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INTRODUCTION CESSNA MODEL 208B G1000 PERFORMANCE - SPECIFICATIONS PASSENGER VERSION * SPEED (KTAS): Maximum Cruise at 10,000 Feet . . . . . . . . . . . . . . . . . . . . 184 Knots Maximum Cruise at 20,000 Feet . . . . . . . . . . . . . . . . . . . . 174 Knots RANGE:With 2224 pounds usable fuel and fuel allowance for engine start, taxi, takeoff, climb, descent and 45 minutes reserve. Max Cruise at 10,000 Feet . . . . . . . . . . . . . . . . . . . Range - 907 NM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 5.1 Hours Max Cruise at 18,000 Feet . . . . . . . . . . . . . . . . . . Range - 1109 NM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 6.6 Hours Max Range at 10,000 Feet . . . . . . . . . . . . . . . . . . Range - 1026 NM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 6.6 Hours Max Range at 18,000 Feet . . . . . . . . . . . . . . . . . . Range - 1163 NM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Time - 7.4 Hours RATE-OF-CLIMB AT SEA LEVEL . . . . . . . . . . . . . . . . . . . . . .975 FPM SERVICE SEALING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23,700 Feet MAXIMUM OPERATING ALTITUDE . . . . . . . . . . . . . . . . . 25,000 Feet TAKEOFF PERFORMANCE: Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1365 Feet Total Distance Over 50 Foot Obstacle . . . . . . . . . . . . . . . 2420 Feet LANDING PERFORMANCE: Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 950 Feet Total Distance Over 50 Foot Obstacle . . . . . . . . . . . . . . . . 1795 Feet STALL SPEED (KCAS): Flaps Up, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 78 Knots Flaps Full, Idle Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 Knots MAXIMUM WEIGHT: Ramp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8785 Pounds Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8750 Pounds Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8500 Pounds STANDARD EMPTY WEIGHT . . . . . . . . . . . . . . . . . . . . . .4511 Pounds Maximum USEFUL LOAD . . . . . . . . . . . . . . . . . . . . . . . . 4274 Pounds iv *Speeds are based on mid-cruise weight. U.S. (Continued Next Page) Revision 1
CESSNA INTRODUCTION MODEL 208B G1000 PERFORMANCE - SPECIFICATIONS PASSENGER VERSION (Continued) WING LOADING . . . . . . . . . . . . . . . . . . . . . . 31.3 Pounds/Square Foot POWER LOADING . . . . . . . . . . . . . . . 13.0 Pounds/Shaft Horsepower FUEL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 335.6 Gallons OIL CAPACITY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 Quarts ENGINE: Pratt & Whitney Canada . . . . . . . . . . . . . . . . . . . PT6A-114A Free Turbine Flat Rated at 675 Shaft Horsepower PROPELLER: McCauley 3-bladed, Constant Speed, Full Feathering, Reversible. Diameter . . . . . . . . . . . . . . . . . 106 Inches NOTE The above performance figures are based on indicated weights, standard atmospheric conditions, level, hardsurfaced dry runways and no wind. They are calculated values derived from flight tests conducted by Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes and numerous factors affecting flight performance. Performance for other operational conditions can be derived by reference to operational data in other sections of this POH/AFM. Revision 1 U.S. v/vi
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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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