Piper Cherokee Six - Page 170

PIPER
CHEROKEE
SIX SERVICE
MANUAL
the
fuel selector.
Install
cable
guard
(20) and
secure
with
cotter
pin.
4.
Position
cables
and
install
the
cable
pulleys
(8) that
attach
to
the lower
section
of the
tee
bar assembly.
Secure
with
bolt,
washer
and nut
(21).
5.
Place
the cable
around
the
pulley
(10)
that
is located
in the
floor
opening
just
aft of
the main
spar
and
install
cotter
pin
cable
guards.
6.
If
the primary
control
cable
in the
wing
is
installed,
connect
the
con-
trol
cable
ends
at the
turnbuckle
(12
or 16)
located
in the
floor
opening
aft
of the
main
spar.
7.
Check
rigging
and adjustment
per paragraph
5-11.
8. Position
the heat
duct and
secure
with
screws.
9.
Install
the tunnel
plate
aft of tee
bar assembly
and secure
with
screws.
10. Put
the
floor carpet
in place
and
secure.
11.
Place
the
fuel
selector
lever
on
the
selector
torque
tube
and secure
with
pin and
cotter
pin.
12. Install
the
lower
and
upper
selector
covers
and
secure
with
screws.
b.
The primary
controlcable
(13
or
17) ineither
wing
may
be installed
by
the
following
procedure:
1. Draw
the
control
cable
into the
wing.
2. Connect
the
cable
to the
forward
end
of the
aileron
bellcrank
(6)
using
a bolt,
washer,
nut
and cotter
pin.
Allow
the
cable
end to
rotate
freely
on
the
bellcrank.
3.
If
the
primary
control
cable
in
the
fuselage
is installed,
connect
the
ends
at the
turnbuckle
(12 or
16)
located
in the
floor
opening
aft of
the main
spar.
4.
Check
rigging
and adjustment
per
paragraph
5-11.
5.
Install
the
access
plate
on the
underside
of the
wing.
c.
Either
balance
cable
(18 or
19) may
be
installed
bythe
following
procedure:
1. Draw
the
cable
into the
wing.
2. Connect
the cable
to
the aft
end of
the aileronbellcrank
(6)
using
a bolt,
washer,
nut
and
cotter
pin.
Allow
the cable
end to
rotate
freely
on
the bellcrank.
3.
Connect
the
balance
cable
ends
at the
turnbuckle
(24) in
the floor
opening
aft
of
the
main
spar.
4.
If the
left
cable
was
removed,
install
the
cotter
pin
cable
guard
at
the
pulley
(10)
located
in the
center
of
the floor
opening.
5.
Check
rigging
and
adjustment
per
paragraph
5-11.
6.
Install
the
access
plate
on the
underside
of the
wing.
7. Install
the
floor
panel,
seat
belt
attachments
and seats.
SURFACE
CONTROLS
Issued:
8/17/72
H
1H2