COMCO IKARUS
Maintenance Manual C42 Series
MaintenanceManual C42-
Series_Issue_VII_18.02.2014.doc
Revison No.:1 86 from 107
Step 13. Connect the pitot tube to its fitting situated to the left of the pilot’s headrest.
Pull out the pitot tube forwards to its full extent.
Step 14. Repeat steps 1 through 12 for the other wing. Now you may remove the
control lock.
Step15. Attach right and left aileron push rods to the central bellcrank connection.
Carefully ensure that the slide mechanisms of the special link connectors
are properly engaged (closed and locked).
Step 16. On the flap drive tube, take the split sleeve fitted around the sprung taper
pins (and through which they protrude), spread it a little, then rotate it over
the pins. Using this sleeve as an aid, squeeze it, thus compressing the
pins. Then move the sleeve so that the drive fitting moves freely on its
tube.
Step 17. Align the flap root tube and its drive fitting on the fuselage. Slide the flap
drive fitting over the junction so that its cutaways engage snugly in the
roots of the flap frame tubes and the sprung pins are fully out. Rotate the
split sleeve so that its holes align with the tips of the pins again, permitting
the pins to spring out fully. Left and right landing flaps must be securely
locked and it may be necessary to wiggle the fitting a little to ensure proper
engagement, particularly when the aircraft is new.
Step 18. Position and fasten the wing centre section (cockpit roof).
Figure 79: Wing root
Forward spar attachment point
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