BRP-Rotax
MAINTENANCE MANUAL
3 The engine assembly as per supply volume. Additionally all added-on parts
as in the supply volume such as filters, intake silencer, fuel pump, external
generator, sensors, ignition unit, electric starter, oil tank.
4
Indication of total engine operating hours (TSN) and where applicable, en-
gine operating hours since a previous overhaul (TSO). NOTE: This informa-
tion must be supplied to allow the service history of components to be
traced.
5
ECU incl. a statement of the number of times it has been plugged in/
unplugged.
6
FUSE BOX incl. a statement of the number of times it has been plugged in/
unplugged.
7
Harness incl. a statement of the number of times it has been plugged in/
unplugged.
8
Data about the type of aircraft used.
9
Useful remarks and observations concerning the engine.
TIME LIMIT FOR PARTS
General note
ATTENTION
This time limit must be followed independently and in addition to the visual in-
spections (see Chapter 05-20-00 section: Visual Inspection) of the respective
components.
Time limit The following components and systems must be replaced every 5 years:
• All rubber hoses of the cooling system (except GENUINE ROTAX® silicon hoses),
which need to be checked by "on-condition" maintenance according to the instructions
of continued airworthiness.
• All rubber hoses of the lubrication system which are part of the engine supply volume
and if they are not in the maintenance schedule of aircraft manufacturer
• Connecting hose of the air intake system
• V-belt
• Fuel pressure regulator assy. (only pressure regulator, not pressure regulator housing)
• Air intake hose (connection between turbocharger and airbox)
Effectivity: 915 i A Series
Edition 0/Rev. 0
05–10–00
Page 5
December 01 2017
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