General
The representation of components in this chapter which are not scope of the delivery is
only symbolic. The design shown in this chapter does not represent a specified execution
but should support the understanding of the system.
The final design, the selection and specification of parts according to the respective appli-
cable regulations, the consideration of the system limitations and interface description as
well as the comprehension of the operating limits in every operational state is in the re-
sponsibility of the aircraft manufacturer.
The aircraft manufacturer has to make sure that the operating limits given in the Operators
Manual can be supervised by the pilot. The execution of the installation must allow the op-
eration of the engine according to the Operators Manual.
INSTALLATION OVERVIEW
Figure 8.7: Cooling system schematic
WATER INLET ELBOW
Effectivity: 915 i A Series
Edition 0/Rev. 0
INSTALLATION MANUAL
INSTALLATION NOTES
Expansion tank
1
3
Radiator
5
Overflow bottle
The hoses should be fixed with appropriate clips to prevent loss e.g. with spring type
hose clips, such as those used for the coolant hoses between the water pump and
BRP-Rotax
2
4
6
ATTENTION
cylinder.
Pressure cap
Water pump
Purging
75–00–00
December 01 2017
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