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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

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Variants

VariantEnginePowerMax. take-off weightSeatsFuelSource
C 42 ARotax 912/UL; 912 S/ULS59,6 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 TurboRotax 912/UL; 912 S/ULS; 914 Turbo59,6 / 73,5 / 84 kW (5 min)540 kg mit Rettungsgerät2wie A: 1 × 65 l (optional 2 × 65 l)DAeC-Kennblatt 66141.1 Ausg. 5 (20.03.2024)
C 42 C / C Turbo / CSRotax 912/UL; 912 iS/iSc Sport; 912 S/ULS; 914 Turbo (nur C)59,6 / 73,5 / 73,5 / 84 kW560 kg (BRS-6-1050 SP oder Junkers 601); 540 kg (Magnum 501 LS)2wie A: 1 × 65 l (optional 2 × 65 l)DAeC-Kennblatt 66141.7 Ausg. 6 (20.03.2024)
C 42 A
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)
Source: DAeC-Kennblatt 66141 Ausg. 2 (14.03.2024)
C 42 B / B Turbo
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)
Source: DAeC-Kennblatt 66141.1 Ausg. 5 (20.03.2024)
C 42 C / C Turbo / CS
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)
Source: DAeC-Kennblatt 66141.7 Ausg. 6 (20.03.2024)

Values from the official type certificate only. Seat figures quoted verbatim; where several weights are certified, we show them all.

Type certificate data: DAeC-Kennblatt 66141 Ausg. 2 (14.03.2024) · DAeC-Kennblatt 66141.1 Ausg. 5 (20.03.2024) · DAeC-Kennblatt 66141.7 Ausg. 6 (20.03.2024) · As of 2026-10-19
C 42 A — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
C 42 B / B Turbo — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)
C 42 C / C Turbo / CS — cross-checked on 2026-10-19 by Cowork (Chrome, amtliche Kennblatt-PDFs, V6-Gegenlesung)

Ferry flight

Distance
—
Flight time
—

Great circle between the two airfields. Not a substitute for flight planning. Airfield data: OurAirports (public domain), as of 2026-10-19

Engine reserve

TBO per the engine manufacturer's service document

Remaining to TBO
— h
Reserve per hour
— EUR

Calculation: overhaul cost ÷ TBO. Manufacturer calendar limits apply in addition.

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.

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