Effectivity: 912 S/ULS BRP-Powertrain page 5-7
OM Edition 2 / Rev. 0 April 01/2010
d04677.fm
Performance
graph
Engine 912 S/ULS
Performance graph for non-standard conditions
The following graph shows the performance drop with increasing
flight altitude. The curves show the performance at 5800, 5500,
5000, 4800 and 4300 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. 6
08636
To Next Page
Loading...
