Piper Cherokee Six - Page 112

PIPER
CHEROKEE SIX
SERVICE MANUAL
b. The PA-32R-300 and 32-300 with S/N 32-7940001 and up. wing tips are removed using
the following
steps.
1. Remove the
screws from around
the wing tip.
2. Pull
the tip away
from the
wing assembly
far enough
to gain access
for removal
of electrical connections for strobe and position lights.
3.
Remove the
tip from the wing.
c. Replacement of wing tip is reverse of removal instructions.
4-5. REMOVAL AND REPLACEMENT OF WING FLAPS.
Remove
the
access plate
at the
wing butt
rib.
b
Disconnect
the flap
push
rod.
c. Remove the three hinge bolts.
d. Pull
the flap straight
back
off the
wing.
e. Install
the flap
in reverse
of removal
instructions.
4-6. REMOVAL
AND REPLACEMENT
OF AILERON.
a.
Disconnect
the aileron
push
rod at the
inboard
end of the
aileron.
b. Remove the eight
bolts which hold the aileron to
the wing assembly.
c.
Remove the aileron
by lowering
the inboard end first,
then swing forward
so the
balance
assembly
will clear
the outboard
portion of the
wing.
d. Install the aileron in reverse of removal instructions.
4-7. REMOVAL AND REPLACEMENT OF WING.
a.
Remove wing root fairings
and all wing inspection
panels.
b. Drain
gas from the desired
wing. (Refer
to Draining Fuel
System. Section
II.)
c. Drain brake lines
and reservoir. (Refer to Draining
Brake System. Section II.)
d.
Remove
seats,
floor panels
and
side panels
as required.
e. Set the airplane
on jacks. (Refer to
Jacking, Section II.)
f. Disconnect aileron
balance cables at aileron bellcranks
and aileron control cables at
center of fuselage.
g. Disconnect
the fuel lines
at the wing butt.
h. Disconnect the airspeed lines.
i. Disconnect brake line and electrical wiring.
j. On PA-32R-300
disconnect landing
gear retraction hydraulic lines.
k. Arrange a suitable fuselage
support cradle and remove
the wing jacks.
1. Remove the eighteen spar
bolts and the bolts on the front
and rear spar.
m. Remove the wing.
n. Reinstall
wing
in reverse
of removal
instructions.
(Torque bolt
heads on
upper spar
cap and nuts on lower spar cap from 360 to 390 inch-pounds.)
STRUCTURE
Revised:
8/3/81
1E16