TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 05 Inspection and Maintenance
Issue: 04.APR 2016 Page 29
Unless stated otherwise the inspection methods follow standard
practice and are mainly visual. However specific attention shall be
paid to the elements listed in section 04-30-10. In case of doubt
perform dye penetrant inspections at the welding connections and
highly stressed areas as indicated in the inspection list.
05-10-01 Component Time Limits
Time Between Overhaul
2000 h / 15 years
(refer to latest ROTAX
documentation applicable to
the actual SN of the engine)
Time Between Replacement
Depending on annual test
result
Fuel, oil and coolant hoses
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