SOCATA
MODEL TB 20
SECTION 7
DESCRIPTION
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. It is supplied in
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Information in this document is subject to change without notice.
© 1988, 1991, 1992, 1994 to 1996, 1997, 2000 -
socata
- All rights reserved
June 30, 1988
Revision 6
7.14
Upper duct central part (see Figure
– ”Flight conditions” placard
– ”Instruction” plate
– Front overhead lights
– Radio loud–speaker (if installed)
– Oxygen control and pressure gage (if installed)
– Alarms loud–speaker
– Blower switch (if installed)
– Autopilot alarm (if installed)
– Rear overhead light
– Rear air outlets.
ADVISORY PANEL
The advisory panel (see Figures
) is located at the top edge of
the L.H. instrument panel, directly in front of the pilot. The panel contains
separate indicator lights which illuminate green, amber or red when a specific
condition occurs in the associated airplane system. A green colored light is
illuminated to indicate a normal or safe condition in the system. However, an
illuminated amber lamp indicates that a cautionary condition exists, but which
may not require immediate corrective action. When a hazardous condition
exists requiring immediate corrective action, a red light illuminates.
A day / night switch is installed in the centre of the advisory panel to control
the intensity of the green indicator lights and of the GPS annunciators (if GPS
installed).
Additional annunciators, associated to the GPS (if installed) are installed in
the centre of the advisory panel.
SWITCH–BREAKERS PANEL
The general electrical equipment switch–breakers are located on the front
part of the central pedestal.
The switch–breakers located on this panel are illustrated in Figure
.
CIRCUIT–BREAKERS PANEL
The electrical equipment circuit–breakers are located on a separate panel
mounted on the L.H. cabin sidewall adjacent to the pilot.
Circuit–breakers located on this panel are illustrated in Figure