Piper Arrow IV Turbo Maintenance Manual page 263

3. Either forward stabilator cable may be removed by the following procedure:
A. Remove the tunnel carpet and cover plate by the following procedure:
(1) Remove the rudder trim covers by removing the knobs and the attaching screws. Remove the
tunnel plate located just aft of the tee bar by laying back enough tunnel carpet to remove the
plate attaching screws.
B. If the right (upper) stabilator control cable is to be removed, remove the cotter pin guards at the
pulley located in the forward area of the tunnel.
C. Disconnect the cables from the lower end of the tee bar removing cotter pin, nut, washer and bolt.
D. Within the access opening aft of the main spar, remove the cable rub blocks that are attached to the
spar housing by removing the block attaching screws.
E. Remove the cotter pin cable guard at the pulley cluster located in the access opening aft of the
main spar.
To facilitate in the installation of control cables, a line may be
attached to the cable end prior to removal.
F. Draw the cable aft through the floor tunnel.
4. Either aft stabilator control cable may be removed by the following procedure:
A. Disconnect the cable end at the bellcrank of the stabilator by removing the cotter pin, nut, washer
and bolt.
B. Remove the cotter pin cable guard at the pulley located forward on lower cable. (See Figure 27-
14)
C. Remove the cable from the airplane.
INSTALLATION OF STABILATOR CONTROL CABLES. (Refer to Figure 27-14.)
1. The forward stabilator cables may be installed by the following procedure:
A. Draw the control cable through the floor tunnel. Ascertain that the right (upper) cable is routed
around the pulley(s) in the forward area of the floor tunnel.
B. Connect the cables to the lower end of the control column tee bar or the idler arm with bolt,
washer, nut and cotter pin. Allow the cable ends freedom to rotate.
C. If the aft control cable is not installed, install per Step 2.
D. Connect the control cable to the aft cable at the turnbuckle in the aft section of the fuselage.
E. For the right control cable, install the cotter pin cable guards at the pulley(s) in the forward area of
the tunnel.
F. Within the access opening aft of the main spar, install the cable rub blocks to the spar housing and
secure with screws.
G. In the access opening, install the cotter pin cable guard at the pulley cluster.
H. Set cable tension and check rigging and adjustment per Rigging and Adjustment of Stabilator
Trim.
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
—NOTE—
1K23
27-30-02
Page 27-28
Revised: February 23, 1979