SOLOY TURBINE PAC
SECTION 8
POHS CESSNA T206H/206H
HANDLING, SERVICE &
MAINTENANCE
8-5
F.A.A. Approved
May 23, 2003
3. Install a surface control lock over the fin and rudder.
4. Tie sufficiently strong ropes or chains to the wing and tail tie-
down fittings and secure each rope or chain to a ramp tie-
down.
5. Tie a rope (no chains or cables) to the nose gear torque link
and secure to a ramp tie-down.
6. Tie a rope (no chains or cables) to the propeller and secure
to the airframe to prevent the propeller from windmilling.
7. Install a pitot tube cover.
8. If dusty conditions exist or if the last flight of the day has
been completed, install the engine inlet and exhaust covers.
The covers may be installed after the engines have cooled
down.
JACKING
– No Change
LEVELING
– No Change
FLYABLE STORAGE
1. If the airplane is to be stored temporarily, or indefinitely, refer
to the Airplane and Engine Maintenance Manuals for proper
storage procedures. The Maintenance Manuals provide
amplification for the following procedures:
a. Compressor preservation shall be accomplished as
warranted by local corrosive conditions encountered.
In no case shall the shutdown period exceed five days
without preserving the compressor.
exceed five days without preserving the compressor.
2. Re-preserve at least each thirty days if the aircraft is stored
outdoors and each ninety days if stored indoors.
a. Install covers on the compressor inlet and the exhaust
collector stacks. Covers shall incorporate desiccant
(No. 88 Absorbent Protective Dehydrating Agent, or
equivalent, MIL-D-344). Inspect desiccant for color
change periodically (time period based on
environmental humidity conditions). Rejuvenate
desiccant as necessary to maintain light blue color.
b. Use wedge to hold compressor bleed valve closed.
Also, cover the diffuser vent orifice hole and engine
gearbox overboard vent during storage.
UNCONTROLLED
COPY