DynAero MCR M

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range
Rotax 100 to 115 turbo
fixed or variable pitch MT
5.53 m
1.53 m
8.66 m
8.3 sq m
2
x
x

x
x
1337km

performance

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