POH LTF-UL-2019 C42B Issue 1 • Pilot Operating Handbook
POH LTF-UL-2019 C42B Issue 1
Page 51 of 84
Figure 10: Angle between trim tab and elevator
f) Trim-tab
Lever nose-down:
trim flap in relation to the elevator rudder area ....................................... -5°
With mechanically actuated trim flaps do not exceed -5° upwards
-5° for mechanical trim
g) Landing gear
Main landing gear
2.0 - 2.5 bar
29 - 36 PSI
Nose landing gear
1.6 - 2.0 bar
23 - 29 PSI
Shock absorbers
28.0 - 34.0 bar
400 - 490 PSI
Amount of oil ..................................................................... 0.43 pts (200 ml)
Hydraulic oil ..................................................................................... HVP 10
h) Brakes
In the Ikarus C42 series different brake systems are used.
e.g.-Sachs, Magura, Tost and Beringer brakes.
For service information, please see our maintenance manual or ask one of
our ISC or ITB.
i) Engine
For service information, please see our maintenance manual, or
maintenance manual by ROTAX or ask one of our ISC and ITB.