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SECTION 4 CESSNA NORMAL PROCEDURES MODEL 208B G1000 4 LEFT WING Trailing Edge 1. Fuel Tank Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (verify no obstructions) 2. Aileron and Servo Tab. . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (verify condition and security) 3. Static Wicks (4 total) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (verify condition) 4. Spoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (verify condition and security) 5. Flap Leading Edge Vortex Generators . . . . . . . . . . . . . CHECK (verify condition and security) 6. Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (verify condition and security) 4-10 U.S. FAA APPROVED 208BPHBUS-00
CESSNA SECTION 4 MODEL 208B G1000 NORMAL PROCEDURES MEASURED FUEL DEPTH VS. FUEL QUANTITY Universal XL Fuel Quantity Generic Fuel Fuel Quantity Fuel Gage Gage-Inches Gage Scale Gallons Pounds Inches Gallons Pounds 0.50 87.4 585 0.50 88.4 592 0.75 91.1 610 0.75 92.6 621 1.00 94.7 634 1.00 96.7 648 1.25 98.2 658 1.25 100.8 675 1.50 101.8 682 1.50 104.7 702 1.75 105.2 705 1.75 108.6 727 2.00 108.6 727 2.00 112.4 753 2.25 111.9 750 2.25 116.1 778 2.50 115.1 771 2.50 119.7 802 2.75 118.3 793 2.75 123.2 826 3.00 121.5 814 3.00 126.7 849 3.25 124.5 834 3.25 130.1 871 3.50 127.5 855 3.50 133.4 894 3.75 130.5 874 3.75 136.6 915 4.00 133.4 894 4.00 139.7 936 4.25 136.2 912 4.25 142.8 956 4.50 138.9 931 4.50 145.7 976 4.75 141.6 949 4.75 148.6 996 5.00 144.3 966 5.00 151.4 1015 5.25 146.8 984 5.25 154.1 1033 5.50 149.3 1000 5.50 156.8 1050 5.75 151.8 1017 5.75 159.3 1068 6.00 154.1 1033 6.00 161.8 1084 6.25 156.5 1048 6.33 165.0 1105 6.50 158.7 1063 6.75 160.9 1078 7.00 163.0 1092 7.25 165.0 1106 Figure 4-2 FAA APPROVED 208BPHBUS-00 U.S. 4-11
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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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CESSNA SECTION 5 MODEL 208B G1000 P
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CESSNA SECTION 6 MODEL 208B G1000 W
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CESSNA SECTION 7 MODEL 208B G1000 A
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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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