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SECTION 2 CESSNA LIMITATIONS MODEL 208B G1000 FUEL LIMITATIONS NOTE To achieve full 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 four gallons per side (eight gallons total). With low fuel quantity (FUEL LOW CAS MSG(s) ON), continuous uncoordinated flight is prohibited. Unusable fuel quantity increases when more severe sideslip is maintained. Due to possible fuel starvation, maximum full rudder sideslip duration time is three minutes. Maximum fuel unbalance in flight is 200 pounds. Fuel Grade (Specification) and Fuel Additives: 2-24 U.S. CAUTION Aviation gasoline is restricted to emergency use and shall not be used for more than 150 hours in one overhaul period; a mixture of one part aviation gasoline and three parts of Jet A, Jet A-1, JP-1, or JP-5 may be used for emergency purposes for a maximum of 450 hours per overhaul period. (Continued Next Page) FAA APPROVED 208BPHBUS-00
CESSNA SECTION 2 MODEL 208B G1000 LIMITATIONS FUEL LIMITATIONS (Continued) Fuel Grade Specification and Fuel Additives Refer to Section 8 for Figure 2-7 additional approved additives and concentrations. FAA APPROVED 208BPHBUS-00 U.S. 2-25
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CESSNA INTRODUCTION MODEL 208B G100
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Page 15 and 16: CESSNA SECTION 1 MODEL 208B G1000 G
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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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