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BE ECHCR AFT Sundowner
180
Section VII
C23(M-1285and
After)
Systems Description
CIRCUIT
BREAKERS
The circuit breakers are located on the
right
subpanel.
FUGHT INSTRUMENTS
The standard
flight instruments
are
grouped
in
a "T"
pattern
on the
main panel
for the best
presentation
for the
pilot.
The
magnetic
compass
is
located above the
instru-
ment panel.
Ram air
pressure
for the
airspeed
indicator
entersthrough
the
pitot
tube under the left
wing,
static air
pressure
for the
altimeter,
vertical
speed and airspeed
indicator
is
supplied
by a static
port
on each side of the fuselage,
just
aft of the
cabin.
M-1285
through
M-1979
except
M-1971:
i
instrument
lights
are turned on and dimmed by a
rheostat
switch
located
on the left subpanel, and a
rheostat
switch
located
below the
power quadrant.
M-1971, M-1980
and after:
Instrument
lights
are turned
on
and
dimmed by
two
rheostat
switches
located
on the
pedestal, below
the
power
quadrant.
GROUND
CONTROL
Steering
is
accomplished
by the
use
of
rudder
pedals
through a spring-loaded
linkage
connecting
the
nose gear
to the rudder
pedals.
The
nose gear maximum
travel
is 40°
±
2°
right
or left, and a
hydraulic
shimmy damper on the
nose gear yoke
compensates
for any tendency to shimmy.
Toe brakes
may
be used to aid in steering the airplane on
the
ground.
January,
1982
7-11
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