2014 JIHLAVAN SKYLEADER 600


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    Aircraft Summary


    General

    Year
    2014
    Manufacturer
    JIHLAVAN
    Model
    SKYLEADER 600
    Serial Number
    6229251T
    FlightRules
    VFR
    Condition
    Used
    Total Time
    159.0
    Number of Seats
    2
    Description
    It is a very special aircraft in the Ultra Light Aircraft (UL) and Light Sports Aircraft (LSA) category. Getting the license is very affordable. It is produced in Czech Republic, which is the world leader in UL and LSA category plane production. The plane is very fast (max. Speed 265 km/h / 143 knots / 165 mph, cruise speed 220 km/h / 122 knots / 137 mph, min. speed 61 km/h / 33 knots / 37 mph), has enormous range of 1.600 km / 860 nm / 1.000 miles, consumes ca. 15-16 liters (4 gallons) per hour of flying (ca. 7,5 liters per 100 km, or 38 miles per gallon) and has a retractable landing gear. Yearly maintenance costs are less than for a passenger car. The aircraft is very well equipped and has more equipment than many aircrafts from the general aviation, like Global Positioning System Garmin 795, Electronic Flight Information System Dynon D1000, Emergency Locater Transmitter, Rescue System GRS 600SD – Parachute, etc. The plane is almost new. It was used less than one year and made only 159 flight hours, which is almost nothing in aviation. It was not used for pilot training. It had only two owners. The previous owner was a professional pilot and he made the majority of the flight hours. The plane has foil stripes with sporty looks, but can be easily removed and replaced with other ones. The aircraft is currently registered in Serbia, but can be exported to any country in the world. It has all papers according to the International Civil Aviation Organization (ICAO), which makes it very easy to be registered in any country. We can provide answers to any question at +40731496551.

    Airframe

    Airframe Notes
    All metal two-seat, low wing constructed aircraft with a trapezoidal wing. The aircraft has a tricycle towed retractable gear.

    Engine

    Engine Notes
    Engine ROTAX 912 ULS 100 HP, electric starter and exhaust system, 4-cylinder, 4-stroke liquid- / air-cooled with opposed cylinders, dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet, 2 carburetors, mechanical fuel pump, dual electronic ignition, propeller speed reduction unit, air intake system.

    Props

    Prop Notes
    Propeller WoodComp SR3000/3WN, 3-blade, flight electrically adjustable + constant speed

    Avionics

    Avionics/Radios
    - Radio Dittel KRT + VHF antenna; - Transponder Funkwerk TRT 800H - S-mode + antenna; - Global Positioning System for navigational assistance - GPS- Garmin 795 + installation frame; - Electronic Flight Information System - Dynon D100 7” – EFIS module, backup battery, heated pitot tube; - Emergency Locater Transmitter Pack – ELT Kannad 406AF;

    Additional Equipment

    Additional Equipment
    RESCUE SYSTEM - Complete Safety set installation (parachute) – GRS 600SD; FLIGHT INSTRUMENTS AND INDICATORS - Airspeed indicator backup (kt, 80 mm) - Altimeter backup (feet, 80 mm) - Variometer backup (feet/min, 80 mm) - Bank indicator (60 mm) - Elevator trim indicator ENGINE INSTRUMENTS - Tachometer - Cylinder head temperature - Oil temperature - Oil pressure - Fuel pressure - Manifold pressure gauge - L and R fuel indicator - Hobbs meter - Voltmeter - Battery charging indicator FLIGHT CONTROLS - Fowler flaps electrically operated with automatic trim - Electrically operated elevator trim from pilot and co-pilot stick - Dual controls, 5 buttons on pilot and co-pilot side control stick - Tricycle retractable landing gear with steerable nose wheel + audio alert - Toe brake on pilot and co-pilot side - Starter button - Choke - Parking brake ELECTRICAL SYSTEMS - Master key - Circuit breakers - Magnetos Switches - 2 x 12V Socket - Flap control - Li-Fe-Po4 battery - Canopy lockout indication FUEL SYSTEMS - Engine driven fuel pump - Auxiliary fuel pump, electric - Fuel selector - Two fuel tanks with 120 L total capacity - Two fuel tanks caps with dipstick CABIN COMFORT SYSTEM - Transparent brown tinted canopy - Ventilation/Photography windows - Cabin heating - Wall to wall carpeting - Hydro-pneumatic canopy struts PRODUCT SUPPORT AND DOCUMENTS - Handling Bar - Pitot tube cover - Flight and Maintenance Manual - Aircraft Logbook - Engine Manual and Logbook - Propeller Logbook - Weight and Balance Protocol, Flight Test Protocol, Leveling Protocol

    Exterior

    Exterior Notes
    - Cabin lock - One tone WHITE paint with foil stripes and logo Skyleader - Strobe tail light - Position lights and strobes (strobe) - Landing light – nose wheel attachment - Wheels: Nose - 300x85 4“, Main -350x115 6“ - Tie-down rings
    Year Painted
    2014

    Interior

    Interior Notes
    - Cockpit with side by side seats - Standard cloth seats upholstering - Four-point safety belts (Schroth co.) in black - Baggage compartment - Instrument panel black painted
    Year Interior
    2014

    Inspection Status

    Inspection Status
    Latest Aircraft Maintenance Program was approved by the Civil Aviation Directorate in February 2017. Yearly Inspection and Regular Service performed in August 2017.


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