2014 JIHLAVAN SKYLEADER 600
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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