Piper PA-32RT-300T User Manual

LANCE
II SERVICE
MANUAL
3. Remove the floor panel located directly aft of the main spar by removing the
center seats,
seat belt attachments
and the screws
securing the panel.
Lift the panel
and
remove from airplane.
4. Within
the floor opening, remove the
cable rub blocks (10) that are attached
to
the spar housing by removing
the block attachment screws. Also remove
the cotter pin cable
guard at the pulley cluster (6) in the aft area of the opening.
5.
Remove the fuel
selector panel cover
by removing
the rudder trim knob
and the
cover attachment screws.
6. Remove the lower
selector cover and disconnect
the fuel selector control lever
from the selector torque tube by
removing the attachment pin located at
the bottom of the
lever.
7. Remove the tunnel plate just aft of the tee bar by removing enough carpet from
the tunnel to allow the plate
attachment screws and plate
to be removed.
8. If the right (upper) stabilator
control cable (2) is to be removed,
remove the
cotter pin cable guards at
the pulley (14) located in the forward
area of the tunnel.
9. Disconnect the cables
(2 and 3) from the lower end of
the tee bar by removing
cotter pin, nut, washer and bolt (15).
10. Draw the cable
aft through the floor
tunnel.
d. Either aft stabilator control cable (4 or 5) may be removed by the following
procedure:
1. Disconnect the cable
end at the bellcrank (20) by removing
the cotter pin, nut,
washer
and
bolt (8).
2. Remove the
cable guard pin at
the pulley (7).
3. Remove the cable from the airplane.
5-14.
INSTALLATION OF STABILATOR
CONTROL CABLES. (Refer to Figure
5-5.)
a. The forward stabilator cables (2 and 3) may be installed by the following procedure:
1. Draw
the control cable through the
floor tunnel. Ascertain that the right
(upper)
cable (2) is routed
around the pulley (14) that is in the
forward area of the forward floor
tunnel.
2. Connect the
cables (2 and 3)
to the lower end
of the control column
tee bar (1)
with
bolt, washer, nut and cotter pin
(15). Allow the cable to be free
to rotate.
3. If the aft control
cable (4 or 5) is not installed,
install per Step b.
4. Connect
the control cable
to the aft cable
at the turnbuckle
(16) in the
aft
section of the fuselage.
5.
For the right control
cable (2), install
the cotter
pin cable guard at
the pulley
(14) in the forward area of the tunnel.
6.
Within the forward
area of the
floor opening aft
of the main spar,
install the
cable rub blocks (10) to the spar housing and secure with screws.
7. In the aft area of the floor opening, install the cotter pin cable guard at the
pulley cluster (6).
8. Install the cable guard (11) under the pulley cluster (19) located in the aft area
of the aft floor tunnel and secure with screws.
9. Set cable tension and check
rigging and adjustment per Paragraph
5-15.
10. Install the tunnel plate directly aft of the tee bar assembly and secure with
screws.
11. Put the floor carpet in place and secure.
12. Place the fuel selector lever on the selector torque tube and secure with pin and
safety
with cotter
pin.
Issued:
1/3/78
SURFACE CONTROLS
1G4

Piper PA-32RT-300T Specifications

General

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