Cessna 152 - Page 111

CESSNA
MODEL
152
SECTION7
AIRPLANE
&
SYSTEMS
DESCRIPTIONS
lighter,
and
engine
instruments
positioned
below
the
pilot's
control
wheel.
The
electrical
switches,
panel
and
radio
light
rheostat
knob,
ignition
and
master
switches,
primer,
and
parking
brake
control
are
located
around
these
instruments.
The
engine
controls,
wing
flap
switch,
and
cabin
air
and
heat
control
knobs
are
to
the
right
of
the
pilot,
at
the
center
of
the
switch
and
control
panel.
Directly
below
these
controls
are
the
elevator
trim
control
wheel,
trim
position
indicator,
microphone,
and
circuit
breakers.
A
map
compartment
is
on
the
extreme
right
side
of
the
switch
and
control
panel.
For
details
concerning
the
instruments,
switches,
circuit
breakers,
and
controls
on
this
panel,
refer
in
this
section
to
the
description
of
the
systems
to
which
these
items
are
related.
GROUND
CONTROL
Effective
ground
control
while
taxiing
is
accomplished
through
nose
wheel
steering
by
using
the
rudder
pedals;
left
rudder
pedal
to
steer
left
and
right
rudder
pedal
to
steer
right.
When
a
rudder
pedal
is
depressed,
a
spring-loaded
steering
bungee
(which
is
connected
to
the
nose
gear
and
to
the
rudder
bars)
will
turn
the
nose
wheel
through
an
arc
of
approximately
8.5°
each
side
of
center.
By
applying
either
left
or
right
brake,
the
degree
of
turn
may
be
increased
up
to
30°
each
side
of
center.
Figure
7-3.
Wing
Flap
System
1
July
1978 7-9