Operation & Maintenance Manual
CD-135 / CD-155
OM-02-02
Revision no.:
Revision date:
Chapter:
Issue:
Issue date:
Page:
Content:
02-OM-06-02
4
30.07.2014
7
74
7
20.07.2016
6.2.6 Every 900 operating hours
• Carry out all steps described in Section 6.2.4, Page 5 of this
Chapter
• Replace timing chain
ONLY applicable for engines Version 01
(refer to RM-02-02, Chapter 72-30.02)
• Replace friction disk, if clutch assy 05-7211-K0094xx is
installed (refer to RM-02-02, Chapter 72-10.14)
6.2.7 Every 1200 operating hours
(only applicable for CD-135)
• Carry out all steps described in Section 6.2.5, Page 6 of this
Chapter
• Replace v-ribbed belt (refer to RM-02-02, Chapter
72-20.01)
• Exchange coolant
(refer to the aircraft manufacturer's specifications)
• Replace coolant hose 05-7523-K0048xx (only DA42
installations)
• Visual inspection of the gasket of the turbocharger oil return
line, replace if necessary.
• Replace proportional pressure reducing valve (part of the
gearbox)
• Inspect gearbox (refer to Chapter 6, Annex 15, Page 63 of
this Manual)
• Inspect timing chain
ONLY applicable for engines Version 02
(refer to RM-02-02, Chapter 05-20.04)
CAUTION: The 1200 hrs gearbox inspection interval is only valid for P/N:
05-7212-K0435 02 CD-135 14V
05-7212-K0436 02 CD-135 28V
05-7212-K0439 02 CD-135 28V DA42
05-7212-K0413 03 CD-135 14V
05-7212-K0414 03 CD-135 28V
05-7212-K0417 03 CD-135 28V DA42
or later approved revisions, in combination with the dual mass
flywheel and the use of gearbox oil Shell Spirax S6 ATF ZM or
CENTURION Gearbox Oil N1.
In all other cases, the interval remains at 300 or 600 hrs.
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