DynAero MCR ULC - short take off and landing

Current version has split flaps and ailerons and upswept wing-tip

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range
Rotax 80to 115 turbo
fixed or variable pitch MT
5.53m
x
8.66m
8.3sq m
2
x
x

x
x
1342km

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling
x
x
335kph
304kph
x
x

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed
x
x
x
x

All specifications are based on manufacturer's calculations