Piper Arrow IV Turbo Maintenance Manual page 250

2. The primary control cable in either wing may be installed by the following procedure:
A. Draw the control cable into the wing.
B. Connect the cable to the forward end of the aileron bellcrank using a bolt, washer, nut and cotter
pin. Allow the cable end to rotate freely on the bellcrank.
C. If the primary control cable in the fuselage is installed, connect the ends at the turnbuckle located
under the rear seat aft of the main spar.
D. Check rigging and adjustment per Rigging and Adjustment of Aileron Controls.
E. Install the access plate on the underside of the wing.
3. Either balance cable may be installed by the following procedure:
A. Draw the cable into the wing.
B. Connect the cable to the aft end of the aileron bellcrank using a bolt, washer, nut and cotter pin.
Allow the cable end to rotate freely on the bellcrank.
C. Connect the balance cable ends at the turnbuckle that is located under the rear seat aft of the main
spar.
D. If the left cable was removed, install the cotter pin cable guard at the pulley located within the
fuselage, aft of the main spar.
E. Check rigging and adjustment per Rigging and Adjustment of Aileron Controls.
F. Install the access plate on the underside of the wing.
4. Replace the rear seat bottom or floor panel and the two front seats.
REMOVAL OF AILERON BELLCRANK ASSEMBLY. (Refer to Figure 27-3.)
1. Remove the bottom half of the rear seat of the airplane.
2. Remove the access plate to the aileron bellcrank located on the underside of the wing, forward of the
center of the aileron.
3. Relieve tension from the aileron control cables by loosening the balance cable turnbuckle located in
the opening aft of the main spar.
4. Disconnect the primary and balance control cables from the bellcrank assembly by removing cotter
pins, nuts, washers and bolts.
5. Disconnect the aileron control rod at the aft or forward end, as desired, by removing the cotter pin, nut,
washer and bolt.
6. Remove the nut, pivot bolt and washers that secure the bellcrank. The nut is visible from the underside
of the wing.
7. Remove the bellcrank from within the wing.
INSTALLATION OF AILERON BELLCRANK ASSEMBLY. (Refer to Figure 27-3.)
1. Ascertain that the bellcrank pivot bushing is lubricated and install in the torque tube portion of the
bellcrank.
2. Place the bellcrank in position in the wing with a washer located between each end of the torque tube
and the mounting brackets.
3. Install the bellcrank pivot bolt with the head up. Install a washer and nut on the bolt, and torque nut
within 20 to 25 inch-pounds. Check that the bellcrank rotates freely with little up-down play.
4. Install and adjust control rod and check aileron travel per Rigging and Adjustment of Aileron Controls.
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
1K10
27-10-04
Page 27-15
Revised: February 23, 1979