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SECTION 4 CESSNA NORMAL PROCEDURES MODEL 208B G1000 CRUISE 1. Ice Protection (if installed) . . . . . . . . . . . . . . . . . AS REQUIRED a. PITOT/STATIC HEAT . ON (when OAT is below 5°C (41°F)) b. STALL HEAT. . . . . . . . ON (when OAT is below 5°C (41°F)) c. PROP HEAT . . . . . . . . ON (when OAT is below 5°C (41°F)) 2. INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 3. PROP RPM Lever . . . . . . . . . . . . . . . . . . . . 1600 to 1900 RPM 4. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET (observe Maximum Cruise ITT and N g limits) Refer to Cruise Performance and/or Cruise Maximum Torque charts in Section 5. 5. Fuel Balance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (maximum 200 pounds imbalance) NOTE Engine operations which exceed 740°C ITT can reduce engine life. CAUTION For every 10° below -30°C ambient temperature, reduce maximum allowable Ng by 2.2%. DESCENT 1. Ice Protection (if installed) . . . . . . . . . . . . . . . . . AS REQUIRED a. PITOT/STATIC HEAT . ON (when OAT is below 5°C (41°F)) b. STALL HEAT. . . . . . . . ON (when OAT is below 5°C (41°F)) c. PROP HEAT . . . . . . . . ON (when OAT is below 5°C (41°F)) 2. INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 3. NO SMOKE/SEAT BELT SIGN Switches (if installed). . . . . . ON 4. Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 5. NAV Source. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECT 4-28 NOTE The overspeed warning horn and MAXSPD annunciation will activate when either PFD1 or PFD2 airspeed reaches greater than 175 KIAS. In addition, the overspeed warning horn and MAXSPD annunciation may appear prior to 175 KIAS if the aircraft is accelerating at a rate that will rapidly exceed VMO. U.S. (Continued Next Page) FAA APPROVED 208BPHBUS-01
CESSNA SECTION 4 MODEL 208B G1000 NORMAL PROCEDURES DESCENT (Continued) CAUTION Set PROP RPM Lever at 1900 RPM prior to beginning any instrument approach procedure. 6. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED BEFORE LANDING NOTE Refer to Landing Distance chart in Section 5 for anticipated ground roll and total distance requirements. 1. Seats, Seat Belts, Shoulder Harnesses . . . . . . . . . . . SECURE WARNING Failure to correctly use seat belts and shoulder harnesses could result in serious or fatal injury in the event of an accident. 2. FUEL TANK SELECTORS . . . . . . . . . . . . . . . . . . . . BOTH ON 3. FUEL CONDITION Lever . . . . . . . . . . . . . . . . . . . . . HIGH IDLE 4. PROP RPM Lever. . . . . . . . . . . . . . . . . . . . . MAX (full forward) 5. Radar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBY 6. AP/YD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (before 200 feet AGL on approach or 800 feet AGL) 7. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET LANDING NORMAL LANDING 1. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL 2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75-85 KIAS 3. Touchdown . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST 4. POWER Lever . . . . . . . BETA RANGE AFTER TOUCHDOWN 5. Brakes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY FAA APPROVED 208BPHBUS-01 U.S. 4-29
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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 3 MODEL 208B G1000 A
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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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