SOLOY TURBINE PAC
SECTION 2
POHS CESSNA U/TU 206G
LIMITATIONS
2-11
F.A.A. Approved
November 17, 2015
MINIMUM FUEL
Due to the possibility of fuel starvation, takeoff or steep climbs at speeds
below V
y
(86 KIAS at sea level) with either fuel quantity gauge indicating
in the yellow arc (1/8 fuel quantity), or if installed FUEL LOW lights are
on, are prohibited.
If installed, illumination of a FUEL LOW light will be handled as follows:
LEFT FUEL LOW – ON
Switch to RIGHT tank.
FUEL CONFIG light illuminated.
RIGHT FUEL LOW – ON
Switch to LEFT tank.
FUEL CONFIG light illuminated.
Both FUEL LOW – ON
Switch to BOTH and
land as soon as practical.
APPROVED FUEL GRADES
(1) PRIMARY FUELS
(A) MIL-T-5624 Grade JP-5.
(B) MIL-T-83133 Grade JP-8.
(C) ASTM D-1655, Jet A or A1.
(D) JP-1 Fuel Conforming to ASTM D-1655, Jet A.
(E) Diesel #1 Fuel Conforming to ASTM D-1655, Jet A.
(2) COLD WEATHER FUELS
To assure consistent starts below 4
C (40
F), the following fuels may be
necessary:
(A) MIL-T-5624, Grade JP-4.
(B) ASTM D-6615, Jet B.
(C) AVGAS/JET A, JET A1, or JP-5 Mixture.
COLD WEATHER FUEL ALTITUDE RESTRICTIONS
The maximum flight altitude is restricted to 8,000 feet when using any
cold weather fuel and the fuel temperature is 4ºC or above.
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.
UNCONTROLLED
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