Rotax 912 ULS 3 Operator's Manual page 56

Performance data
Engine 912 A/F/UL
Effectivity: 912 A/F/UL
OM Edition 2 / Rev. 0
Performance data variable pitch propeller
The following graph shows the performance drop with increasing
flight altitude. The curves show the performance at 5800, 5500,
5000, 4500 and 4000 rpm, at full throttle.
The engine allows operation with fully open throttle valve over the
whole rpm range, without limitation. But full throttle performance
above 5500 rpm is limited to 5 minutes.
At deviation of temperature conditions from standard atmosphere
conditions the engine performance to be expected can be calcu-
lated from the performance indicated, multiplied by standard tem-
perature, divided by actual temperature in K.
Fig. 3
BRP-Powertrain
08635
page 5-4
April 01/2010