FLIGHT MANUAL TSA-M, VARIANT S6
Doc.-No.:P400-006.000 E
Page: 4-25
Revision: 1
Date of Issue: 07. October 2008
Agency approved
Date of Rev.: 28.01.2011
1. Engine-master-switch
ON
2. Propeller-RPM
SET propeller-RPM to 2100 RPM
3. Propeller-switch
left switch MANU, right switch HIGH
RPM
Note: propeller reaches full pitch
after 90 seconds
4. Fuel-shut-off-valve
OPEN
5. TCU-self-test
CHECK if red MAP-warning-light and
yellow TCU-caution-light go ON for
approx. 1 -2 seconds and than go
OFF again
6. Cowl-flaps
fully OPEN
7. Fuel-gauges
CHECK
8. Fuel-pressure
CHECK if red warning-light is OFF,
fuel-pressure-gauge 2.5 ±1.0 (250 ±
100 hPa) / 3.6 ± 1.5 psi.
If necessary, ACTIVATE auxiliary-
fuel-pump
9. Choke
fully OPEN if engine is cold (oil-temp.
< approx. 120°F / 50°C)
fully CLOSED if engine is warm (oil-
temp. > approx. 120°F / 50°C)
10. Throttle
IDLE if engine is cold
(oil-temp. < approx. 120°F / 50°C)
approx. 10% THROTTLE if engine is
warm
(oil-temp. > approx. 120°F / 50°C)
11. Indication-light of propeller-T/O-
position
WAIT for green LIGHT is ON, then
left propeller switch AUTO,
right propeller switch STOP
propeller speed 2100 RPM
12. Ignition-switch
a) Windmilling propeller :
only BOTH
b) Propeller has stopped: START
until engine starts to run,
then BOTH,
Note:
The ignition is activated only approx. 2 seconds after
operating the ignition-switch. Do not activate the engine-
starter for more than 10 seconds, then allow a 2 minute
break.