Piper Cherokee Six - Page 163

PIPER CHEROKEE SIX SERVICE MANUAL
10.
Tighten
the
connecting
bolts
(22)
of the
idler sprockets
(19
and
21).
11.
Install the
floor
tunnel plate
and secure
with
screws.
Fasten
the tunnel
carpet
in
place.
12.
Install
the fuel
selector
lever
on the
selector
torque
tube
and
secure
with clevis
pin
and
safety
with cotter
pin.
13. Install
the fuel
selector covers
and
the rudder
trim control
knob.
b.
Either control
wheel
assembly
may
be installed
by
the following
procedure:
1. Insert
the
control
wheel
tube
through
the
instrument
panel.
2. Should
wires
for the
various
Autopilot
systems
need
to be installed
in the
control
tube,
route
them through
the hole
in the
forward
side of
the tube
and
out of
the
small
hole
in the forward
side.
Position
the rubber
grommet
in the
hole in the
side of
the
tube.
3. On the
left control
tube install
the
stop (6).
4. Connect
the control
wheel
tube (2)
to the
flexible
joint (4)
of the
tee bar
assembly.
If
the control
cables
and/or
chains have
not been
removed
or loosened,
place
the
ailerons
in neutral
and install
the
control tube
on the
flexible
joint to
allow the
control
wheel
to be
neutral. Install
bolt,
washer
and nut
(3) and
tighten.
5-5a. REMOVAL
OF CONTROL
COLUMN
ASSEMBLY
(PA-32R-300).
(Refer
to
Figure
5-1a.)
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 turbuckles
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.
SURFACE
CONTROLS
Revised:
6/18/76
1G19