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