THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 8
Jun 1/03
2J4
27-10-00
B. Installation (Refer to Figure 3.)
(1) To install left or right primary control cable in fuselage:
(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.
(3) To install left or right balance cable:
(a) Draw the cable into wing.
(b) Connect cable to the aft end of aileron bellcrank using a bolt, washer, nut and cotter pin.
Allow the cable end to rotate freely on bellcrank.
(c) Connect balance cable ends at turnbuckle located under rear seat aft of main spar.
(d) If left cable was removed, install cotter pin cable guard at pulley located within fuselage aft
of main spar.
(e) Check rigging and adjustment per Rigging and Adjustment of Aileron Controls.
(f) Install access plate on the underside of wing.
(4) Install floor panel, seat belt attachments, rear seat and two front seats.
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