Ac Generation; Description And Operation - Raytheon BEECH BARON 58P Maintenance Manual

BEECHCRAFT
BARON 58P AND BARON 58TC
MAINTENANCE MANUAL
GENERAL DESCRIPTION
AND
OPERATION
through
TJ-90 and TK-1
through
TK-26. On
airplane serials
TJ-91 through TJ-114, TJ-119 through TJ-125, TK-27
AC GENERA TION
through TK-50, and TK-56 through TK-58 the inverter for the
fuel flow indicator is located in the main
compartment
of the
Since
the major portion of the airplane instrumentation
right nacelle
on
the outboard side. On
airplane
serials TJ-1I5
functions
on
de power, the
ac power
requirements
are
through TJ-118, TJ-126 and after, TK-51 through TK-55,
and
confined
to
the fuel flow indicator and the
electroluminescent TK-59 and after the fuel flow inverter is
not
installed. The
panel lights. Each
system
includes
an
inverter which is inverter for the electroluminescent panel lights is located
on
designed
to
supply
power
to
the system by converting
28 vdc
the left hand side of the fuselage
at
F.S. 58.00 and is
to
the required
ac
voltage of that
system.
The inverter for the
accessible from within the fuselage. Power is supplied to
fuel flow indicator is located in the inboard side of
the right each inverter when the battery
master
switch is placed in the
nacelle just forward of the main spar
on
airplane serials TJ-2
on
position.
"END"
24-20-00
Page
1
Nov
30/78