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SECTION 7 CESSNA AIRPLANE AND SYSTEMS DESCRIPTION MODEL 208B G1000 STANDBY INDICATOR CONTROL KNOB The knob labeled STANDBY IND varies the intensity of the integral lighting of the standby airspeed indicator, attitude indicator, altimeter, torque indicator, and magnetic compass. Clockwise rotation of the knob increases light brightness and counterclockwise rotation decreases brightness. SWITCH/CIRCUIT BREAKER PANEL CONTROL KNOB The knob labeled SW/CB PANELS varies the intensity of the backlit LED panels. These panels are inscribed with labels for most of the switches, controls, and circuit breakers mounted on the instrument panel. Clockwise rotation of the knob increases panel brightness and counterclockwise rotation decreases brightness. CIRCUIT BREAKER/PEDESTAL/OVERHEAD PANEL KNOB The knob labeled CB/PED/OVHD varies the intensity of the lights that illuminate the left sidewall switch and circuit breaker panel, the flood light that illuminates the control pedestal, and the post lights that illuminate the overhead panel. Clockwise rotation of the knob increases panel brightness and counterclockwise rotation decreases brightness. LEFT FLOOD LIGHTING CONTROL KNOB This knob labeled LEFT FLOOD varies the brightness of the left side floodlight located on the right aft side of the overhead panel. This floodlight may also be used to illuminate the left sidewall switch and circuit breaker panel. Clockwise rotation of this control knob increases lamp brightness while counterclockwise rotation decreases brightness. RIGHT FLOOD LIGHTING CONTROL KNOB This knob labeled RIGHT FLOOD varies the brightness of the right side floodlight located on the left aft side of the overhead panel. Clockwise rotation of this control knob increases lamp brightness while counterclockwise rotation decreases brightness. CONTROL WHEEL MAPLIGHTS A control wheel maplight is mounted on the bottom of each control wheel. These lights illuminate the lower portion of the cabin in front of the pilot and copilot, and are used for checking maps and other flight data during night operation. Brightness of these lights is adjusted with a rheostat control knob on the bottom of the control wheel. Rotating the near side of the knob to the right increases light brightness and to the left decreases brightness. 7-82 U.S. 208BPHBUS-00
CESSNA SECTION 7 MODEL 208B G1000 AIRPLANE AND SYSTEMS DESCRIPTION CABIN LIGHTS WITHOUT TIMER (208B Passenger) The 208B passenger cabin light system without timer consists of four cabin lights installed on the interior of the airplane and courtesy lights under each wing to facilitate boarding or loading cargo during night operations. Two lights are located above the center cabin area, one above the aft cargo door, and one above the aft passenger door. Controls for the lighting system consists of one 2-way toggle switch labeled CABIN on the lighting control panel as well as a rocker switch just forward of both the aft passenger and cargo doors. All three of these switches will toggle all cabin on or off at any time regardless of the other switch positions. The circuit for the cabin lights is protected by a pull-off type circuit breaker, labeled CABIN LTS, on the J-Box panel in the engine bay. CABIN LIGHTS WITH TIMER (if installed) The 208B cabin light system with timer consists of four cabin lights installed on the interior of the airplane and courtesy lights under each wing to facilitate boarding or loading cargo during night operations. Two lights are located above the center cabin area, one above the aft cargo door, and one above the aft passenger door. Controls for the lighting system consists of one 3-way momentary switch labeled CABIN on the lighting control panel as well as a rocker switch just forward of both the aft passenger and cargo doors. The passenger door toggle switch will control all lights except the cargo door light, while the cargo door toggle switch will control only the cargo door light. The 3-way momentary switch labeled CABIN on the lighting control panel will control all lights regardless of the other switch positions. The timer circuitry includes a solid state timer that will turn off all lights after 30 minutes automatically unless they are switched off manually. The circuit for the cabin lights is protected by a "pull-off" type circuit breaker, labeled CABIN LTS, on the J-Box panel in the engine bay. CABIN LIGHTS WITH TIMER (Super CargoMaster) The Super CargoMaster cabin light system consists of four cabin lights installed on the interior of the airplane and courtesy lights under each wing to facilitate boarding or loading cargo during night operations. Two lights are located above the center cabin area, one above the aft cargo door and one opposite the aft cargo door. Controls for the lighting system consists of one 3-way momentary switch labeled CABIN on the lighting control panel as well as a rocker switch just forward of the cargo door. 208BPHBUS-00 U.S. 7-83
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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 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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