SECTION 7 CESSNA
AIRPLANE AND SYSTEMS DESCRIPTION MODEL 208B 867 SHP
GARMIN G1000
U.S.
PANEL LAYOUT
To the left of the pilot PFD is a switch panel which has many of the
switches necessary to operate the airplane systems. At lower left are a
circuit breaker panel for avionics systems, the left fresh air outlet and
pull knob, test switches for prop overspeed, fire detection, and fuel
selection warning systems, microphone and headset jacks and an
alternate static source valve.
Below the MFD are standby indicators for airspeed, attitude, altitude,
and torque. Below these indicators are the parking brake, light dimming
controls, inertial separator control, and cabin heat controls. Provisions
are included for optional air conditioning controls and HF and ADF
displays.
At lower right are the map compartment, right fresh air outlet and pull
knob, and microphone and headset jacks. At upper right are the hour
meter and ELT remote switch. Mounted above the glare shield is a
magnetic compass. 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.
CONTROL PEDESTAL
A control pedestal, extending from the center of the instrument panel to
the floor, contains the EMERGENCY POWER lever, POWER lever,
PROP RPM lever, FUEL CONDITION lever, WING FLAPS selector and
position indicator, elevator, rudder and aileron trim controls with
position indicators, the FUEL/OIL SHUTOFF knob, CABIN HEAT
FIREWALL SHUTOFF control, a microphone, 12VDC power outlet, and
an auxiliary audio input jack
Equipment mounted on this panel is illustrated in Figure 7-2. For details
concerning the instruments, switches, and controls on the pedestal,
refer to the description of the systems to which these items are related.
208BPHCUS-00
7-16
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