Cessna 208B - Left Sidewall Switch and Circuit Breaker Panel; Right Flight Instrument Panel

CESSNA
SECTION 7
MODEL
2088 (675 SHP) AIRPLANE AND SYSTEMS DESCRIPTION
INSTRUMENT PANEL (Continued)
For details concerning the instruments, switches, and controls on this
panel, refer in this section to the description of the systems to which
these items are related.
RIGHT FLIGHT INSTRUMENT PANEL
A supplementary flight instrument group may be installed directly in
front of the right front passenger. Like the pilot's flight instrument panel,
the right flight panel groups the attitude and directional indicators
vertically with the airspeed indicator to the left and the altimeter to the
right to form a basic
"T" arrangement. the remainder of the instruments
(turn and bank indicator and vertical speed indicator) are grouped
around the basic
"T". The right flight instruments utilize a second,
independent pitot-static pressure system for operation.
LEFT SIDEWALL SWITCH AND CIRCUIT BREAKER
PANEL
Most of the engine control switches and all 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
and 7-5.
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