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
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