Rotax 912 i series Installation Manual

d05781.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 2
24-00-00
Page 6
January 01/2014
NOTE: The battery must be selected so that there is a min. voltage
of 9 V on the ECU during start-up (also in cold weather
conditions). The engine bus voltage is displayed via the
CAN BUS. It can also be displayed using the BUDS Aircraft
diagnostic tool.
NOTE: Whether the required minimum voltage of 9 V is actually
observed (e. g. during engine start) can only be determined
with an oscilloscope.

WARNUNG
NOTICE
It must be remain displayed during the electric starter
operation.
During its first installation in an aircraft model, the volt-
age must be measured at 3 places.
- Battery voltage (separate voltmeter)
- Voltage on electric starter (separate voltmeter)
- Engine bus voltage (displayed in BUDS diagnostic
tool or on display).

WARNUNG
NOTICE
The connection from the battery to the EMS system
must be kept separate from the one to the starter relay
in order to avoid unnecessary voltage drop.

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