Operation & Maintenance Manual
CD-135 / CD-155
OM-02-02
Revision no.:
Revision date:
Chapter:
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02-OM-06-02
4
30.07.2014
3
74
7
20.07.2016
6.2.1
After the 3rd - 6th operating hour
•
Check the oil system for leakage (refer to Annex 2, Page 13
of this Chapter)
•
Check the fuel system for leakage
(refer to Annex 2, Page 13 of this Chapter)
•
Check the cooling system for leakage (refer to Annex 3,
Page 14 of this Chapter)
•
Visual inspection of the air filter
•
Visual inspection of hoses and fuel pipes
(refer to RM-02-02, Chapter 05-20.03)
•
Visual inspection of the FADEC sensors (refer to Annex 7,
Page 20 of this Chapter)
•
Visual inspection of the exhaust system
•
Visual inspection of the v-ribbed belt
(refer to Annex 1, Page 12 of this Chapter)
•
Perform an engine test run according to Chapter 4, Section
4.4.2, Page 5 of this Manual, read out the FADEC. E-mail
both the Real Time Log Files and Event Log Files to
Technify Motors GmbH (refer to Annex 10, Page 38 of this
Chapter)
•
Exchange the gearbox oil filter (refer to Annex 8, Page 25
of this Chapter);
The used gearbox oil filter should be labeled, stored in a
clean container and made available to Technify Motors
GmbH on request for the complete engine life time. The
sample will be required for a later long-run analysis. The
label must show the aircraft serial number, registration
number, engine serial number, operation time and date.
•
Check the presetting of the proportional pressure reducing
valve (refer to RM-02-02, Chapter 72-10.05 or
Chapter 72-10.16)
