Ikarus C42 for sale
Used Comco Ikarus C42 from dealers in Europe — the Rotax-912 microlight, two seats side by side, 540 to 560 kg take-off mass depending on variant. All data from the DAeC light sport office data sheets. Calculate ferry flight and engine reserve right on this page.
Ikarus C42 for sale
No listings collected yet. Collection from dealer websites starts after launch — get new listings by e-mail.
Variants
| Variant | Engine | Power | Max. take-off weight | Seats | Fuel | Source |
|---|---|---|---|---|---|---|
| C 42 A | Rotax 912/UL; 912 S/ULS | 59,6 kW; 73,5 kW („lt. Hersteller“) | 540 kg mit Rettungsgerät | „2 / nebeneinander“ | 1 × 65 l (optional 2 × 65 l) | DAeC-Kennblatt 66141 Ausg. 2 (14.03.2024) |
| C 42 B / B Turbo | Rotax 912/UL; 912 S/ULS; 914 Turbo | 59,6 / 73,5 / 84 kW (5 min) | 540 kg mit Rettungsgerät | 2 | wie A: 1 × 65 l (optional 2 × 65 l) | DAeC-Kennblatt 66141.1 Ausg. 5 (20.03.2024) |
| C 42 C / C Turbo / CS | Rotax 912/UL; 912 iS/iSc Sport; 912 S/ULS; 914 Turbo (nur C) | 59,6 / 73,5 / 73,5 / 84 kW | 560 kg (BRS-6-1050 SP oder Junkers 601); 540 kg (Magnum 501 LS) | 2 | wie A: 1 × 65 l (optional 2 × 65 l) | DAeC-Kennblatt 66141.7 Ausg. 6 (20.03.2024) |
- Engine
- Rotax 912/UL; 912 S/ULS
- Power
- 59,6 kW; 73,5 kW („lt. Hersteller“)
- Max. take-off weight
- 540 kg mit Rettungsgerät
- Seats
- „2 / nebeneinander“
- Fuel
- 1 × 65 l (optional 2 × 65 l)
- Engine
- Rotax 912/UL; 912 S/ULS; 914 Turbo
- Power
- 59,6 / 73,5 / 84 kW (5 min)
- Max. take-off weight
- 540 kg mit Rettungsgerät
- Seats
- 2
- Fuel
- wie A: 1 × 65 l (optional 2 × 65 l)
- Engine
- Rotax 912/UL; 912 iS/iSc Sport; 912 S/ULS; 914 Turbo (nur C)
- Power
- 59,6 / 73,5 / 73,5 / 84 kW
- Max. take-off weight
- 560 kg (BRS-6-1050 SP oder Junkers 601); 540 kg (Magnum 501 LS)
- Seats
- 2
- Fuel
- wie A: 1 × 65 l (optional 2 × 65 l)
Values from the official type certificate only. Seat figures quoted verbatim; where several weights are certified, we show them all.
Frequently asked questions
Which engines does the Ikarus C42 have?
Depending on variant Rotax 912/UL (59.6 kW), 912 S/ULS or 912 iS (73.5 kW) or 914 Turbo (84 kW, 5 min) — DAeC data sheets 66141 series.
What is the take-off mass of the C42?
A and B: 540 kg with rescue system; C/CS: 560 kg (with BRS-6-1050 SP or Junkers 601) or 540 kg (Magnum 501 LS) — DAeC data sheets.
Which data sheets apply to the C42?
The data sheets of the DAeC light sport office (delegated by the LBA): 66141 (A), 66141.1 (B), 66141.7 (C/CS) — sheet per serial number.