Rotax 915 i A SERIES Maintenance Manual

BRP-Rotax
MAINTENANCE MANUAL
Complete inspection of these components:
• power supply • cooling system
• gearbox • valve train system
• engine suspension frame • exhaust system
• fuel system • lubrication system
• cylinder unit • start system
In most cases an overhaul is necessary, in this regard send the engine without delay to an
authorized ROTAX® overhaul facility for inspection.
If an engine was submerged into water, all electrical components
(e. g.: electric fuel pumps, ignition coils, stators, spark plugs, spark plug connectors, FUSE
BOX, sensors, ECU, wiring harness) must be replaced.
NNOOTTEE
Discoloration or corrosion are signs of submerging in water.
INSPECTION IN EXTREME CLIMATIC CONDITIONS
General note
ATTENTION
Every 25 hr. checks of air filter, coolant radiator and oil cooler are necessary.
Flying in deserts or areas with heavily contaminated or dusty air causes increased wear
on all components. For this reason, shorter maintenance intervals are recommended.
Flying in areas with extreme climatic conditions or in extreme altitudes requires adjust-
ment of the cooling system. To do this, it is necessary to contact the aircraft manufacturer
and an authorized ROTAX® aircraft engines distributor.
DIMINISHED FUNCTIONAL CAPABILITY OF EMS
General note
NNOOTTEE
The diminished functional capability of EMS must be entered by the pilot into the
engine log book, stating duration extant of diminished functional capability and all
pertinent details.
• Perform engine inspection.
05–50–00
Page 16
December 01 2017
Effectivity: 915 i A Series
Edition 0/Rev. 0

Rotax 915 i A SERIES Specifications

General

Brand	Rotax
Model	915 i A SERIES
Category	Engine
Language	English