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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
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