MCR
MCR4S
Four seats in a carbon ULM-sized package.
The MCR4S is the four-seat stretch of the MCR idea — still carbon, still fast for the power, and one of the few light four-seaters that started life in the French kit/ULM world.
Key figures
Max speed
310 km/h
Range
1,600 km
Engine
Rotax 915 iS
Seats
4
Dimensions
Top view
Wingspan
8.7 m
Side view
Length
6.7 m
Height
2.3 m
Performance
Cruise
280 km/h
Max speed
310 km/h
Vne
335 km/h
Stall
90 km/h
Stall speed (clean)
101 km/h
Climb
6 m/s
Airframe
- Category
- Kit
- Wing
- Low wing
- Seats
- 4
- Variant
- MCR4S
- First flight
- 2000
- Construction
- Carbon composite
- Materials
- Carbon sandwich
- Propeller
- Constant-speed
- Status
- in production
General
- Propeller
Composite ground-adjustable, typical Rotax installation
Estimated · Manufacturer brochure / published figures
- Fuel
MOGAS 95 / 100LL
Likely · Manufacturer brochure / published figures
- Best glide ratio
11:1
Estimated · Manufacturer brochure / published figures
Weights
- Empty weight
430 kg
Likely · Dyn'Aéro MCR4S
- Max takeoff weight
750 kg
Likely · Dyn'Aéro MCR4S
- Useful load
320 kg
Estimated · Manufacturer brochure / published figures
- Fuel capacity
150 L
Likely · Dyn'Aéro MCR4S
Powerplant
- Propeller
Composite ground-adjustable, typical Rotax installation
Estimated · Manufacturer brochure / published figures
- Fuel
MOGAS 95 / 100LL
Likely · Manufacturer brochure / published figures