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iKarus C42 Series Maintenance Manual

iKarus C42 Series
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COMCO IKARUS
Maintenance Manual C42 Series
MaintenanceManual C42-
Series_Issue_VII_18.02.2014.doc
Revison No.:1 38 from 107
2.8.6 Wing flaps:
The wing flaps are actuated by a lever located in the middle of the longitudinal tube
of the canopy roof frame. The lever is linked to the flap horns via push-rods.
As an option, the wing flaps can also be actuated electrically via a servo motor which
is controlled by means of a rocker switch in the control stick or a separate rocker
switch in the instrument panel.
Figure 43: Flap controls
flap horn
spring-loaded lock
(also on the rear
side)
wing flap lever
wing flap track
wing
flap push rod
sliding sleeve
flap
spar

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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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