SOLOY TURBINE PAC
SECTION 4
POHS CESSNA U/TU 206G
NORMAL PROCEDURES
4-4
F.A.A. Approved
October 4, 2005
CHECKLIST PROCEDURES
PREFLIGHT INSPECTION
1.
CABIN
1. Control Wheel Lock – REMOVE.
2. Battery Switch – ON.
3. Fuel Quantity Indicators – CHECK QUANTITY
4. Wing Flaps – DOWN
5. Battery Switch -- OFF
6. Fuel Selector Valve – ON (BOTH if fuel low warning system
installed)
2.
EMPENNAGE
1. Rudder Gust Lock – REMOVE
2. Tail Tie-Down – DISCONNECT
3. Control Surfaces – CHECK freedom of movement and security.
4. Check cargo doors securely latched and locked (right side only).
If cargo load will not permit access to the front cargo door inside
handle, lock the door from the outside by means of the T-handle
stored in the map compartment.
NOTE
The cargo doors must be fully closed and latched
before operating the electric wing flaps. A switch
in the upper door sill of the front cargo door inter-
rupts the wing flap electrical circuit when the front
door is opened or removed, thus preventing the
flaps being lowered with possible damage to the
cargo door or wing flaps when the cargo door is
open. If operating with the cargo doors removed
and the optional spoiler kit installed, check that
the wing flap interrupt switch cover plate is
installed so that the wing flaps can be lowered in
flight.
3.
RIGHT WING Trailing Edge
1. Aileron – CHECK freedom of movement and security.
2. Wing Flaps – CHECK play and security.
UNCONTROLLED
COPY
