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DynAero MCR CLUB
Separate flaps and ailerons give reduced stall speed, classic
handling, gentle stall and better short field performance.
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 pitch or variable speed MT
5.53
m
x
6.90
m
6.46
sq m
2
x
x
x
x
1299km |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
x
x
339
kph
306
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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