C42 SERIES Pilot Operating Handbook
POH Issue 4 Rev. 5 Page 56 of 91
Trim-tab
Lever nose-down:
trim flap in relation to the elevator rudder area ....................................... -5°
Note:
With mechanically actuated trim flaps do not exceed -5° upwards
-5°
d) 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 ..................................................................... 0.42 pts (200 ml)
Hydraulic oil .................................................................................... HVP 10
e) 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.
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