BEECHCRAFT
Baron
58
Serial TH
773
and
After
AIRFRAME
Section
VII
Systems
Description
The BEECHCRAFT BARON 58 is a
four
to six
place
all-metal.
low-wi
ng,
twin-engi
ne
airplane
with
retractable
tricycle
landing
gear, and a
conventional
horizontal
and
vertical
stabilizer.
FLIGHT
CONTROLS
CONTROL SURFACES
Control
surfaces
are
bearing
supported
and
operated
through
push-pull
rods and
conventional
cable
systems
terminating
in
bellcranks.
CONTROL
COLUMN
The
throw-over
type
control
column
for
elevator
and
aileron
control
can be placed in
front
of
either
front
seat. Pu
11
the
T
~
handle
latch
at
the
back of
the
control
arm
and
position
the
control
wheel
as desired. Check
for
full
freedom
of
move-
ment
after
repositioning
the
control.
NOTE
If a reduced power throttle position exists when
throwing over the control column, it will be
necessary to momentarily move the throttle
levers forward for
passage
of
the
control
column.
The
optional
dual
control
column
is
required
for
flight
in-
struction.
RUDDER PEDALS
To
adjust the rudder pedals, press the spring-loaded lever
on the side of each pedal arm and move the pedal to its
forward or aft position. The adjustment lever can also be
used to place the right set of rudder pedals against the floor,
(when the copilot brakes are not installed) when not in use.
September,
1979
7-5
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