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AIRCRAFT PROGRAM

Skyleader 500

Lift typeFixed wing
Construction typeFactory-built
Control typePiloted
Engine typePiston
ApplicationTouring, Trainer, Ultralight
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Low wing, single piston light aircraft.

Type variants

Variant Launch/First flight Production end  
Skyleader 500 2004 / 2003 Two-seat side by side recreation ultralight/light sport aircraft developed from Kappa KP-2U Sova.

Supply chain

  (9 links)
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Airframe Systems / Safety & Security Systems

Galaxy GRS s.r.o. Analysis Whole Aircraft Parachutes:

Avionics / Communications (Airborne)

Garmin International Analysis Radar Transponders: GTX 327 transponder; Radio Communications Equipment: SL40 radio

Avionics / Indicators and Instruments

Dynon Avionics, Inc. Analysis Electronic Flight Instrument Systems: Optional EFIS-D100, EMS-D120

Avionics / Navigation Aids (Airborne)

Power Systems / Engines

BRP-Rotax GmbH & Co KG Analysis Piston Engines: (R912 Series - Skyleader 500 - Optional Rotax 912 UL/ULS R914 Series - Skyleader 500 - Optional Rotax 914 UL )
Jabiru Aircraft Pty Ltd. Analysis Piston Engines: Optional Jabiru 2200/3300 (Kappa)

Power Systems / Rotors & Propellers

2XP TECHNOLOGIES Analysis Composite Propellers: Three blade, ground adjustable pitch propeller
Woodcomp sro Analysis Composite Propellers: Three blade, ground adjustable pitch propeller (Kappa)
Information on this page is compiled from a variety of published sources, and links do not necessarily imply recommendation or confirmation by the airframe manufacturer.