ULPOWER UL260i - Standard operation; Daily;Pre-flight checks; Engine start

Operating Manual ULPOWER UL260i UL260iF UL260iS UL260iSA
MO 260A01 Revision No: 6 Date: 2014-09-15 Page: 15 of 22
At deviation of temperature conditions from standard atmosphere conditions the engine
performance to be expected can be calculated from the performance indicated, multiplied by
standard temperature in °K, divided by actual temperature in °K.
P
actual
= P
standard
. ( T
standard
/ T
actual
)
T
[°K]
= t
[°C]
+ 273.15