SOLOY TURBINE PAC
SECTION 8
POHS CESSNA U/TU 206G
HANDLING, SERVICE &
MAINTENANCE
8-6
F.A.A. Approved
November 17, 2015
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-3464). 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.
c. Accomplish fuel system preservation. If the engine will
be stored for over 45 days, re-preserve at least each 90
days if stored outdoors and each 180 days if stored
indoors.
CAUTION
RED TAG THE POWER CONTROL
AFTER ANY PRESERVATION HAS
BEEN MADE.
SERVICING
NOTE
Refer to the Airplane and Engine
Maintenance Manuals for complete
servicing requirements.
ENGINE OIL
The oil specifications listed in Table I are compliant with the engine
manufacturer’s requirements. These oil specifications are approved
for use in the Soloy Turbine Pac 780-1000-1 engine. Refer to the Soloy
Turbine Pac 780-1000-1 Maintenance and Overhaul Manual S1014T
for the most current listing of oils and limitations.
UNCONTROLLED
COPY