Kappa 77 KP 2U-SOVA

The Kappa 77 KP 2U-SOVA is a two-seat civil utility aircraft designed in the Czech Republic and available in kit form for homebuilding. It is a conventional low-wing monoplane featuring all-metal construction and retractable tricycle undercarriage. It is marketed in the United States by Aero Adventure Aviation.

pecifications (KP 2U-SOVA)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=
crew=one pilot
capacity=one passenger
payload main=
payload alt=
length main= 7.17 m
length alt= 23 ft 7 in
span main= 9.90 m
span alt= 32 ft 6 in
height main= 2.60 m
height alt= 8 ft 7 in
area main= 11.9 m²
area alt= 128 ft²
airfoil=
empty weight main= 285 kg
empty weight alt= 682 lb
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 450 kg
max takeoff weight alt= 1,058 lb
more general=
engine (prop)= Rotax 912 piston engine
type of prop=
number of props=1
power main= 80/100 hp
power alt= 60/77 kW
power original=
max speed main=260 km/h
max speed alt= 160 mph
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main= 875 km
range alt=547 miles
ceiling main=
ceiling alt=
climb rate main= 450 m/min
climb rate alt= 1,475 ft/min
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=
armament=
avionics=
*
* [http://www.airliners.net/photo/Kappa-KP-2UR-Sova/1328831/L/ Picture of PH-3D7, a Dutch Kappa KP-2UR Sova]

ee also

aircontent
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similar aircraft=

sequence=KP 2 -
KP-5

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