Beechcraft Baron G58, Pilot Operating Handbook

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Systems Description
Section 7
Model G58
7-9
SUBPANEL
The magneto/start switches and switches for the batteries,
alternators, avionics master, prop sync, fuel vent, stall warning
heat, windshield heat, surface deice, air condition and heat
control, pitot heat, propeller deice, exterior and interior lights,
vent blower, and fuel boost pumps are located in the left sub-
panel. Also located in the left subpanel are the landing gear
position indicator lights and landing gear handle. The prop
deice ammeter is located in the center subpanel. Located in
the right subpanel are the flap switch, flap position lights, utility
power outlet, lighting rheostats, and glove compartment. The
avionics circuit breaker panel is below the right subpanel and
the left circuit breaker panel is on the side panel to the left of
the pilot’s seat.
OAT GAGE (TH-2125 THRU TH-2339, EXCEPT TH-
2310)
The OAT (Outside Air Temperature) gage is located on the left
cabin side panel just aft of the instrument panel. Its tempera-
ture sensing probe extends through the cabin sidewall into the
outside air. The indicated Outside Air Temperature (IOAT)
shown on this gage varies with airspeed and must be cor-
rected for compressibility effects to provide true outside air
temperature. The indicated OAT is equal to true outside air
temperature only at zero airspeed.
PEDESTAL
The pedestal is located below the center portion of the instru-
ment subpanel. The upper portion of the pedestal houses the
throttle (black), propeller (blue), and mixture (red) controls. The
elevator trim tab control is located on the left side of the pedes-
tal. The rudder and aileron trim tab controls are mounted on
the front of the pedestal along with the cowl flap controls.
May, 2015
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