Cessna 182 1978 - Control Column; Pilots Control Column

MODEL
182
& T182
SERIES
SERVICE
MANUAL
6-3.
TROUBLE
SHOOTING
(Cont).
TROUBLE
PROBABLE
CAUSE
REMEDY
CONTROL
WHEELS
NOT
Improper
adjustment
of
Refer
to paragraph
6-18.
LEVEL
WITH
AILERONS
cables.
NEUTRAL.
Improper
adjustment
of
Adjust
push-pull
rods
to obtain
aileron
push-pull
rods.
proper
alignment.
DUAL CONTROL
WHEELS
Cables
improperly
adjusted.
Refer to
paragraph
6-18.
NOT
COORDINATED.
INCORRECT
AILERON
Push-pull
rods not
adjusted
Refer
to paragraph
6-18.
TRAVEL.
properly.
Incorrect
adjustment
of
travel
Refer
to paragraph
6-18.
stop
bolts.
6-4.
CONTROL COLUMN.
(See figure
6-2.)
adapter
(35) to control
wheel tube assembly
(13) and
remove
control
wheel
assembly.
6-5.
DESCRIPTION.
Rotation
of the control
wheel
2.
Disconnect
electrical
wiring
to map
light and
rotates
four
bearing roller
assemblies
(3)
on the
end
mike switch
at
connector
(39) if installed.
Slide
of
the control
wheel
tube (13),
which
in
turn,
rotates
cover
(1) off
control
wheel
tube
assembly
(13).
a
square
control
tube
assembly
(15)
inside
and
ex-
3.
Remove
decorative
cover
from
instrument
tending
from
the control
wheel
tube (13).
Attached
panel.
to this
square
tube
(15)
is
a quadrant
(24)
which
oper-
4.
Remove
screw
securing
adjustable
glide
plug
ates
the aileron
system.
This
same
arrangement
is
(14)
to control
tube
assembly
(15)
and
remove
plug
provided
for
both
control
wheels.
Synchronization
of
and
glide
assembly.
the
control
wheels
is
obtained
by
the
interconnect
5.
Disconnect
push-pull
tube
(16)
at
sleeve
weld
cable
(29),
turnbuckle
(30)
and
adjustment
terminals
assembly
(5).
(27).
The
forward
end
of the
square
control
tube
(15)
6.
Remove
screws
securing
support
plate
(10)
at
is mounted
in
a
bearing
block
(21)
on
firewall
(31)
and
instrument
panel.
does
not move
fore-and-aft,
but
rotates
with
the
con-
trol
wheel.
The
four
bearing
roller
assemblies
(3)
NOTE
on
the end
of
the
control
wheel
tube
reduce
friction
as
the
control
wheel
is
moved
fore-and-aft
for
ele-
To
ease
removal
of
control
wheel
tube
assem-
vator
system
operation.
A
sleeve
weld
assembly
(5),
bly
(13),
snap
ring
(9)
may
be
removed
from
containing
bearings
which
permit
the
control
wheel
its
locking
groove
to allow
sleeve
weld
assem-
tube
to rotate
within
it,
is secured
to
the
control
bly
(5)
additional
movement.
wheel
tube
by
a sleeve
and
retaining
ring
in
such
a
manner
it
moves
fore-and-aft
with
the
control
wheel
7.
Using
care,
pull
control
wheel
tube
assembly
tube.
This
movement
allows
the
push-pull
tube
(16)
(13)
aft
and
work
assembly
out
through
instrument
attached
to
the
sleeve
weld
assembly
(5)
to
operate
panel.
an
elevator
arm
assembly
(18),
to which
one
elevator
cable
(20)
is attached.
A
torque
tube
(19)
connects
NOTE
this
arm
assembly
(18)
to
the
one
on the
opposite
end
of the
torque
tube (19),
to which
the
other
elevator
If removal
of
control
tube
assembly
(15)
or
cable
is attached.
When
dual
controls
are
installed,
quadrant
(24)
is
necessary,
proceed
to step
the
copilot's
control
wheel
is
linked
to the
aileron
and
8.
elevator
control
systems
in
the
same
manner
as
the
pilot's
control
wheel.
8.
Remove
safety
wire
and relieve
direct
cable
tension
at turnbuckles
(index
8, figure
6-1).
6-6.
REMOVAL
AND
INSTALLATION.
(See
figure
6-2.)
9. Remove
safety
wire
and
relieve
interconnect
a.
PILOT'S
CONTROL
COLUMN.
cable
tension
at
turnbuckle
(30).
1.
Slide
cover
(1)
toward
instrument
panel
to
10.
Remove
safety
wire
and
remove
roll
pin (28)
expose
adapter
(35).
Remove
screws
securing
through
quadrant
(24)
and
control
tube
assembly
(15).
6-2