SOLOY TURBINE PAC
SECTION 4
POHS CESSNA T206H/206H
NORMAL PROCEDURES
4-20
F.A.A. Approved
November 17, 2015
Prior to engine run-up, set parking brake ON. Check that all doors and
windows are closed and that the passenger’s seat belts and shoulder
harnesses are secure.
Check fuel quantity and temperature. Refer to limitations section for
restrictions. Check that the engine instruments are normal and the flight
controls are free and correct. Set the propeller control fully forward. Trim
should be set to the TAKEOFF position.
Set the power control to GROUND IDLE.
CAUTION
AVOID CONTINUOUS OPERATION (>60 SECONDS)
BETWEEN 1358 RPM AND 1630 RPM PROPELLER
SPEED AT TORQUE SETTING GREATER THAN 20
PSI
To test the auto feather system, press the propeller overspeed governor
switch and hold. The AUTO FEATHER light will illuminate. Gradually
push the power control and observe an increase in torque pressure with
little or no change in NP. Pull power control aft, then release governor
switch. The AUTO FEATHER light will extinguish.
Check that the suction gauge is reading within limits.
CAUTION
BE PREPARED FOR A SURGE IN POWER AS THE
PROPELLER BLADES MOVE TO A GREATER
PITCH ANGLE.
The operation of the alternate engine air system should be checked daily
especially after the cowling has been removed.
NOTE
A drop in torque and a rise in TOT is normal with the
actuation of the engine ice protection system.
Reduce power control back to GROUND IDLE.
Check and set flight instruments and radios as desired. Be sure that the
autopilot is OFF for takeoff. Check that the normal static source is
selected. Check that necessary lights and electrical systems are ON,
including ice protection systems if weather conditions warrant.
UNCONTROLLED
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