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SECTION 7 CESSNA AIRPLANE AND SYSTEMS DESCRIPTION MODEL 208B G1000 7-64 U.S. FUEL SYSTEM Figure 7-10 208BPHBUS-00
CESSNA SECTION 7 MODEL 208B G1000 AIRPLANE AND SYSTEMS DESCRIPTION UNITS OF MEASURE POUNDS GALLONS (U.S.) UNITS OF MEASURE FUEL QUANTITY DATA FUEL QUANTITY DATA FUEL LEVEL (QUANTITY EACH TANK) FULL (OUTBOARD FILLERS) 1124.25 167.8 FUEL LEVEL (QUANTITY EACH TANK) TOTAL FUEL 2248.5 335.6 TOTAL FUEL TOTAL UNUSABLE 24.1 3.6 TOTAL UNUSABLE U.S. TOTAL USABLE ALL FLT CONDITIONS 2224.4 332 TOTAL USABLE ALL FLT CONDITIONS NOTE Pounds are based on a fuel specific weight of 6.7 pounds per U.S. gallon. WARNING To achieve full capacity, fill fuel tank to the top of the fuel filler neck. Filling fuel tanks to the bottom of the fuel filler collar (level with the flapper valve) allows space for thermal expansion and results in a decrease in fuel capacity of four gallons per side (eight gallons total). Figure 7-11 208BPHBUS-00 7-65
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CESSNA INTRODUCTION MODEL 208B G100
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CESSNA SECTION 1 MODEL 208B G1000 G
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CESSNA SECTION 2 MODEL 208B G1000 L
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SECTION 3 CESSNA EMERGENCY PROCEDUR
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SECTION 3 CESSNA ABNORMAL PROCEDURE
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CESSNA SECTION 3 MODEL 208B G1000 A
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CESSNA SECTION 4 MODEL 208B G1000 N
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CESSNA SECTION 5 MODEL 208B G1000 P
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CESSNA SECTION 6 MODEL 208B G1000 W
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SECTION 7 CESSNA AIRPLANE AND SYSTE
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CESSNA SECTION 8 MODEL 208B G1000 H
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