SOLOY TURBINE PAC
SECTION 2
POHS CESSNA T206H/206H
LIMITATIONS
2-12
F.A.A. Approved
November 17, 2015
COLD WEATHER FUEL ALTITUDE RESTRICTIONS
When using any cold weather fuel the maximum flight altitude is
restricted to:
(A) 6,000 feet with a fuel temperature of 110ºF (43.3ºC)
(B) 20,000 feet with a fuel temperature of 40ºF (4.4ºC)
FUEL ADDITIVE
For flight at ambient temperatures of 40
F and below, the fuel used
in this aircraft MUST have an anti-icing additive in compliance with
MIL-DTL-85470B, incorporated or added into the fuel during
refueling in accordance with the additive manufacturer’s
instructions.
CAUTION
PROPER MIXING OF THE ANTI-ICING ADDITIVE WITH
FUEL IS EXTREMELY IMPORTANT BECAUSE
CONCENTRATION IN EXCESS OF THAT
RECOMMENDED (0.15% BY VOLUME) WILL RESULT
IN DETRIMENTAL EFFECTS TO THE FUEL TANKS.
ASSURE THAT THE FUEL ADDITIVE IS DIRECTED
INTO AND BLENDING WITH FLOWING FUEL FROM
THE FUELING NOZZLE. DO NOT ALLOW
CONCENTRATED ADDITIVE TO CONTACT THE FUEL
CELL OR AIRPLANE FINISH. SOME FUELS HAVE
ANTI-ICING ADDITIVES PREBLENDED IN THE FUEL
AT THE REFINERY, SO NO ADDITIONAL ADDITIVES
SHOULD BE ADDED.
Refer to Section 8, Handling, Service & Maintenance for further
information.
NOTE
Fuel containing Tri-Cresyl-Phosphate (TCP)
additives shall not be used.
UNCONTROLLED
COPY