Piper SARATOGA PA-32-301 Maintenance Manual page 233

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
F.
Remove the cable pulleys attached to the lower section of the control column tee bar assembly by
removing the pulley attachment bolt.
G.
Mo\e the cable guard located under the pulley cluster below the fuel selector by removing the
cotter pin from the exposed end of the guard and sliding it to the left or right as required.
H.
Remove the cotter pins used as cable guards at the pulley in the forward area of the floor opening
aft of the main spar.
I.
Disconnect the cable from the control chain at the control column tee bar assembly by removing
the cotter pin, nut. bolt and bushing that connect the two together. Secure the chains in some manner to
prevent them from unwrapping from around the sprockets.
J.
Draw the cable back through the floor tunnel.
3. The primary control cable in either wing may be removed by the following procedure:
A. Remove the access plate to the aileron bellcrank located on the underside of the wing forward of
the inboard end of the aileron.
B. If not previously disconnected, separate the cable at the turnbuckle located in the floor opening
aft of the main spar.
C.
Disconnect the pulley guard pin from pulley.
D. Disconnect the cable from the forward end of the aileron bellcrank by removing the cotter pin.
nut. washer and bolt.
E. Draw the cable from the wing.
4.
Either balance cable may be removed by the following procedure:
A. Separate the balance cable at the turnbuckle in the right side of the floor opening aft of the main
spar.
B. If the left balance cable is to be remo ed. remove the cotter pin used as a cable guard at the pulley
in the center of the floor opening.
C.
Remove the access plate to the aileron bellcrank located on the underside of the wing forward of
the inboard end of the aileron.
D. Disconnect the cable from the aft end of the aileron bellcrank by removing the cotter pin, nut.
asher and bolt.
E. Draw the cable from the wing.
INSTALLATION OF AILERON CONTROL CABLES. (Refer to Figure 27-3.)
I.
The installation of either the right or left primary control cable that is located in the fuselage maybe
accomplished as follows:
A. Draw the cable through the fuselage floor tunnel.
B. Connect the cable to the end of the control chain and secure using bushing. bolt. nut and cotter
pin.
C. Place the cable around the pulley that is located in the tunnel below the fuel selector.
D. Position cables and install the cable pulleys that attach to the lower section of the tee bar
assembly. Secure with bolt. washer and nut.
E. Place the cable around the pulley that is located in the floor opening just aft of the main spar.
F.
If the primary control cable in the wing is installed, connect the control cable ends at the
turnbuckle located in the floor opening aft of the main spar.
G. Check rigging and adjustment per Rigging and Adjustment of Aileron Controls.
H. Position the heat duct and secure with screws.
I.
Install the tunnel plate aft of tee bar assembly and secure with screws.
J.
Put the floor carpet in place and secure.
K. Install the lower and upper selector covers and secure with screws.
L. Place the fuel selector knobs in place and secure with set screws.
27-11-02
Page 27-13
Revised: August 11, 1983
1J17