AIRCRAFT PROGRAM
| Lift type | Fixed wing | ||
| Construction type | Factory-built | ||
| Control type | Piloted | ||
| Engine type | Piston | ||
| Application | Ultralight | ||
| Final assembly | Mengen-Hohentengen | ||
| Search for other aircraft programs with these properties on the Aircraft Programs directory page. | |||
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High wing single piston ultralight. Includes the variants C42 C (shorter span) and C42 CS (most agile).
| Variant | Launch/First flight | Production end | |
| Ikarus C42 B | 2003 / 2003 | Single piston ultralight aircraft with high trapezoidal, includes C42 C/CS variants. |
| Beringer Aero (was Beringer SA) | Analysis | Brake System Components: Brake system including parking brake (C42 CS) |
| Full Lotus Floats | Analysis | Aircraft Floats: Inflatable floats (option) |
| BRS Aerospace | Analysis | Whole Aircraft Parachutes: Optional BRS 6-10-50-SP ballistic recovery parachute (C42 B) |
| Junkers Profly | Analysis | Whole Aircraft Parachutes: Optional ballistic recivery parachute (C42 B) |
| Becker Avionics GmbH | Analysis | Radio Communications Equipment: Optional radio communication system (C42 C) |
| BRP-Rotax GmbH & Co KG | Analysis | Piston Engines: (R912 Series - Ikarus C42 B - Optional Rotax 912 UL/ULS/iS R914 Series - Ikarus C42 B - Optional Rotax 914 ) |
| DUC Hélices Propellers | Analysis | Composite Propellers: Optional propeller (C42 B) |
| GSC Systems | Analysis | Wooden Propellers: Optional three-blade, ground adjustable pitch propeller (C42 B) |
| Neuform Composite Propellers | Analysis | Composite Propellers: Optional propeller (C42 B) |
| Warp Drive Inc | Analysis | Composite Propellers: Optional two/three-blade, carbon fibre propeller (C42 B) |
