AIRCRAFT PROGRAM
| Lift type | Fixed wing | ||
| Construction type | Factory-built | ||
| Control type | Piloted | ||
| Engine type | Piston | ||
| Application | Ultralight | ||
| Search for other aircraft programs with these properties on the Aircraft Programs directory page. | |||
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High wing composite single piston ultralight.
| Variant | Launch/First flight | Production end | |
| Ekolot JK-05L Junior | 2001 / 2001 | Side by side seated ultralight aircraft. | |
| Ekolot KR-030 Topaz | 2007 / 2006 | Side by side seated ultralight aircraft, high-wing configuration designed to comply with French ultralight rules. |
| Ekolot |
Other aircraft programs: Ekolot KR-010 Elf
| Beringer Aero (was Beringer SA) | Analysis | Aircraft Wheels: (KR-030) |
| Galaxy GRS s.r.o. | Analysis | Whole Aircraft Parachutes: GRS 6/473 softpack ballistic recovery parachute (KR-030) |
| f.u.n.k.e. Avionics GmbH | Analysis | Radio Communications Equipment: ATR833 Mk II radio (KR-030); Radar Transponders: TRT800H transponder (KR-030) |
| Garmin International | Analysis | Electronic Flight Instrument Systems: Garmin G3X suite (KR-030) |
| Kanardia | Analysis | Electronic Flight Instrument Systems: Indu series (KR-030); Electronic Flight Instrument Systems: Nemis III EFIS (KR-030) |
| AIR Avionics | Analysis | Collision Avoidance Systems/TCAS: TRX 2000F collision warning system (KR-030) |
| BRP-Rotax GmbH & Co KG | Analysis | Piston Engines: (R912 Series - Ekolot JK-05L Junior - Rotax 912 UL; Ekolot KR-030 Topaz - Rotax 912 UL/ULS/iS ) |
| 2XP TECHNOLOGIES | Analysis | Composite Propellers: Three-blade 1.73m ground adjustable propeller (JK-05); optional AS 16500/1950 or AS 1730/1950 ground adjustable propeller (KR-030) |
| DUC Hélices Propellers | Analysis | Composite Propellers: Optional Swirl three-blade constant speed propeller (KR-030) |
| Woodcomp sro | Analysis | Wooden Propellers: Optional KW-20 constant speed propeller (KR-030) |
