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Rotax 912 i series Operator's Manual

Rotax 912 i series
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Effectivity: 912 i Series BRP-Powertrain page 4-1
OM Edition 1/Rev. 0 January 01/2012
d05873.fm
4) Abnormal operation
Introduction
NOTE: Further checks - see Maintenance Manual.
Table of contents This chapter of the Operators Manual contains expanded operat-
ing and maintenance instruction at abnormal operation.
WARNU
WARNING
Non-compliance can result in serious injuries
or death!
At unusual engine behaviour conduct checks
as per Maintenance Manual Line Chapter
05-50-00 before the next flight.
Subject Page
Fault indicated by the EMS lamps
EMS lamps
EMS lamps operating states
Page 4-2
Page 4-2
Page 4-2
Engine not responding to power inputs Page 4-3
Occurence of uncharacteristic and server engine vibra-
tions
Page 4-3
Re-Start during flight Page 4-3
Failure of the EMS power supply Page 4-3
Exceeding max. admissible engine speed Page 4-3
Exceeding of max. coolant temperature Page 4-4
Exceeding of max. admissible oil temperature Page 4-4
Oil pressure below minimum - during flight Page 4-4
Oil pressure below minimum - on ground Page 4-4
Oil pressure above permitted range at low ambient tem-
peratures
Page 4-5
Engine on fire or fire in the engine compartment Page 4-5
Fuel pressure outside range Page 4-5
Maximum permissible exhaust temperature exceeded Page 4-6
EMS voltage supply below the minimum required level Page 4-6
The sprag clutch decouples not from the starter Page 4-6
Trouble shooting
Table of content
Page 4-7
Page 4-7

Table of Contents

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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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