THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 19
Jun 1/03
3J9
35-10-00
(d) Remove retaining nut from rear of control knob.
(e) Pull cable from airplane through instrument panel. Retrieve retainer nut as cable bitter end
pulls through the instrument panel.
(2) Installation
(a) Insert cable through instrument panel. Slide retainer nut onto cable and secure control
knob to instrument panel.
(b) Feed cable up through windshield centerpost and along H. P. Gauge feed line to
cylinder.
(c) Secure cable to H. P. Gauge feeder line and structure with same number of tie wraps,
CR-2M ring connectors and clamps installed at same locations as those cut or loosened
to remove cable.
(d) Trim cable shield and core to allow sufficient material to make a two turn loop, two inches
(5.08 cm) from the end of the shield.
(e) Bend core wire end for 1 1/2 to 2 turns with 0.188 (0.478 cm) inside diameter.
(f) Place loop over pin on regulator control arm and secure with washer and cotter pin.
Secure cable with retaining screw and clamp to cable support bracket
(g) Check operation, adjust as required.
(h) Replace and secure overhead panels in the cabin.
(i) Replace and secure finished bulkhead in aft cabin. If used, remove tailstand.
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