Rotax 912 i series Installation Manual

d05780.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 0
00-00-00
page 6
January 01/2012
Auxiliary equip-
ment tested
NOTE: The following equipment is not included as part of the stan-
dard engine version!
The following auxiliary equipment has been tested on ROTAX engine
type 912 i for safety and durability to the standards of aviation.
The furnishing of proof in accordance to the latest FAR or EASA has to be
conducted by the aircraft manufacturer.
- external alternator
- oil cooler with connections
- coolant radiator
- coolant overflow bottle
Auxiliary equip-
ment not tested
The following auxiliary equipment has not been tested on ROTAX
engine type 912 i for safety and durability to the standards of avia-
tion.
- intake filter
- shock mount

WARNUNG
NOTICE
Any equipment not included as part of the standard en-
gine version and so does not be part of the engine is
not in the scope of supply.
Components especially developed and tested for this
engine are readily available at BRP-Powertrain.

WARNUNG

WARNING
Non-compliance can result in serious injuries or death!
The user assumes all risks possibly arising by utilizing
auxiliary equipment.
The furnishing of proof in accordance to the latest FAR
or EASA has to be conducted by the aircraft manufac-
turer.

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