Piper Cherokee Six - Page 182

PIPER
CHEROKEE SIX
SERVICE MANUAL
5.
Install the
cable guard
at the
cable pulleys
(35) in
the aft lower
section
of the fuselage
forward
of the
cable turnbuckles.
6. Install
the cable
guard plate
(33) at
the underside
of the
pulley cluster
(34)
located
in the aft
area of the
aft floor
tunnel and
secure with
screws.
7. Install
the roll pin
type cable
guard (38)
at the
underside
of the pulleys
(36)
located in
the forward
area of the
aft floortunnel
and secure
it with
a cotter
pin.
8. Install the
cable rub blocks
(39) located on
the aft side of
the main spar
housing
and
secure
with
screws.
9. Remove
the blocks
that secure
the aft trim cable
and check
that the
cables are
seated on their
pulleys.
10. Set cable
tension
and check
rigging and
adjustment
per paragraph
5-21.
Check
safety of
all turnbuckles.
11.
Install the tunnel
cover on the
forward tunnel
and secure with
screws.
12. Install
the carpet
over
the floor
tunnel.
13. Install
the heat deflectors on
each side of the floor tunnel.
14. Install the cover over the trim control wheel and secure with screws
and special
washers.
15. Install
the seat
belts removed
from
thetopof
the floortunneland
secure
with bolt,
washer and
nut.
16. Install the floor panel and
seat belt attachments aft of
the main spar,
and secure
panel with screws.
17.
Install the
aft floor
tunnel and secure
with
screws.
18. Install the carpet
over the aft floor
tunnel.
19.
Install
the trim plate
on top
of the forward
end of
the aft floor
tunnel.
c. Install
the panel
to the
aft section
of the
airplane
and the seats.
5-19.
REMOVAL
OF STABILATOR
TRIM CONTROLS
(AFT). (Refer
to Figure
5-8.)
a. Remove the access panel to the aft section of the fuselage.
b. Block
the trim cables
at the first set
of pulleys (35)
forward of the cable
turnbuckles
(10 and 11)
in the aft section
of the fuselage
by a method shown
in
Figure
5-7.
c. Disconnect the cable (12)
at the turnbuckles (10 and 11) in
the aft section
of the fuselage.
d. Remove the
tail cone by removing
its attachment screws.
e. Disconnect
the link (25) between the trim
screw (23) and the trim control
arm (28) by removing the nut, washer and bolt (24) that connects the link to the
screw.
f. Remove the cotter pin from the top of the screw (23), and turn the screw
down and out of the barrel (20).
SURFACE
CONTROLS
Issued:
8/17/72
1H14