The JK05L Junior is a high-wing monoplane with struts. All major classes of aircraft are constructed of glass and carbon fiber composites in the form of a shell structure.
The body consists of a self-supporting shell structure PARABEAM material. In the front part of the trunk cabin is with two side-ended arrange seats. The cabin is very comfortable 120 cm wide. The hull consists of two symmetrical parts with fastenings and an integrated floor. The seats are made of composite materials built into the shell structure and based on demand with leather. The cab windshield is made of UV-resistant polycarbonate, is symmetrically divided and opens upward.
The two wings connecting a pipe truss. The fin is integrated in the fuselage. The chassis is a three wheeled chassis with nose wheel. Cantilever legs made of composite materials. Main wheels braked integrated, the nose wheel controllable, coupled with rudder. Clad wheels optional. Rectangular surfaces, trunk characteristic narrowed for improving visibility. Was used in the profile NN-1817 because of its strength to resist contamination and favorable aerodynamic characteristic which has proven itself a glider PW-5 "SMYK".
The wing structure is like a shell, with supporting bar and the support with a brace. On the whole leaf width Flaperon in shell structure, attached to the wing to the fuselage operated five moveable arms. Flaperon made of carbon fiber composite for extremely high stiffness with minimal mass (anti-flutter requirements).
Inside the wing there are no installations or control systems.
Tailplane rectangular in shell structure made of composite materials. Rudder in shell structure.
Ram-type control systems. Height Trimmer feathery, electrically controlled. The aircraft is equipped with a stick (stick) in the mid-cabin. This allows plenty of room for writing and maps on the lap of the pilot and copilot. As a ROTAX 912 UL engine comes with 80 hp is used, which has more than enough power. Fuel tanks for 60 liters located behind the cockpit and allow in addition to Fuelanzeige in the cockpit a direct view of the liter capacity behind a glass.
Wing Span 35.3'
Wing Area 109.8sqft
Horizontal tail surface 15.5sqft
Useful Load 654.8lbs
Gross weight 1041.7lbs
Wing loading 8.4 lbs/sqft
Maximum speed 124 mph
Cruising speed 75% power 112 mph
Cruising speed 50% power 93 mph
Stall Clean 37 mph
Stall Landing Configuration 34 mph
Engine Rotax 912UL 80HP
Fuel capacity 16 gal