Rotax 912 Series Installation Manual

d04920.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
24-00-00
page 3
August 01/2012
1) Requirements for the circuit wiring
General note

WARNUNG
NOTICE
The connections have to be made by the aircraft man-
ufacturer in accordance with applicable regulations
and the enclosed wiring diagram.
See chap. 24-00-00 section: Switch requirements.

WARNUNG
NOTICE
The power supply to the various consumers (e.g. bat-
tery) must be adequately protected by fuses. Using in-
correctly rated fuses may result in destruction of the
equipment.
Under no circumstances must consumer cables (e.g.
battery) be routed alongside the ignition cable. There
is a risk of electromagnetic interference or damage.

WARNUNG
NOTICE
Do not bend, kink, pinch or otherwise improperly stress
the wiring harness. Use proper routing, clamping and
strain relief on wiring harnesses.

Rotax 912 Series Specifications

General

Redline	5800 rpm
TBO	2000 hours
Displacement	1211 cc
Bore	79.5 mm
Stroke	61 mm
Power Output	80 hp (59.6 kW)
Compression Ratio	9.0:1
Fuel Type	Avgas 100LL
Ignition System	Dual electronic ignition
Fuel System	Fuel Injected
Oil System	Dry sump
Engine Type	4-cylinder, horizontally opposed, 4-stroke