Aileron Control Cables Installation; Aileron Bellcrank Assembly Removal - Piper PA-44-180 SEMINOLE Maintenance Manual

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.
INSTALLATION OF AILERON CONTROL CABLES. (Refer to Figure 27-8.)
1. To install either the right or left primary control cable located in the fuselage:
A. Draw the cable through the fuselage floor tunnel.
B. Connect the cable to the end of the control chain and secure using bushing, bolt, nut and cotter
pin.
C. Place the cable around the pulley that is located in the tunnel, below the fuel selector. Install
cable guard and secure with cotter pin.
D . Position cables and install the cable pulleys that attach to the lower section of the tee bar assembly.
Secure with bolt, washer and nut.
E. Place the cable around the pulley that is located in the floor opening just aft of the main spar and
install cotter pin cable guards.
F. If the primary control cable in the wing is installed, connect the control cable ends at the turnb u c kle
located in the floor opening aft of the main spar.
G. Check rigging and adjustment.
H. Position the heat duct and secure with screws.
I. Install the tunnel plate aft of tee bar assembly and secure with screws.
J. Put the floor carpet in place and secure.
K. Install the lower and upper selector covers and secure with screws.
L. Place the fuel selector knobs in place and secure with set screws.
2. To install primary control cable in the left or right wing:
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
in the floor opening aft of the main spar.
D. Check rigging and adjustment.
E. Install the access plate on the underside of the wing.
3. To install either balance cable:
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 in the floor opening aft of the main spar.
D. If the left cable was removed, install the cotter pin cable guard at the pulley located in the center
of the floor opening.
E. Check rigging and adjustment.
F. Install the access plate on the underside of the wing.
G. Install the floor panel, seat belt attachments and seats.
AILERON BELLCRANK.
REMOVAL OF AILERON BELLCRANK ASSEMBLY. (Refer to Figure 27-9.)
1. Remove the the center seats, seat belt attachments.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
1K18
27-10-04
Page 27-16
Revised: June 20, 1995