Rotax 912 i series Installation Manual

d05781.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 2
24-00-00
Page 20
January 01/2014
5.1) Fitting the Faston connector to the Harness Interface Connector
General note See Fig. 10.
NOTE: Faston connectors (1) are supplied loose. The Faston con-
nectors and connector receptacles for the airframe are in-
cluded in the scope of delivery.
Special tools The following special tools and equipment are necessary for fitting the
Faston connector.
Procedure Fitting the Faston cnnector
NOTE: The TPA pin holder must not be pressed pushed with ex-
cessive force.
Part number Description
n.a. MOLEX Crimping crap 64016-0035/63811-4400
n.a. MOLEX Disassembly tool 63813-1500
Step Procedure
1 Strip cable (2) as required (A).
2 Use suitable crimping crap (3) to fit the Faston connector (B).
3 Press down white integral terminal position assurance (TPA) with needle nose
pliers until audible click is heard.
4 Push the Faston connector in the corresponding slot (4) of the Harness Inter-
face Connector receptacle until it is locked in place (C).
5 Check for tight fit.

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