iKarus C42 Series Maintenance Manual

COMCO IKARUS
Maintenance Manual C42 Series
MaintenanceManual C42-
Series_Issue_VII_18.02.2014.doc
Revison No.:1 22 from 107
2.4 Landing gear
Nose wheel landing gear:
The nose wheel landing gear comprises the sprung nose wheel fork, the axle bolt,
the nose wheel, the nose wheel spar and the steering bar. Up until 2003, a steel
compression spring was used. However, since 2003 spring elements made of
polyurethane have replaced the pressure spring. The nose wheel fork is stored in the
nose wheel spar which passes through the fuselage tube and the engine mount and
is attached to the engine mount by means of a mounting bracket.
Figure 18: Nose wheel landing gear
2.4.1 Main landing gear:
The main landing gear comprises the cross beam, joists, axle tubes, shock
absorbers, trailing arms and spar struts as well as wheel axles and main wheels. The
individual elements of the landing gear are connected to each other by screws.
Figure 19: Main landing gear
steering bar
nose wheel mount
(nose wheel
spar
)
nose wheel fork
rubber boot with subjacent spring
(before 2003)
axle bolt
fuselage tube
engine mount
spar strut
cross beam
trailing arm
axle tube
shock absorber
wheel axle
fuselage tube
joists
polyurethane spring elements
(since 2003)

iKarus C42 Series Specifications

General

Brand	iKarus
Model	C42 Series
Category	Aircrafts
Language	English