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CESSNA SECTION 7<br />

MODEL 208B G1000 AIRPLANE AND SYSTEMS DESCRIPTION<br />

FLASHING BEACON LIGHT<br />

A red flashing beacon light is installed on the top of the vertical fin as<br />

additional anti-collision protection in flight and for recognition during<br />

ground operation. The light is visible through 360°. The flashing beacon<br />

light circuit is protected by a pull-off type circuit breaker, labeled<br />

BEACON LIGHT, on the left sidewall switch and circuit breaker panel.<br />

WARNING<br />

The flashing beacon should not be used when<br />

flying through clouds or overcast; the flashing light<br />

reflected from water droplets or particles in the<br />

atmosphere, particularly at night, can cause<br />

disorientation or vertigo.<br />

COURTESY LIGHTS<br />

Two courtesy lights are installed, one under each wing. The lights<br />

illuminate the area outside of the airplane adjacent to the crew entry<br />

doors. The lights operate in conjunction with the cabin lights and are<br />

controlled by the cabin light switches as described in the Cabin Lights<br />

paragraph in this section.<br />

INTERIOR LIGHTING<br />

Instrument and control panel lighting is provided by integral, flood and<br />

post lights. Six lighting control knobs are grouped together on the lower<br />

part of the instrument panel to the left of the control pedestal. These<br />

controls vary the intensity of the lighting for the instrument panel,<br />

pedestal, overhead panel, left sidewall panel, LED panels, Garmin<br />

displays, and internally lit instruments. The following paragraphs<br />

describe the function of these controls. The circuits for these lights are<br />

protected by two pull-off type circuit breakers, labeled AVN/FLOOD<br />

LIGHT and INST LIGHT, on the left sidewall switch and circuit breaker<br />

panel. Other miscellaneous lighting provided or available includes<br />

control wheel map lights, cabin lights, passenger reading lights, and a<br />

no smoking/seat belt sign. Discussion of these lights and their controls<br />

is also included in the following paragraphs.<br />

GARMIN DISPLAYS, OPTIONAL ADF, AND HF DISPLAYS (if<br />

installed)<br />

The knob labeled AVIONICS varies the intensity of the Garmin and<br />

optional displays (if installed). Clockwise rotation of the knob increases<br />

display brightness and counterclockwise rotation decreases brightness.<br />

The displays cannot be dimmed to full dark. Rotating this knob<br />

counterclockwise past the dimmest setting will place the displays in<br />

photosensitive mode.<br />

208BPHBUS-00<br />

U.S.<br />

7-81

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