Aileron Control Cables Installation - Piper PA-32R-301 SARATOGA SP Maintenance Manual

AILERON CONTROLS (cont)
D. Aileron Control Cables Removal (Refer to Figure 8) (cont)
(3) To remove primary control cable in either wing:
(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 open-
ing 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) To remove either balance cable:
(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 removed, 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,
washer and bolt.
(e) Draw the cable from the wing
E. Aileron Control Cables Installation (Refer to Figure 8)
(1) To install left or right primary control cable:
(a) Draw cable through fuselage floor tunnel.
(b) Connect cable to the end of control chain and secure using bushing, bolt, nut and cotter pin.
(c) Place cable around pulley located in the tunnel below the fuel selector.
(d) Position cables and install cable pulleys that attach to lower section of tee bar assembly.
Secure with bolt, washer and nut.
(e) Place the cable around pulley located in floor opening just aft of main spar.
(f) If primary control cable in the wing is already installed, connect control cable ends at
turnbuckle located in floor opening aft of main spar.
(g) Check rigging and adjustment per Rigging and Adjustment of Aileron Controls.
(h) Position heat duct and secure with screws.
(i) Install tunnel plate aft of tee bar assembly and secure with screws.
(j) Put floor carpet in place and secure.
(k) Install lower and upper selector covers and secure with screws.
(l) Place fuel selector knobs in place and secure with set screws.
(2) To install primary control cable in left or right wing:
(a) Draw control cable into wing.
(b) Connect cable to the forward end of aileron bellcrank using a bolt, washer, nut and cotter pin.
Allow cable end to rotate freely on bellcrank.
(c) If primary control cable is already installed in fuselage, connect ends at turnbuckle located
under rear seat aft of main spar.
(d) Check rigging and adjustment per Rigging and Adjustment of Aileron Controls.
(e) Install access plate on underside of wing.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
2B13
27-10-00
Page 27-15
Reissued: July 1, 1993