Piper Cherokee Six - Page 120

PIPER
CHEROKEE
SIX
SERVICE
MANUAL
4-10.
REMOVAL
AND
INSTALLATION
OF
STABILATOR.
The
complete
stabilator
assembly
can be
removed
by
following
the procedure
given
below:
a.
Remove
the tail
cone
assembly.
b.
Relieve
the tension
on the
trim
cable
and remove
the
trunnion
assembly.
c. From
inside
the
fuselage
disconnect
the
two
stabilator
control
cables
from
the
stabilator
balance
arm
assembly.
d. Remove
the
two
hinge
bolts
at
the
pivot
points
and
remove
the
stabilator
as a
complete
assembly.
e.
Reinstall
the
stabilator
in reverse
of
removal
instructions.
Tension
trim
cable
and
stabilator
control
cables
to
specifications
given
in Table
V-I. Section
V.
NOTE
Check
the
surface
for
proper
travel
and
all turnbuckles,
pins,
etc.
for
safety.
4-11.
REMOVAL
AND
INSTALLATION
OF
FIN.
a.
Remove
the
tail cone
fairing
and fairing
at the
forward
edge
of the
fin.
b.
Remove
the
rudder.
(Refer
to Paragraph
4-9.)
c.
Disconnect
the antenna
wire
from
the antenna
assembly,
attach
a fish
line to
the
antenna
cable
before
removing
it
from
the fin.
d.
Separate
the
stabilator
trim
cable
at turnbuckle,
and
remove
the cable
from
the
trim
mechanism.
e.
Remove
the one
bolt at
the leading
edge
of the
fin.
f.
Remove
the
two
bolts which
secure
the trim
mechanism
to the
fin
spar. Remove
the
four
bolts which
secure
the
fin spar
to the
aft bulkhead.
Remove
the fin.
g.
Install
the
fin in
reverse
of
removal
instruction
using
Figure
4-1a
as reference
for
proper
hardware
and
torques.
Check
all bolts
for
safety.
NOTE
Modifications
to
the fuselage
are
permissible
if they
do not
involve
alterations
to
the primary
structure.
It is
recommended
that the
manufacturer
be contacted
for
information
regarding
specific
alterations
proposed.
4-12.
REMOVAL
AND
INSTALLATION
OF DOOR
LOCK ASSEMBLY.
a.
Remove
door
latch
assembly
by
removing
door trim
upholstery
and
removing
screws
attaching
latch
plate
and
latch
assembly
to door.
b. Disconnect
latch
pull
rod
from
inside
door
handle.
c. Remove
complete
latch
assembly.
d.
Install the
door latch
in reverse
of
the removal
instructions.
STRUCTURE
1E24
Revised:
11/4/83