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Cvjetkovic CA-65B High Performance
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
00 HP Rotax 912S Engine
x
20 ft.
7 ft. 4 in.
25 ft.
108 sq. ft.
2
681 lbs.
x
1200 lbs.
16.3 gals.
x |
performance
takeoff
distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
640 ft.
600 fpm
150 mph
130 mph
x
12000 ft. |
limiting and recommended speeds
design
manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
x
0 mph
x |
All specifications are based on
manufacturer's calculations |
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