CESSNA SECTION 2
MODEL 208B (867 SHP) OPERATING LIMITATIONS
GARMIN G1000
U.S.
FAA APPROVED
FUEL LIMITATIONS
FUEL CAPACITY
TOTAL FUEL
Both Tanks and Reservoir: . . . . . . . . . . .339.1 U.S. Gallons (1283 l)
Both Tanks: . . . . . . . . . . . . . . . . . . . . . .335.6 U.S. Gallons (1270 l)
Each Tank: . . . . . . . . . . . . . . . . . . . . . . . .167.8 U.S. Gallons (635 l)
TOTAL USABLE FUEL
Both Tanks ON and Reservoir: . . . . . . . .335.3 U.S. Gallons (1268 l)
Both Tanks ON: . . . . . . . . . . . . . . . . . . .332.0 U.S. Gallons (1256 l)
Single Tank ON: . . . . . . . . . . . . . . . . . . . .165.0 U.S. Gallons (624 l)
TOTAL UNUSABLE FUEL
Both Tanks ON: . . . . . . . . . . . . . . . . . . . . . . .3.6 U.S. Gallons (13 l)
Single Tank ON: . . . . . . . . . . . . . . . . . . . . . . .2.8 U.S. Gallons (10 l)
Maximum Fuel Imbalance:. . . . . . . . . . . . . . . . . . . .200 Pounds (90 kg)
To achieve full fuel capacity, fill fuel tank to the top of the
filler neck. Filling fuel tanks to the bottom of the fuel filler
collar (level with flapper valve) allows space for thermal
expansion and results in a decrease in fuel capacity of 4.0
U.S. gallons (15 l) per side (8.0 U.S. gallons (30 l) total).
The fuel quantity, fuel used and fuel remaining functions of the G1000
are supplemental information only and must be verified by the pilot.
Continuous uncoordinated flight is prohibited if L FUEL LOW, R FUEL
LOW or L-R FUEL LOW annunciator is shown on PFD.
Unusable fuel quantity will continue to increase the longer a significant
sideslip is maintained.
Due to possible fuel starvation, maximum full rudder sideslip duration is
limited to a maximum of three minutes.
208BPHCUS-00 2-25
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