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2017 EKOLOT JK-05 JUNIOR

Details

General Specs

For Sale

2017

EKOLOT JK-05 JUNIOR

Odessa, FL USA


General Specs

New

2017

2017

N/A


Additional Classifications


Detailed Description

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.

Avionics / Equipment

Control system:

Control surfaces are stacked with the system of push rods and torsion pipes. Stacking of elevator and ailerons using a one control stick placed between the pilot seats. Stacking of rudder by two sets of pedals in front of each seat. Stacking of flaps and elevator trimmer electrical by using two sets of push-button on the top of control stick. Stacking of brakes- by lever placed on the control stick . Stacking of power by folding throttle levers on both sides. Stacking of fuel mixture by choke rod placed on the left side of control panel.

Fuel system:

Fuel system combines with two jointed fuel tanks of total capacity of 60 litres, placed behind the pilots cabinet or two tanks in wings 2x30litres as optional equipment, sedimentation tank and fuel filter. Fuel pipes made of rubber.

Electrical system:

Electrical units:

starter
ignition system
engines of stacking flaps and trimmer
indicators of engine functioning
indicators of fuel level
electrical pump of fuel
Supply:

battery
alternator
Switches in the cockpit:

main switch of current
two firing switches
ignition switches
flap control switches
trimmer control switches
Navigation equipment:

speedometer
altimeter
variometer
bank indicator
compass
static and dynamic pressure sensor
flap position indicator
trimmer indicator
Power system indicators:

tachometer
cooling fluid temperature indicator
voltmeter
fuel level indicator
fuel pressure indicator
time counter of engine

Engines / Mods

Power plant:

Engine: Rotax 912 UL The engine is mounted to the fuselage using frame of steel pipe construction and rubber shock absorbers. Three blades propeller Aero-Sail of 1,73 m diameter with adjustable on the ground spiral lead. Engine covers fixed by rapid mounted system cam-lock type. Automatic control of the engine temperature (thermostat). Anti icing system (carburettors heating system)

Interior / Exterior

Cabinet equipment:

Two shell plating reinforced with glass and carbon bucked seats, adjustable on the ground. Two kits of safety belts Side air inlets on the canopy Heating of the cockpit.

Painting:

External surface is painted white with acrylic enamel. Internal cabinet surface is painted grey.

Remarks

Fuselage:

Shell plating of composite with reinforcement with glass and carbon. On the top of cockpit there is a steel frame for mounting the wings. Fin is an integral part of the fuselage. In front of fuselage is placed the pilots cabinet contained two pilot seats twin set. Behind the cabinet three is the space used for mounting Rescue system. Glazing: Main windows with the Plexiglas of thickness 2mm reinforced by composite frame divided in plane symmetric axe top ward opened from the side to the top direction. Two side and one top window permanent cemented to the fuselage. Wings: Shell plating of composite reinforced with glass and carbon and with the reinforced carbon composite beam. Wings are fixed to the fuselage by two pins each side and supported by single struts. On the whole span the wigs are equipped with composite shell plating structure float-ailerons, reinforcement of the carbon rowing. The float-ailerons are fixed by five consoles each. Every float-aileron is equipped with anti flutter mass balance Tail plane: Elevator and ruder are the same construction i.e. composite frames. Undercarriage: Three-wheeled, with a nose wheel. Nose undercarriage is manufactured with steel and is equipped with rubber rings as a shock absorber. Main chassis on the separated cantilever suspension springs of reinforced composite structure. Wheel axis are made of steel. Main chassis brakes are hydraulic disc brakes. Each wheel tires have dimensions 350x100 mm. Nose and main chassis is equipped with covering spinners.

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