Dyn'Aéro MCR01
Dyn'Aéro · France · first flew 1996 · light aircraft
The Dyn'Aéro MCR01 is a two-seat, low-wing, all-composite carbon-fibre light aircraft.
Recognition (WEFT)
| W — Wings | Low-mounted, tapered |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 5.4 m fuselage |
| T — Tail | T-tail |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- All-composite carbon-fibre low-wing two-seater
- T-tail
- Rotax 912 engine in the nose
A low-wing T-tail light aircraft with a Rotax 912 engine and a top speed of about 318 km/h.
Specifications
- The Dyn'Aéro MCR01 has a length of 5.4 m (18 ft).
- It has a wingspan of 6.63 m (22 ft).
- Its maximum speed is 318 km/h (198 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
The MCR01 is a variant of the Colomban MC-100 Ban-bi originally designed by Michel Colomban.
Variants
It was built by Dyn'Aéro and is now supplied in kit form and ready-to-fly by SE Aviation. The MCR4S is a variant.
Where you'll see it
It was originally manufactured by Dyn'Aéro and is now available in kit form and ready-to-fly through SE Aviation.
Related aircraft
- Dyn'Aéro CR.100
- Dyn'Aéro MCR4S
- Dyn'Aéro Twin-R
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- Aero Bravo 700
- AeroKuhlmann Scub
- Aerolite 103
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