SOLOY TURBINE PAC
SECTION 2
POHS CESSNA T206H/206H
LIMITATIONS
2-10
F.A.A. Approved
November 14, 2014
C. Engine alternate air must be on while operating in falling or
blowing snow regardless of ambient temperature.
D. Engine inlet anti-ice may be turned off when alternate air is
on.
CAUTION
THE ENGINE ALTERNATE AIR SYSTEM MUST BE
OPERATED IN THE ABOVE MENTIONED
CONDITIONS EVEN IF THERE IS NO VISIBLE SIGN
OF AIRFRAME ICE AND/OR SNOW
ACCUMULATION.
Deactivation of the system shall not be made until the above mentioned
conditions no longer exist and all accumulated airframe ice and/or snow has
dissipated.
CAUTION
SIGNIFICANT POWER LOSS (10 PSI TORQUE)
WILL OCCUR WHILE OPERATING IN THE
ALTERNATE AIR MODE. EXTREME CAUTION
SHOULD BE USED TO MAINTAIN A MINIMUM
OF 14 PSI TORQUE IN FLIGHT ON APPROACH
TO LANDING.
FUEL LIMITATIONS
Valve must be on BOTH for takeoff, landing or uncoordinated flight
maneuvers.
Total Fuel:
92 U.S. Gallons (2 tanks at 46.0 gallons each)
Usable Fuel:
88.0/87.0 U.S. Gallons *
Unusable Fuel:
4.0 U.S. Gallons (2.0 gallons each tank)
*
For Model 206H from S/N 20608174 & on, usable fuel is 87 gal.
For Model T206H from S/N T20608362 & on, usable fuel is 87 gal.
NOTE
To ensure maximum fuel capacity and minimize cross-
feeding when refueling, always park the airplane in a wings-
level, normal ground attitude and place the fuel selector in
the LEFT or RIGHT position. Refer to Figure 1-1 for normal
ground attitude definition.
UNCONTROLLED
COPY