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SECTION 4 CESSNA NORMAL PROCEDURES MODEL 208B G1000 AIRSPEEDS FOR NORMAL OPERATION (Continued) BALKED LANDING: Takeoff Power, Flaps 20° . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS MAXIMUM RECOMMENDED TURBULENT AIR PENETRATION SPEED: 8750 Pounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 148 KIAS 7500 Pounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 137 KIAS 6250 Pounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 125 KIAS 5000 Pounds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 112 KIAS MAXIMUM DEMONSTRATED CROSSWIND VELOCITY: Takeoff or Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 KNOTS 4-4 U.S. FAA APPROVED 208BPHBUS-00
CESSNA SECTION 4 MODEL 208B G1000 NORMAL PROCEDURES PREFLIGHT INSPECTION WARNINGS WARNING • Visually check airplane for general condition during walk-around inspection and remove any inlet, exit or exhaust covers. If cargo pod is installed, check its installation for security during the walk-around inspection. Use of a ladder will be necessary to gain access to the wing for visual checks, refueling operations, checks of the stall warning and pitot heat, and to reach outboard fuel tank sump drains. • It is the pilot's responsibility to ensure that the airplane's fuel supply is clean before flight. Any traces of solid contaminants such as rust, sand, pebbles, dirt, microbes, and bacterial growth or liquid contamination resulting from water, improper fuel type, or additives that are not compatible with the fuel or fuel system components must be considered hazardous. Carefully sample fuel from all fuel drain locations during each preflight inspection and after every refueling. • It is essential in cold weather to remove even the smallest accumulations of frost, ice, snow, or slush from the wing, tail, control surfaces, propeller blades, and engine air inlets. Exercise caution to avoid distorting the vortex generators on horizontal stabilizer while deicing. To assure complete removal of contamination, conduct a visual and tactile inspection of all critical surfaces. Also, make sure the control surfaces contain no internal accumulations of ice or debris. If these requirements are not performed, aircraft performance will be degraded to a point where a safe takeoff and climb may not be possible. • Prior to any flight in known or forecast icing conditions, check that PITOT/ STATIC tube(s) and STALL warning heaters are warm to touch after turning PITOT/STATIC and STALL HEAT switches ON for 30 seconds, then OFF. Make sure the pitot covers are removed prior to turning PITOT/STATIC HEAT ON. • If a night flight is planned, check operation of all lights, and make sure a flashlight is available and properly stowed. FAA APPROVED 208BPHBUS-00 U.S. 4-5
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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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Page 118 and 119: SECTION 3 CESSNA EMERGENCY PROCEDUR
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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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