iKarus C 42 Series - Rigging Data; Wing Incidence Angle; Stabilizer Incidence Angle; Incidence Angle Difference

C42 SERIES Pilot Operating Handbook
POH Issue 4 Rev. 5 Page 53 of 91
16 Rigging data
Wingspan C42 / C42 B / C42 E: .................................... 31,0 ft (9450 mm)
Wing area .................................................................... 134,5 sq ft (12,5 m
2
)
Wingspan C42 C / C42CS .............................................. 28,6 ft (8710 mm)
Wing area .................................................................... 128,1 sq ft (11,9 m
2
)
Wing chord at root: ............................................................4,7 ft (1435 mm)
Wing dihedral ............................................................................................ 1°
a.) Incidence angle of the wing
relative to the fuselage main tube: ............................................... 8,5°
Note The incidence angle is measured from the lower edge of the rear
wing tube to the lower edge of the front wing tube at the root rib.
b.) Incidence angle of the horizontal stabilizer
relative to the fuselage main tube: .................................................. 7°
Note The stabiliser incidence angle is measured from the lower edge
of the front tube to the lower edge of the rear tube of the
horizontal stabiliser.
Incidence angle difference
of the wing to the horizontal stabiliser
measured at the root rib: .................................................................. 1,5°