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DynAero MCR 4S
New four seat aircraft. Can be built with just
two seats and a large payload capacity.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
Rotax
80 to 115 turbo
fixed or
variable pitch MT
6.72m
1.95m
8.66m
8.30sq m
4
x
x
x
x
1706km |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
x
x
320kph
x
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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