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SECTION 4 CESSNA NORMAL PROCEDURES MODEL 208B G1000 TAXIING 1. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK NOTE Propeller BETA range can be used during taxi with minimum blade erosion up to the point where Ng increases (against beta range spring) to control taxi speed and improve brake life. 2. Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK BEFORE TAKEOFF 1. PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 2. Seats, Seat Belts, Shoulder Harnesses . . . . CHECK SECURE 4-22 U.S. WARNING Failure to correctly use seat belts and shoulder harnesses can result in serious or fatal injury in the event of an accident. 3. Flight Controls . . . . . . . . . . . . . . . . . . . . . FREE and CORRECT 4. Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 5. Altimeters: a. PFD 1 and 2 BARO . . . . . . . . . . . . . . . . . . . . . . . . . . . SET b. Standby Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 6. ALT SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 7. Standby Flight Instruments . . . . . . . . . . . . . . . . . . . . . . CHECK 8. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM 9. FUEL TANK SELECTORS . . . . . . . . . . . . . . . . . . . . BOTH ON 10. FUEL QTY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 11. FUEL SHUTOFF Knob . . . . . . . . . . . . . . . . . . . . . . . FULLY ON 12. ELEVATOR, AILERON, and RUD TRIM Controls. . . . . . . 3 SET (for takeoff) 13. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 400 FT-LBS a. BUS VOLTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK b. INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . . . CHECK Turn control counterclockwise, pull to BYPASS position and check torque drop; move control back to NORMAL position and check that original torque is regained. c. EIS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK See Section 2, Limitations for minimum oil temperature required for flight. (Continued Next Page) FAA APPROVED 208BPHBUS-01
CESSNA SECTION 4 MODEL 208B G1000 NORMAL PROCEDURES BEFORE TAKEOFF (Continued) 14. Overspeed Governor . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (first flight of the day and after maintenance) a. PROP RPM Lever . . . . . . . . . . . . . . . . . MAX (full forward) b. OVERSPEED GOVERNOR TEST Button . . . . . . . . . . . . . . . . . . . PRESS and HOLD c. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE (propeller RPM stabilize at 1750 ±60 RPM) d. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE e. OVERSPEED GOVERNOR TEST Button . . . . . RELEASE 15. Quadrant Friction Lock . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST 16. Standby Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (first flight of the day and before all flights into known icing conditions) a. ENGINE Softkey. . . . . . . . . . . . . . . . . . . SELECT SYSTEM b. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . ON c. GEN AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOAD (to approximately 30 amps) Generator load can be increased by using the TAXI/RECOG Lights. Do not exceed 60 amps. d. ALT AMPS . . . . . . . . VERIFY (alternator output near zero) e. GENERATOR Switch . . . . . . . . . . . . . . . . . . . . . . . . . . TRIP f. ALT AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY LOAD g. BUS VOLTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (for alternator output and voltage approximately one volt less than with generator ON) NOTE A fully charged battery will carry part of the electrical load when initially switching from generator to standby alternator power because of the generator’s higher voltage regulation. h. STBY PWR ON CAS MSG . . . . . . . . . . . . . . . CHECK ON (verify GENERATOR OFF CAS MSG ON) i. GENERATOR Switch . . . . . . . . . . . . . . . . . . . . . . . . RESET (verify GENERATOR OFF CAS MSG OFF) j. STBY PWR ON CAS MSG . . . . . . . . . . . . . . CHECK OFF k. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . OFF (verify STBY PWR INOP CAS MSG ON) l. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . ON (Continued Next Page) FAA APPROVED 208BPHBUS-01 U.S. 4-23
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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 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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