pitch propeller, two or 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 lights
Fuel tanks: 80L or 100L or 150L
Cowling flap
Ground anchor loops
Glider towing possible

270

kg
payload

249

Km/h
(TAS at FL65)

1200

feet / minute

2525

range

MCR ULC EVOLUTION

Rotax engine 912 UL

Power 80 hp
Speed 238 km/h
MTOW 525 kg
Capacity 80L - 150 L
Consumption 17 L/h

MCR ULC EVOLUTION

Rotax engine 912 ULS

Power 100 hp
Speed 249 km/h
MTOW 525 kg
Capacity 80L - 150L
Consumption 20 L/h

Brochure ULC English

ULC EVOLUTION

2525 km de range (with 150L wing fuel tanks)

Fast

Large payload

Safe Ultralight with BRS parachute

MCR ULC EVOLUTION

Rotax engine 912 UL

MCR ULC EVOLUTION

Rotax engine 912 ULS

MCR Evolution - SE Aviation Aircraft