Dyn'Aéro MCR4S
Dyn'Aéro · France · first flew 2000 · light aircraft
The Dyn'Aéro MCR4S is a four-seat kit-built development of the two-seat MCR01.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Carbon-fibre monocoque fuselage with a large forward-hinged canopy |
| T — Tail | T-tail |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Low-wing, single-engine four-seat kit aircraft
- T-tail with an all-moving tailplane
- Carbon-fibre monocoque fuselage with a large forward-hinged canopy
A low-wing T-tailed four-seater with faired main wheels on short vertical legs and winglets.
Specifications
- The Dyn'Aéro MCR4S has a length of 6.72 m (22 ft).
- It has a wingspan of 8.66 m (28 ft).
- Its maximum speed is 250 km/h (155 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It differs mainly in a longer fuselage with an extra row of seats and slotted flaps in place of flaperons. It first flew on 14 June 2000.
Variants
It is sold in several versions by SE Aviation of Pontarlier, with a range of Rotax flat-four engines. The Dyn'Aéro Twin-R was a derivative.
Where you'll see it
It is sold as a kit for homebuilding; about 90 appeared on European civil registers by mid-2010.
Related aircraft
- Dyn'Aéro MCR01
- Dyn'Aéro CR.100
- Dyn'Aéro Twin-R
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