iKarus C42 User Manual

Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 57 of 73
d.) Main Landing Gear
Main Landing Gear 2.0 - 2.5 bar 29 - 36 psi
Nose Landing Gear 1.6 - 2.0 bar 23 - 29 psi
Shock Absorbers 28.0 - 34.0 bar 400 - 490 psi
Quantity of Oil 200 ml (0.42 pts)
Hydraulic Oil HVP 10 (hydraulique)
e.) Brakes
In the Ikarus C42 series different brake systems are used. e.g.-Sachs,
Magura, Tost and Beringer brakes.
For service information, please see our maintenance manual or ask one
of our IFC, ISC, Importer or the manufacturer.
f.) Moteur
For service information, please see our maintenance manual, or
maintenance manual by ROTAX or ask one of our IFC, ISC, Importer or
the manufacturer.

iKarus C42 Specifications

General

Manufacturer	Comco Ikarus
Type	Ultralight Aircraft
Engine	Rotax 912
Cruise Speed	160 km/h
Stall Speed	65 km/h
Seats	2
Height	2.3 m
Maximum Takeoff Weight	472.5 kg
Range	800 km
Service Ceiling	4000 m
Power Output	80 hp
Rate of Climb	5 m/s