iKarus C42 Owner's Manual

C42 Owner’s Manual (Microlight) Page 40
SECTION 13 - SETTING (RIGGING) AND MISCELLANEOUS DATA
13.1 Incident angle of wing with respect to main fuselage tube: 8°
Note: The incident angle is defined as the angle between a line parallel to the fuselage tube
and a line joining the undersides of the leading and trailing edge tubes at their roots.
13.2 Angle of stabilizer with respect to the main fuselage tube: 7°
Note: The stabilizer angle is defined as the angle between a line parallel to the fuselage tube
and a line joining the undersides of the leading edge and trailing edge of the stabilizer.
Angle difference between wing and stabilizer: 1°
13.3 Control Surface Deflections
Aileron Up 20 ±2° or 85 mm, ±9 mm measured 250 mm from the hinge axis.
Down 14° ±2° or 60 mm, ±9 mm measured 250 mm
from the hinge axis.
A
rea 0,58 m
2
per side.
Elevator Up 30° ±3° or 205 mm +
21 mm measured 410 mm from the hinge axis.
Down 20° ±3°. Or 140 mm +
21 mm measured 410mm from the hinge axis.
Area 0.82 m
2
total
Rudder L/R 32° ±3° or 217 mm +
21 mm measured 410mm from the hinge axis.
Area 0.44 m
2
Fin Area 0.61 m
2
Stabilizer Area 1,42 m
2
total
Flaps - 4.5° -15° - 42°
Relative to the fuselage tube.
Area 0.46 m
2
per side.
Elevator Trim Tab Up 1 to 5º
Down 25º±3º (relative to elevator)
13.4 Air pressure for tyres and shock absorber:
Main wheels 1.8 - 2.5 bar 26 to 36 psi.
Front wheel 1.5 - 1.8 bar 22 to 26 psi.
Shock absorbers 29 - 33 bar 425 to 486 psi
A special pressure pump, available from Red Aviation, is used for setting the shock
absorber pressures.

iKarus C42 Specifications

General

Brand	iKarus
Model	C42
Category	Aircrafts
Language	English