KLN VL-3

The VL- 3 is an ultralight, single-engine, low-wing aeroplane of classical design with a bow-type retractable or fixed landing-gear and two side-by-side seats. The plane has been certified according to regulation UL-2 of the Amateur Aeronautical Association of the Czech Republic for maximum take-off weight (MTOW) of 450 kg. Harmonious aerodynamic shape and excellent flying performance make the aeroplane suitable for touring or recreational flying.

The design uses carbon and hybrid materials, mainly in the form of sandwiches.

The airplane is being certified in UL category for MTOW 450 kg and for MTOW 560 kg according JAR - VLA

specifications
 
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range
100 hp
x
20.5 ft
6.7 ft
27,7 ft
105 sq ft
2
x
x

992 lb
24 gal
x

performance

takeoff distance, ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling
x
1200 fpm
151 kts
113 135 kts
x
x

limiting and recommended speeds

design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed
x
162 kts
35 kts
x

All specifications are based on manufacturer's calculations