Piper PA-32RT-300T User Manual

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
control
cable
(13
or
17)
in
either
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.
Install
the
pulley
guard
cotter
pin
for
pulley
(28).
4.
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.
5.
Check
rigging
and
adjustment
per
Paragraph
5-11.
6.
Install
the
access
plate
on
the
underside
of
the
wing.
c.
Either
balance
cable
(18
or
19)
may
be
installed
by
the
following
procedure:
1.
Draw
the
cable
into
the
wing.
2.
Connect
the
cable
to
the
aft
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.
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.
5-9.
REMOVAL
OF
AILERON
BELLCRANK
ASSEMBLY.
(Refer
to
Figure
5-2.)
a.
Remove
the
floor
panel
located
directly
aft
of
the
main
spar
by removing
the
center
seats,
seat
belt
attachments
and
the
screws
securing
the
floor
panel.
Lift
the
panel
and
remove
from
the
airplane.
b.
Remove
the
access
plate
to
the
aileron
bellcrank
(6)
located
on
the
underside
of
the
wing,
forward
of
the
inboard
end
of
the
aileron.
c.
Relieve
tension
from
the
aileron
control
cables
by
loosening
the
balance
cable
turnbuckle
(24)
located
in
the
floor
opening
aft
of the
main
spar.
d.
Disconnect
the
primary
(13
or 17)
and
balance
(18
or
19)
control
cables
from
the
bellcrank
assembly
by
removing
cotter
pins,
nuts,
washers
and
bolts.
e.
Disconnect
the
aileron
control
rod
(7)
at the
aft
or
forward
end,
as desired.
f.
Remove
the
nut,
pivot
bolt
(25)
and
washers
that
secure
the
bellcrank.
The
nut
is
visible
from
the
underside
of
the
wing.
g.
Remove
the
bellcrank
from
within
the
wing.
Issued:
1/3/78
SURFACE
CONTROLS
1F22
LANCE
II SERVICE
MANUAL

Piper PA-32RT-300T Specifications

General

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