Piper PA-34-200T Seneca II User Manual

PIPER SENECA
I SERVICE
MANUAL
5.
Tie
the cables
forward
to prevent
them
from
slipping
back
into
the
floor
tunnel.
e. The
trim
control
cables (19)
may
be removed
by the
following
procedure:
1.
Remove
the center
seats
and the
pilot
and
rear
seats
if desired.
2.
Remove
the seat
belts
attached
to the
forward
floor
tunnel by
removing
attachment
nuts,
washers
and bolts.
3.
Unfasten
the carpet
from
the
aft portion
of
the forward
floor
tunnel
and lay
it forward.
4. Remove
the tunnel
cover
located
between
the
trim control
wheel
and the
spar
cover
by
removing
attachment
screws.
5. Remove
the cable
pulleys
(3) located
in the forward
tunnel by
removing
the
cotter
pin,
washer and clevis pin.
6. Remove
the floor
panel
aft of the
main
spar by
removing
the panel
attachment
screws
and
seat
belt
attachments.
Lift
the panel
and
remove
from
airplane.
7. Remove
the
cable
rub blocks
(39)
located
in the
floor opening
on
the aft
side of
the main
spar
by removing
the block
attachment
screws.
8.
Remove
the
carpet and
the
heater
duct over
the
aft floor
tunnel.
9. Remove
the cover
plate
from
the top
of the
aft floor
tunnel
by
removing
attachment
screws.
10. Remove
the cable
guard
(see
Sketch
A)
from
the underside
of the
trim
cable pulleys
(4)
located
at station
130.167
by removing
the
cotter
pin
and withdrawing
the roll
pin.
11.
Remove
the
cable fairlead
(see
Sketch
B) from
the
underside
of the
pulley
cluster
(5)
located
at station
166.837
by
removing
the
plate
attachment
screws.
12. With
the
cables
disconnected
from
the trim
control
wheel,
draw the
cable(s)
through
the
floor tunnel.
5-18. INSTALLATION
OF
STABILATOR
TRIM
ASSEMBLY
(FORWARD).
(Refer
to Figure
5-5.)
a.
The trim
control
wheel
with
drum may
be
installed
by the
following
procedure:
1. Wrap
the right
trim
cable on
the trim
drum
by inserting
the swaged
ball
of the
cable in
the
slot provided
in the
side (right
side)
of the
drum that
mates
with
the control
wheel,
and
looking
at this
side,
wrap the drum
with three
and a
half wraps
of the cable
in a clockwise
direction.
2. Attach
the
control
wheel
to
the cable
drum
by
aligning
the long
lug
of the
drum
with
the
long slot
of the wheel
and securing
the
two pieces
together
with three
screws.
3.
Wrap
the left
trim
cable
on the
drum
by inserting
the
swaged
ball
of the
cable
in the
slot
provided
in
the flanged
side (left side)
of the drum
and looking
at this
side, wrap
the drum
with three
and a
half
wraps of the cable
in a clockwise direction.
4.
Lubricate
and
install
the
bushing
in
the control
wheel
and
drum.
5.
Align the
control
cables
and position
the control
wheel
assembly
between
its
mounting
brackets.
Ascertain
that the
end of
the trim
indicator
wire is
positioned
in the
spiraled
slot of the
drum
with
no bind
on
the end.
Install
the retainer
bolt
from the
left side
and
install washer
and
nut.
6.
Install
the
cover
over
the
control
wheel
and
secure
with
screws,
unless
the control
cables
have
yet
to
be installed.
b. The
trim
control
cables (19)
may
be installed
by the
following
procedure:
1.
Draw
the cable(s)
through
the
floor
tunnel.
2. Wrap
the
cable
drum
and install
the
trim
control
wheel
as given
in
Step
a.
3. Position
the
cable
pulleys
(3)
on the
mounting
bracket
and
install
the
clevis
pin,
washer
and
cotter pin.
4.
Connect
the cable
(19)
to
the
aft cable
(16)
at
the turnbuckle
(17)
in
the aft
section
of
the
fuselage.
Install
aft cable (16)
if not
installed.
Reissued:
10/11/79
SURFACE
CONTROLS
1G18
Island Enterprises

Piper PA-34-200T Seneca II Specifications

General

Brand	Piper
Model	PA-34-200T Seneca II
Category	Tools
Language	English