Piper Cherokee Six - Page 160

PIPER
CHEROKEE
SIX SERVICE
MANUAL
The wing
flap
system
consists
of an
operating
handle,
a
cable
routed
from
the handle
to a
torque
tube
and push-pull
rods.
Through
the
push-pull
rods
and
torque
tube,
the flaps
are interconnecting
and
can
be positioned
in
three
locations
of 10,
25 and 40
degrees.
5-3.
CONTROL
COLUMN
ASSEMBLY.
5-4. REMOVAL
OF CONTROL
COLUMN
ASSEMBLY
(PA-32-260
and
300). (Refer
to
Figure
5-1.)
a.
To
remove
either
control
wheel
(1)
with
tube
(2),
the
following
procedure
may
be
used:
1.
Separate
the
control
wheel
tube
(2)
from
the
flexible
joint
(4)
that
islo-
cated
on either
side
of
the
tee
bar
assembly
(5)
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
(6)
from
the
tube.
3.
Should
wires
for
the
various
AutoPilot
systems
be
installed
in the
con-
trol
tube,
disconnect
them
at
the
quick
disconnect
terminals
behind
the
instru-
ment
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
(5)
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
(11)
at one
of
the
stabilator
cable
turnbuckles
in the
aft
section
of the
fuselage.
3.
Relieve
tension
from
the
aileron
control
cables
(12)
and
chains
(7
and
8) at
the
turnbuckle
(9)
that
connects
the
chains
at
the
top
of
the
tee
bar
(5).
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
(2)
at
the
flexible
joints
(4)
by removing
the
nuts,
washers
and
bolts
(3).
6.
Remove
the
fuel
selector
panel
cover
by
removing
the
rudder
trim
knob
and
the
cover
attachment
screws.
7.
Remove
the
lower
selector
cover
and
disconnect
the
fuel
selector
con-
trol
lever
from
the
selector
torque
tube
by
removing
the
attachment
pin
located
at
the
bottom
of
the
lever.
8.
Remove
the
tunnel
plate
just
aft
of
the
tee
bar
by
laying
back
enough
tunnel
carpet
to remove
the
plate
attachment
screws.
9.
Remove
the
two
aileron
control
cable
pulleys
(13)
attached
to
the
lower
section
of
the
tee
bar
by
removing
the
pulley
attachment
bolt
(14).
SURFACE
CONTROLS
Revised:
7/28/75
1G16