Removal Of Aileron Bellcrank Assembly - Piper APACHE PA-23-235 Service Manual

PIPER AZTEC SERVICE MANUAL
7. Install the cable to the aft aileron pulleys (15) and secure in place with
bolt, guard clip (11), rub-block (12), washers and nut.
8. Install the aileron rub-blocks (5) to the fuselage frame on each side of
the forward cabin area.
9. Install the cable to the forward pulleys (7) and secure them in place
with bolt, washers and nut.
10. Secure the left front floor plate using a machine screw in the aft left
corner, and a bolt and nut in the forward left corner.
II. Apply plastic tape around the edge of the left front floor plate to cover
rough edges and provide a seal between the floorboards and the plate.
12. Wrap the cables around the control column pulley (9) and install the
pulley to the lower end of the control column with bolt, washers and nut.
13. Connect the turnbuckle assemblies (8) to the chainonthe control column.
14. Install the pulley covers on the front floor plates on each side.
c. Set cable tension per Table V-I and check control cable rigging and adjust-
ment per paragraph 5-13.
NOTE
If an autopilot is installed, consult the bottom of the Section
XII (Electronics) Table of Contents page (Aerofiche Grid
5A9) for the part number of the appropriate Service Manual
for information on installation of the bridle cable.
d. Install all access plates, panels and trim.
5-11.
REMOVAL OFAILERON BELLCRANK ASSEMBLY. (Refer to Figure 5-3.)
a. Remove the access plate to the bellcrank assembly.
(Refer to Access and
Inspection Providions, Section II.)
b. Relieve cable tension from the control system by rotating one of the turn-
buckles attached to the bellcrank.
c. Disconnect the turnbuckle ends from the forward and aft ends of the bell-
crank (25) by removing cotter pin, nut, washer and clevis bolt.
d. Disconnect the aileron control tube (23) at the bellcrank.
e. Remove the pivot bolt securing the bellcrank by first bending the corners
of the bolt stop (26) away from the nut and removing the nut and bolt.
f. Remove the bellcrank (25) from the wing.
g. The stop block (28) may be removed by unbolting it and removing it from
the wing.
SURFACE CONTROLS
1J12
Reissued: 2/18/81
1J 12