Installation Of Aileron Control Cables - Piper Lance II Service Manual

LANCE II SERVICE MANUAL
5. Separate the primary control cable (14 or 15) at the turnbuckle (12 or 16)
located in the floor opening aft of the main spar.
6. Remove the cable pulleys (8) attached to the lower section of the control
column tee bar assembly by removing the pulley attachment bolt (21).
7. Move the cable guard (20) located under the pulley cluster (9) below the fuel
selector by removing the cotter pin from the exposed end of the guard and sliding it to the
left or right as required.
8. Remove the cotter pins used as cable guards at the pulley (10) in the forward
area of the floor opening aft of the main spar.
9. Disconnect the cable (14 or 15) from the control chain (4) at the control
column tee bar assembly by removing the cotter pin, nut, bolt and bushing (23) that
connect the two together. Secure the chains in some manner to prevent them from
unwrapping from around the sprockets.
10. Draw the cable back through the floor tunnel.
c. The primary control cable (13 or 17) in either wing may be removed by the
following procedure:
1. Remove the access plate to the aileron bellcrank (6) located on the underside of
the wing forward of the inboard end of the aileron.
2. If not previously disconnected, separate the cable at the turnbuckle (12 or 16)
located in the floor opening aft of the main spar.
3. Disconnect the pulley guard cotter pin from pulley (28).
4. Disconnect the cable from the forward end of the aileron bellcrank by removing
the cotter pin, nut, washer and bolt.
5. Draw the cable from the wing.
d. Either balance cable (18 or 19) may be removed by the following procedure:
1. Separate the balance cable at the turnbuckle (24) in the right side of the floor
opening aft of the main spar.
2. If the left balance cable is to be removed, remove the cotter pin used as a cable
guard at the pulley ( 1) in the center of the floor opening.
3. Remove the access plate to the aileron bellcrank (6) located on the underside of
the wing forward of the inboard end of the aileron.
4. Disconnect the cable from the aft end of the aileron bellcrank by removing the
cotter pin, nut, washer and bolt.
5. Draw the cable from the wing.
5-8. INSTALLATION OF AILERON CONTROL CABLES. (Refer to Figure 5-2.)
a. The installation of either the right or left primary control cable (14 or 15) that is
located in the fuselage may be accomplished as follows:
1. Draw the cable through the fuselage floor tunnel.
2. Connect the cable to the end of the control chain (4) and secure using bushing,
bolt, nut and cotter pin (23).
3. Place the cable around the pulley (9) that is located in the tunnel, below the fuel
selector. Install cable guard (20) and secure with cotter pin.
4. Position cables and install the cable pulleys (8) that attach to the lower section
of the tee bar assembly. Secure with bolt, washer and nut (21).
5. Place the cable around the pulley (10) that is located in the floor opening just
aft of the main spar and install cotter pin cable guards.
6. If the primary control cable in the wing is installed, connect the control cable
ends at the turnbuckle (12 or 16) located in the floor opening aft of the main spar.
Issued:
1/3/78
F20SURFACE
CONTROLS
IF20-