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iKarus C42 Series User Manual

iKarus C42 Series
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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)

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iKarus C42 Series Specifications

General IconGeneral
ManufacturerComco Ikarus
TypeLight sport aircraft
Maximum takeoff weight472.5 kg (1, 042 lb)
EngineRotax 912
Horsepower80 hp (60 kW)
Cruise speed160 km/h
Range800 km
Service ceiling4, 000 m
Stall speed65 km/h
Rate of climb5 m/s

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