Operation & Maintenance Manual
CD-135 / CD-155
OM-02-02
Chapter:
Issue:
Issue date:
Page:
Content:
02-OM-06-02
4
30.07.2014
4
74
Revision no.:
Revision date:
7
20.07.2016
6.2.2
Every 100 operating hours
•
Visual inspection of the air filter
•
Visual inspection of the cooling system
•
Visual inspection of the oil system
(refer to Annex 2, Page 13 of this Chapter)
•
Visual inspection of the fuel system
(refer to Annex 2, Page 13 of this Chapter)
•
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)
•
Visual inspection of the clamp on the turbocharger
•
Visual inspection of all fuel, oil, cooling system lines and
hoses for chafe marks
(refer to RM-02-02 Chapter 05-20.03)
•
Visual inspection of the engine mount for chafe marks
•
Check the airframe fuel pump
(refer to the aircraft manufacturer's specifications)
•
Test the cooling system under pressure at 2.0 bar
Duration: 2 minutes. Max. 2.0 bar must not be exceeded!
Afterwards check for leakage
(refer to the aircraft manufacturer's specifications).
•
Perform an engine test run according to Chapter 4, Section
4.4.2, Page 5 of this Manual and 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 engine oil and the oil filter (refer to Annex 5,
Page 16 of this Chapter);
A sample of the oil and the used 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.
Quantity of oil to be taken for sample: 100ml
•
Check the mixture ratio of the coolant
•
Replace the fuel filter (refer to the aircraft manufacturer's
specifications)
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