Rotax 912 i series Installation Manual

d05165.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 0
10-10-00
Page 9
January 01/2012
2.3) Definition of attachment points
General note See Fig. 5.
Graphic Attachment points
Fig. 5

WARNUNG

WARNING
Non-compliance can result in serious injuries or
death!
The aircraft or fuselage manufacturer must design the
engine suspension so that it can safely carry the max-
imum occurring operational loads without exceeding
the max. allowable forces and bending moments on
the engine housing and attachment points.
Tighten all engine suspension screws as specified by
the aircraft manufacturer.

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