iKarus C42 User Manual

Pilot Operating Handbook for the C42 Series
POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 54 of 73
16. Parameter
Wingspan C42 (A) & C42B : 9450mm (31,0 ft)
Wing area: 12.5m
2
(134,5 ft
2
)
Wingspan C42 C & C42CS : 8710mm (28,6 ft)
Wing area: 11.9m
2
(128,1 ft
2
)
Wing chord at root: 1435mm (4,7 ft)
Wing dihedral (type-V) 1°
a.) Configuration angle of the wing relative to the main tube:
8,5°
Note: The incidence angle is measured from the lower
edge of the rear wing tube to the lower edge of
the front wing tube at the root rib.
b.) Configuration angle of the horizontal stabilizer relative to the
main tube: 7°
Note: The stabilizer incidence angle is measured from
the lower edge of the front tube to the lower edge
of the rear tube of the horizontal stabilizer.
Configuration difference angle: between the wing and
horizontal stabilizer, measured at the root of the rib : 1,5°

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