STEMME S6-RT, Руководство по эксплуатации самолета, Страница: 202 / 236

7 31 Revision:
Date of Issue: 18. November 2011 Date of Rev.: . .
The inducted air is compressed (and warmed to some extent) in the turbo
charger. Therefore, a carburetor heat system is not necessary because ice will
not form in any flight conditions.
0 "6 Just before reaching the setting for take off power (between
108% and 110% power), the target MAP will rise in a step.
Setting the engine power precisely is not possible anymore.
Instead, periodic oscillations of the control unit and the
engine RPM might occur. Avoid the range between 100%
115% engine power and move through it quickly, when the
throttle is set.
To avoid damage to the engine, the MAP is reduced when the engine RPM is
too high or when the inducted air is too warm.
To monitor the turbo control unit, use the red MAP warning light and the yellow
TCU caution light. When turning ON the electrical system, both lights will go ON
for approx. 1 to 2 sec. during a self test.
# 6 If the self test fails, do not start the engine!
A !! 8 @#= # , "
OFF TCU is operational
FLASHING TCU is NOT operational, for procedures refer to section 3
“Emergency Procedures“.