PIPER CHEROKEE
SIX 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 controlchain(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) ineither wing may
be removed by the
following procedure:
1. Remove
the access platetotheaileronbellcrank
(6) located on the under-
side 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 cable from the forward end of the aileron bellcrank by
removing the cotter pin, nut, washer and bolt.
4. Draw the cable from the wing.
d. Either balance cable (18 or 19) may be removed by the followingprocedure:
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 (11) in the center of the floor opening.
3. Remove the
access plate to the aileron bellcrank
(6) located on the un-
derside of the
wing forward of the inboard
end of the aileron.
4. Disconnect
the cable from the aft end
of the aileron bellcrank by
re-
moving 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
SURFACE CONTROLS
Issued: 8/17/72
1H1
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