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Rotax 912 i series Service Manual

Rotax 912 i series
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BRP-Rotax
MAINTENANCE MANUAL LINE
Chapter: 05–20–00
SCHEDULED MAINTENANCE CHECKS
TOPICS IN THIS CHAPTER
Scheduled maintenance checks ..............................................................................................................2
Unscheduled maintenance checks..........................................................................................................3
Visual inspection.....................................................................................................................................5
Maintenance schedule procedures (maintenance check list) ..................................................................6
Check List/Maintenance Schedule...........................................................................................................7
Maintenance Schedule ............................................................................................................................9
Introduction The owner and/or user is primarily responsible for the maintenance and airworthiness of
the engine. This includes compliance with all applicable airworthiness directives.
This inspection protocol is not intended to be all-inclusive, for no such protocol can
replace the knowledge and experience of a certified aircraft mechanic. As the party
primarily responsible for the maintenance and airworthiness of the engine, the owner or
user should only have the maintenance work carried out by qualified engineers
(corresponding to the iRMT levels).
Documentation
required
It is the responsibility of the owner and/or user to make sure that the aircraft mechanic
performing the work on the engine has access to the previous Inspection Protocols and
any other required documents.
Effectivity: 912 i Series
Edition 2/Rev. 0
05–20–00
Page 1
September 01/2018

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Rotax 912 i series Specifications

General IconGeneral
Number of Cylinders4
Max Power100 hp (73.5 kW)
Max Power Output RPM5800 rpm
Ignition SystemDual electronic ignition
Oil SystemDry sump, forced lubrication with separate oil tank
Reduction Gear Ratio2.43:1
TBO2000 hours
Engine Type4-stroke, horizontally opposed
Displacement1352 cm³
Bore x Stroke84 mm x 61 mm
Max Torque128 Nm
Fuel TypeAvgas 100LL or unleaded automotive gasoline
Fuel SystemElectronic fuel injection
Cooling SystemLiquid/air-cooled

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