Rotax 912 Series Installation Manual

d04925.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
76-00-00
page 7
August 01/2012
See also the relevant instructions of the instrument supplier/aircraft man-
ufacturer for correct connection and wiring.
Graph current
over pressure
See Fig. 3.
Graphic Oil pressure sensor
Fig. 3 08379,08442

WARNUNG
NOTICE
The graph current over pressure (2) has been deter-
mined, and is effectiva at the following conditions only:
Ambient temperature: 20 °C (68 °F)
Tolerance: Max ±3 %
Part Function
1 Oil pressure sensor
2 Graph current over pressure sensor
0
5
10
15
20
25
246810
(bar)
(mA)
1
2

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