Modele ULC EVOLUTION | MCR Evolution - SE Aviation Aircraft | The world reference in MCR
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

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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

km

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

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