iKarus C42C User Manual

C42 SERIES Pilot Operating Handbook
POH Issue 4 Rev. 5 Page 55 of 91
Rudder
Left 32°±-2° 8.86” ± 0.39” (210 mm ± 10 mm)
Right 32°±-2° 8.86” ± 0.39” (210 mm ± 10 mm)
Measuring point distance from the steering axis: ............. 16.24” (410 mm)
Elevator
Up 28°±-2° 8.27” ± 0.59” (210 mm ± 15 mm)
Down 20°±-2° 5.12” ± 0.59” (130 mm ± 15 mm)
Measuring point distance from the steering axis: ............. 16.24” (410 mm)
Flettner (Servo) trim-tab (model C42C and C42CS)
When the elevator neutral: Flettner tab ................... 0° ± 2° 78 mm ± 3 mm
Flaps
Note:
Flap angle is measured from the flap bottom to the bottom of the wing at the
root area (tangent front to rear spar)
Position I -5° ± 1° 1.06” ± 0.39” (27 mm ± 10 mm)
Position II +11° ± 1° 2.36” ± 0.39” (60 mm ± 10 mm)
Position III +32° ± 1° 6.69” ± 0.39” (170 mm ± 10 mm)
Measuring point distance from the steering axis: ............. 12.20” (310 mm)

iKarus C42C Specifications

General

Brand	iKarus
Model	C42C
Category	Aircrafts
Language	English