Rotax 912 i series Installation Manual

d05781.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 2
24-00-00
Page 3
January 01/2014
1) Requirements for the circuit wiring
General note
NOTE: Follow the relevant building regulations (licensing condi-
tions) of the maintenance staff, during manufacturing of
the wiring harness and repairs or modifications of the air-
craft.

WARNUNG
NOTICE
The connections have to be made by the aircraft man-
ufacturer in accordance with applicable regulations
and the enclosed wiring diagram.
See chap. 24-00-00 section:
Switch requirements and warning lamps.

WARNUNG
NOTICE
The power supply to the various consumers (e.g. bat-
tery) must be adequately protected by fuses. Using in-
correctly rated fuses may result in destruction of the
equipment.
Under no circumstances must consumer cables (e.g.
battery) be routed alongside the ignition cable. There
is a risk of electromagnetic interference or damage.

WARNUNG
NOTICE
Do not bend, kink, pinch or otherwise improperly
stress the wiring harness. Use proper routing, clamp-
ing and strain relief on wiring harnesses.

Rotax 912 i series Specifications

General

Number of Cylinders	4
Max Power	100 hp (73.5 kW)
Max Power Output RPM	5800 rpm
Ignition System	Dual electronic ignition
Oil System	Dry sump, forced lubrication with separate oil tank
Reduction Gear Ratio	2.43:1
TBO	2000 hours
Engine Type	4-stroke, horizontally opposed
Displacement	1352 cm³
Bore x Stroke	84 mm x 61 mm
Max Torque	128 Nm
Fuel Type	Avgas 100LL or unleaded automotive gasoline
Fuel System	Electronic fuel injection
Cooling System	Liquid/air-cooled