iKarus C42 User Manual

Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 37 of 73
8. Weight and Balance
Place the aircraft in a level position on three scales with the stabilizer and
elevator leveled.
The center of gravity is measured in mm behind the reference datum and
then calculated as a percentage of the wing chord.
Reference datum (leading edge)
Wing chord l = 1360 mm.
X1 = 230 mmm
X2 = 1770 mm ou 1775 mm (C42CS)

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