Piper PA-32RT-300T User Manual

5-3.
CONTROL
COLUMN
ASSEMBLY.
5-4.
REMOVAL
OF
CONTROL
COLUMN
ASSEMBLY.
(Refer
to
Figure
5-1.)
a.
To
remove
either
control
wheel
(5)
with
tube
(4),
the
following
procedure
may
be
used:
1.
Separate
the
control
wheel
tube
(4)
from
the
flexible
joint
(2)
that
is
located
on
either
side
of
the
tee
bar
assembly
(7)
by
removing
the
nut,
washer
and
bolt
(3).
Pull
the
tube
from
the
flexible
joint.
2.
If removing
the
left
control
tube,
slide
the
stop
(12)
from
the
tube.
3.
Should
wires
for
the
various
Autopilot
systems
be installed
in the
control
tube,
disconnect
them
at
the
quick
disconnect
terminals
behind
the
instrument
panel.
Draw
the
wires
back
into
the
tube
and
back
out
through
the
forward
end
of
the
tube.
4.
Remove
the
control
wheel
assembly
from
the
instrument
panel.
b.
The
tee
bar
(7)
with
assembled
parts
may
be
removed
from
the
airplane
by
the
following
procedure:
1. Remove
the
access
panel
to
the
aft
section
of
the
fuselage.
2.
Relieve
cable
tension
from
the
stabilator
control
cables
(23)
at
one
of
the
stabilator
cable
turnbuckles
in
the
aft
section
of the
fuselage.
3.
Relieve
tension
from
the
aileron
control
cables
(22)
and
chains
(14
and
16)
at
the
turnbuckle
(6)
that
connects
the chains
at
the
top
of the
tee
bar
(7).
4.
Disconnect
the
control
chains
from
the
control
cables
where
the
chains
and
cables
join
by
removing
the
cotter
pins,
nuts,
bolts
and
bushings.
5.
If
the
control
wheel
assemblies
have
not
been
previously
disconnected
from
the
tee
bar
assembly,
separate
the
control
wheel
tubes
(4)
at
the
flexible
joints
(2)
by
removing
the
nuts,
washers
and
bolts
(3).
6.
Remove
the tunnel
plate
just
aft
of
the tee
bar
by
laying
back
enough
tunnel
carpet
to
remove
the
plate
attachment
screws.
7.
Remove
the
two
aileron
control
cable
pulleys
(21)
attached
to
the
lower
section
of the
tee
bar
by
removing
the
pulley
attachment
bolt
(8).
8. Disconnect
the
stabilator
control
cables
(23)
from
the
lower
end
of
the tee
bar
assembly.
9.
Disconnect
the
necessary
control
cables,
such
as the
propeller
pitch
control,
mixture
control,
etc.,
that
will
allow
the
tee
bar assembly
to be
removed.
10. Remove
the
tee
bar assembly
by
removing
the
attachment
bolts
(3)
with
washers
and
nuts
which
are through
each
side
of
the
floor
tunnel,
and
lifting
it up
and
out
through
the
right
side
of
the
cabin.
5-5.
INSTALLATION
OF
CONTROL
COLUMN
ASSEMBLY.
(Refer
to
Figure
5-1.)
a. The
tee
bar
assembly
may
be
installed
in
the
airplane
by the
following
procedure:
1. Swing
the
tee
bar
assembly
into
place
from
the
right
side
of the
cabin
and
secure
with
attachment
bolts
(3),
washers
and
nuts
inserted
in
through
each
side
of
the
floor
tunnel.
2. Connect
the
stabilator
control
cables
(23)
to
the
lower
end
of the
tee
bar
with
bolt
(3),
washer,
nut
and
cotter
pin.
Allow
the
cable
ends
free
to
rotate.
3.
Place
the
aileron
control
cables
(22) around
the pulleys
(21)
that
attach
to the
lower
section
of
the tee
bar
(7); position
pulleys
and
secure
with
bolt,
washers
and
nut.
4.
Install
the
control
wheel
per Step
b.
5.
Place
the
control
wheels
in
neutral
(centered)
position
and
install
the
aileron
control
chains
(14
and 16)
on
the
control
wheel
sprockets
(1
and 13)
and
idler
cross-over
sprockets
(15 and
18).
The turnbuckle
(6)
must
be centered
between
the
two control
wheel
sprockets.
Isued:
1/3/78
SURFACE
CONTROLS
1F18
LANCE
II SERVICE
MANUAL

Piper PA-32RT-300T Specifications

General

Brand	Piper
Model	PA-32RT-300T
Category	Aircrafts
Language	English