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