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SECTION 1 CESSNA GENERAL MODEL 208B G1000 FUEL (Continued) NOTE Refer to Section 8 for allowable concentrations of the above additives and additional information. Fuel Capacity: Total Capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . 335.6 U.S. Gallons Total Capacity Each Tank . . . . . . . . . . . . . . . . . . 167.8 U.S. Gallons Total Usable . . . . . . . . . . . . . . . . . . . . . . . . . . . . 332.0 U.S. Gallons OIL Oil Grade (Specification): Oil conforming to Pratt & Whitney Engine Service Bulletin No. 1001, and all revisions or supplements thereto, must be used. Refer to Section 8 for a listing of approved oils. Total Oil Capacity: . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 U.S. Quarts (including filter, cooler, and hoses) Drain and Refill Quantity . . . . . . . . . . . . . . . . . . . . . .9.5 U.S. Quarts (approximately) Oil Quantity Operating Range: Fill to within 1 1/2 quarts of MAX HOT or MAX COLD (as appropriate) on dipstick. Quart marking indicate U.S. quarts low if oil is hot. For example, a dipstick reading of 3 indicates the system is within 2 quarts of MAX if the oil is cold and within 3 quarts of MAX if the oil is hot. WARNING 1-8 Make sure oil dipstick cap is securely latched down. Operating the engine with less than the recommended oil level and with the dipstick cap unlatched will result in excessive oil loss and eventual engine stoppage. U.S. (Continued Next Page) 208BPHBUS-00
CESSNA SECTION 1 MODEL 208B G1000 GENERAL OIL (Continued) NOTE To obtain an accurate oil level reading, it is recommended the oil level be checked within 10 minutes after engine shutdown while the oil is hot (MAX HOT marking) or prior to the first flight of the day while the oil is cold (MAX COLD marking). If more than 10 minutes has elapsed since engine shutdown and engine oil is still warm, perform an engine dry motoring run before checking oil level. MAXIMUM CERTIFICATED WEIGHTS Ramp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8785 Pounds Takeoff. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8750 Pounds Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8500 Pounds NOTE Refer to Section 6 of this POH/AFM for recommended loading arrangements. CABIN AND ENTRY DOOR DIMENSIONS Detailed dimensions of the cabin interior and entry door openings are illustrated in Section 6. BAGGAGE/CARGO COMPARTMENT AND CARGO DOOR ENTRY DIMENSIONS Detailed dimensions of the baggage/cargo area and cargo door openings are illustrated in Section 6. SPECIFIC LOADINGS Wing Loading . . . . . . . . . . . . . . . . . . . . . . 31.3 Pounds/Square Foot Power Loading . . . . . . . . . . . . . . . . 13.0 Pounds/Shaft Horsepower 208BPHBUS-00 U.S. 1-9
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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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