Rotax 912 i series Installation Manual

d05781.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 2
24-00-00
Page 30
January 01/2014
Legend
Scope of deliv-
ery
Graphic EMS Wiring diagram. See also Page 31.
Wiring power side. See also 32.
Wiring power side (optional). See also 33.
Wiring HIC Switch and warning lamp. See also 34.
R
iBatt
Internal resistance battery
R
CStarter relay
Contact resistance starter relay
R
L
Line resistance
R
Other
Any other resistors (e.g. Master relays, contact resistance)

WARNUNG
NOTICE
Items/components which are not included in the stan-
dard engine scope of delivery must be certified the
aircraft or fuselage manufacturer in accordance with
the latest regulations, such as FAR or EASA.

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