Rotax 915 i A series Maintenance Manual page 99

Installation-related point
See "Documentation of aircraft manufacturer".
See relevant Maintenance Manual Line Chapter
12–20–00 Planned maintenance.
Checking the engine for contamination and
damage.
See relevant Maintenance Manual Line 05–00–00
Maintenance.
Installation of the engine and its components.
See also Chapter 71–00–00 section Power plant.
Control unit (ECU) connections checked for se-
cure connection. Connector lock!
See also Chapter 71–00–00 section Power plant.
Laying of wiring harness checked.
Grounding cable checked according to aircraft
manufacturer's specifications. Allocation checked.
See documentation of aircraft manufacturer.
Fuel pump connection checked.
See also Chapter 71–00–00 section Power
Fuel system checked for leaks.
See relevant Maintenance Manual Line Chapter
12–20–00
Fuel filter checked for blockages.
See relevant Maintenance Manual Line Chapter
12–20–00.
Propeller installed according to the aircraft manu-
facturer's and propeller manufacturer's
specifications.
See "Documentation of aircraft manufacturer".
Lubrication system filled.
To do this, see relevant Maintenance Manual Line
Chapter 12–10–00 section Adding operating
fluids.
Engine test run/functional test.
See relevant Maintenance Manual Line Chapter
12–20–00.
General notes/remars:
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Effectivity: 915 i A Series
Edition 0/Rev. 0
BRP-Rotax
MAINTENANCE MANUAL HEAVY
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71–00–00
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August 01 2018