iKarus C42 Series Pilot Operating Handbook page 56

Pilot Operating Handbook for the C42 Series
Rudder
Left
Right
Measuring point distance from the steering axis: 410 mm
Elevator
Upwards
Downwards
Measuring point distance from the steering axis: 410 mm
Flettner rudder (C42C & C42CS)
When the elevator neutral: Flettner rudder
Flaps
Note :
Position I
Position II
(take-off/ landing)
Position III
(landing)
Measuring point distance from the steering axis: 310 mm
Trim tab
Lever nose-down:
Note: with mechanically actuated trim flaps do not exceed -5°
upwards.
POH C42 SERIES ISSUE1 (B) REV7
32° ± 2°
32° ± 2°
28° ± 2°
20° ± 2°
0° ± 2°
Flap angle is measured from the flap bottom to the
bottom of the wing at the root area (tangent front to rear
spar)
-5°± 1°
+11°± 1°
+32°± 1°
trim flap in relation to the rudder area -5°
210 mm ± 15 mm
210 mm ± 15 mm
210 mm ± 15 mm
130 mm ± 15 mm
78 mm ± 3 mm
27 mm ± 5 mm
60 mm ± 5 mm
170 mm ±10 mm
25/04/2020 Page 56 of 73