Name: iKarus C42
Brand: iKarus
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Pilot Operating Handbook for the C42 Series

POH C42 SERIES ISSUE1 (B) REV7 25/04/2020 Page 55 of 73

c.) Control Surface Deflections

Note: The angle of the aileron bottom relative to the

wing chord is -5° (tangent front to rear spar). It is

defined by the length of the aileron push rods.

-5°

Distance from axis of rotation

Aileron

Neutral position: -7°± 1° -35mm ± 10mm

Upwards: 20°± 2° 90mm ± 10mm

Downwards: 14°± 2° 70mm ± 10mm

Measuring point distance from the steering axis: 250mm

Spade settings on the aileron in the C42C and C42CS model.

Spade angle in relation to the QR-bottom +3° ± 1°

Measurement with water level at base of 1 cm under Aileron end strip.

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