Operation & Maintenance Manual
CD-135 / CD-155
OM-02-02
Chapter:
Issue:
Issue date:
Page:
Content:
Checklist
4
17.04.2015
2
8
Revision no.:
Revision date:
5
20.07.2016
Engine Maintenance Checklist - General
Visual inspection of the engine mount for chafe marks
xxxxxxxx
Visually inspect the air filter
xxxxxxxx
Visual inspection of the cooling system
xxxxxxxx
Check the mixture ratio of the coolant
xxxxxxxx
Exchange coolant
(refer to the aircraft manufacturer's specifications)
x
every
24 month
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).
xxxxxxxx
Visual inspection of the oil system
(refer to Chapter 6, Annex 2 of this Manual)
xxxxxxxx
Visual inspection of the fuel system
(refer to Chapter 6, Annex 2 of this Manual)
xxxxxxxx
Replace the fuel filter
(refer to the aircraft manufacturer's specifications)
xxxxxxxx
Visual inspection of the FADEC sensors
(refer to Chapter 6, Annex 7 of this Manual)
xxxxxxxx
Visual inspection of the exhaust system
xxxxxxxx
Visual inspection of the clamp on the turbocharger
xxxxxxxx
Visual inspection of the gasket of the turbocharger oil
return line, replace if necessary.
x
only
CD-135
Visual inspection of the v-ribbed belt
(refer to Chapter 6, Annex 6 of this Manual)
xxxxxxxx
Replace v-ribbed belt
(refer to RM-02-02, Chapter 72-20.01)
x
Check the airframe fuel pump
(refer to the aircraft manufacturer's specifications)
xxxxxxxx
Inspection Items
Interval
(Engine operation hours)
Initials
100
200
300
600
900
1200
1500
1800
Time