Piper Cherokee Six - Page 161

PIPER CHEROKEE SIX SERVICE MANUAL
10. Disconnect
the stabilator
control
cables
(11)
from the
lower end
of the
tee bar
assembly.
11. Disconnect
the
necessary
control
cables,
such
as the propeller
pitch control,
mixture
control, etc.,
that will
allow the
tee bar
assembly
to be removed.
12.
Remove
the tee
bar assembly
by
removing
the
attachment
bolts
(15) 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
(PA-32-260
and 300).
(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
(15), washers
and nuts
inserted
in through each
side of
the floor
tunnel.
2. Connect
the
stabilator
control
cables
(11) to
the lower
end of
the tee
bar with
bolt,
washer,
nut and
cotter
pin (16).
Allow
the cable
ends
free to
rotate.
3.
Place the aileron
control
cables (12)
around
the pulleys
(13) that attach
to the
lower
section of
the tee
bar (5), position
pulleys
and
secure with
bolt, washers
and
nut (14).
4. Install
the
control
wheel
per
step
b.
5. Place
the control
wheels
in
neutral
(centered)
position
and
install the
aileron
control
chains
(7 and
8) on
the control
wheel
sprockets
(17
and
18) and
idler cross-over
sprockets
(19 and
21). The
turnbuckle
(9) must
be centered
between
the two
control
wheel
sprockets.
6. Loosen
the
connecting
bolts
(22) of
the idler
sprockets
(19 and
21) to
allow the
chain to
fit snug
around
the control
wheel
sprockets
and over
the idler
sprockets.
7. Connect
the
aileron
control
cables
(12)
to the
ends
of the
chains
(7 and
8) with
bolts, bushings,
nuts
and
cotter pins
(10).
8. Adjust
the
chain
turnbuckle
(9) between
the two
control
wheel
sprockets
to
allow
the control
wheels
to be
neutral and
obtain
proper cable
tension
as given
in Table
V-I.
It
may be
necessary
in order
to
have both
control
wheels
neutral
to set
the chain
turnbuckle
to
neutralize
the wheels
and then
set cable
tension
with the
turnbuckles
located
under the
floor
panel
aft of
the main
spar
as instructed
in paragraph
5-11.
Before safetying
the
turnbuckle,
check
that
when
the ailerons
are
neutral,
the control
wheels
will
be neutral
and
the chain
turnbuckle
centered.
Also the
aileron
bellcranks
should
contact
their
stops
before
the control
wheel
hits its stop.
Maintain .030
to .040 clearance
between
sprocket
pin and
adjustable
stop
bolts
on models
having
adjustable
tee
bar stops.
9. Set
stabilator
cable tension
with the
turnbuckle
in the aft section
of the
fuselage
and instructions
given
in paragraph
5-15. Check
safety
of
all turnbuckles
upon completion
of adjustments.
SURFACE
CONTROLS
Revised:
6/18/76
1G17