Rotax 912 iS Sport Operator's Manual page 61

Effectivity: 912 i Series
Edition 2 / Rev. 0
Performance graph for non-standard conditions Engine
912 iSc/iS
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 2: Performance graph
Further essential information regarding engine behavior
see Service Letter SL-912 i-003, latest edition.
BRP-Rotax Page 5-3
January 01 2019