Rotax 912 Series Operator's Manual

Effectivity: 912 Serie
Edition 4 / Rev. 0
BRP-Rotax Page 5-7
November 01/2016
Performance
graph
Engine 912 S/ULS
Performance graph for non standard conditions
The following graph shows the performance drop with increas-
ing flight altitude. The curves show the performance at 5800,
5500, 5000, 4800 and 4300 rpm, at full throttle.
At deviation of temperature conditions from standard atmos-
phere conditions the engine performance to be expected can
be calculated from the performance indicated, multiplied by
standard temperature, divided by actual temperature in °K.
Figure .6: Performance graph

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