FLIGHT MANUAL TSA-M, VARIANT S6
Doc.-No.: P400-006.000 E
Page: 7-25
Revision: ---
Date of Issue: 07. October 2008
Date of Rev.: --.--.----
The inducted air is compressed (and warmed to some extent) in the turbo-
charger. Therefore, a carburator-heat-system is not necessary because ice will
not form in any flight-conditions.
Warning:
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.
Caution:
If the self-test fails, do not start the engine!
Yellow TCU-Caution-Light
OFF
TCU is operational
FLASHING TCU is NOT operational, for procedures see chapter 3 „Emergency
Procedures“
