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SECTION 3 CESSNA ABNORMAL PROCEDURES MODEL 208B G1000 XSIDE AHRS This message is displayed on both PFDs and indicates that both PFDs are displaying data from the opposite side Attitude Heading Reference System. Normally the pilot’s side displays ADC1 and the copilot’s side displays ADC 2. Refer to GARMIN G1000 Cockpit Reference Guide for additional information. MULTI-FUNCTION DISPLAY FAN FAILED An overheat condition may arise in the associated display. In this case, screen brightness will be reduced automatically by 50% to lower internal temperature. Use reversionary capabilities, if necessary. PRIMARY FLIGHT DISPLAY 1 FAN FAILED An overheat condition may arise in the associated display. In this case, screen brightness will be reduced automatically by 50% to lower internal temperature. Use reversionary capabilities, if necessary. PRIMARY FLIGHT DISPLAY 2 FAN FAILED An overheat condition may arise in the associated display. In this case, screen brightness will be reduced automatically by 50% to lower internal temperature. Use reversionary capabilities, if necessary. INADVERTENT OPENING OF AIRPLANE DOORS IN FLIGHT If any of the airplane doors should inadvertently open in flight, the airplane should be slowed to 125 KIAS or less to reduce buffeting of the doors. If the upper cargo door is open, slow to 100 KIAS or less and lower flaps to full down so that wing downwash will move the door towards its normally closed position. Closing the upper cargo door (or upper half of the passenger door on the Standard 208B) can be accomplished after airspeed has been reduced by pulling the door forcefully closed and latching the door. If the door cannot be closed in flight, a landing should be made as soon as practical in accordance with the checklist procedures. On Cargo Versions, an open cargo door cannot be closed in flight since the inside of the upper door has no handle. If any cargo pod doors inadvertently open in flight, the airplane should be slowed to 125 KIAS or less and landed as soon as practical. During the landing, avoid a nose-high flare to prevent dragging an open rear cargo pod door on the runway. 3-80 U.S. FAA APPROVED 208BPHBUS-01
CESSNA SECTION 4 MODEL 208B G1000 NORMAL PROCEDURES NORMAL PROCEDURES Table of Contents Page Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-3 Speeds for Normal Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-3 CHECKLIST PROCEDURES Preflight Inspection Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-5 Preflight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-6 Preflight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-6 Cabin. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-6 Left Side . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-8 Left Wing, Leading Edge. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-8 Left Wing, Trailing Edge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-10 Measured Fuel Depth vs. Fuel Quantity . . . . . . . . . . . . . . . . . . . 4-11 Empennage. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-12 Right Wing, Trailing Edge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-13 Right Wing, Leading Edge . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-13 Nose . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-15 Before Starting Engine. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-17 Starting Engine (Battery Start) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-18 Starting Engine (External Power Start) . . . . . . . . . . . . . . . . . . . . . .4-20 Taxiing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-22 Before Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-22 Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-25 Normal Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-25 Short Field Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-26 Type II, Type III or Type IV Anti-ice Fluid Takeoff . . . . . . . . . . . .4-26 Enroute Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-26 Cruise Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-26 Maximum Performance Climb. . . . . . . . . . . . . . . . . . . . . . . . . . .4-27 Cruise . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-28 Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-28 Before Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-29 Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-29 Normal Landing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-29 Short Field Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-30 Balked Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4-30 (Continued Next Page) FAA APPROVED 208BPHBUS-00 U.S. 4-1
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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 4 MODEL 208B G1000 N
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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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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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