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SECTION 7
CESSNA
AIRPLANE AND SYSTEMS DESCRIPTION
MODEL 208B 867 SHP
GARMIN G1000
LIGHTING SYSTEMS
(Continued)
INTERIOR LIGHTING
Instrument and control panel lighting is provided by integral and flood
lights. Six lighting control knobs are grouped together on the lower part
of the instrument panel to the left of the control pedestal. These
controls vary the intensity of the lighting for the instrument panels,
pedestal, overhead panel, left sidewall panel, LED panels, Garmin
displays, and internally lit standby instruments. The following
paragraphs describe the function of these controls. The circuits for
these lights are protected by two pull-off type circuit breakers, labeled
AVN/LED/STBY LIGHTS and COCKPIT FLOOD LIGHTS, on the left
sidewall switch and circuit breaker panel. Other miscellaneous lighting
provided or available includes control wheel map LED lights, cabin
lights, LED passenger reading lights, and a no smoking/seat belt sign.
Discussion of these lights and their controls is also included in the
following paragraphs. Most interior lighting is LED.
GARMIN DISPLAYS, OPTIONAL ADF, AND HF DISPLAYS (if
installed)
The AVIONICS knob varies the intensity of the Garmin and optional
displays (if installed). Clockwise rotation of the knob increases display
brightness and counterclockwise rotation decreases brightness. The
displays cannot be dimmed to full dark. Rotating this knob
counterclockwise past the dimmest setting will place the displays in
photosensitive mode.
STANDBY INDICATOR CONTROL KNOB
The STANDBY IND knob varies the intensity of the Non-LED 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.
7-102
208BPHCUS-00
U.S.
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