Installation Of Stabilator Control Cables - Piper Lance II Service 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