Left Sidewall Switch And Circuit Breaker Panel; Overhead Panel - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

CESSNA SECTION 7
MODEL 208B 867 SHP AIRPLANE AND SYSTEMS DESCRIPTION
GARMIN G1000
LEFT SIDEWALL SWITCH AND CIRCUIT BREAKER
PANEL
Most of the engine control switches and non-avionics circuit breakers
are located on a separate panel mounted on the left cabin sidewall
adjacent to the pilot. Switches and controls on this panel are illustrated
in Figure 7-4, the Left Sidewall Switch and Circuit Breaker Panel. For
details concerning the instruments, switches, and controls on this
panel, refer to the ELECTRICAL EQUIPMENT descriptions in this
section.

OVERHEAD PANEL

The overhead panel, located above and between the pilot and copilot,
contains FUEL TANK SELECTORS control valves, OXYGEN control
lever and pressure gage (if installed), vent outlets and controls,
overhead lighting, and STBY FLAP MOTOR control switches.
Equipment mounted on this panel is illustrated in Figure 7-3, Overhead
Panel. For details concerning the instruments, switches, and controls
on the overhead panel, refer in this section to the description of the
systems to which these items are related.
208BPHCUS-00 7-19
U.S.