Cessna 182 1978 - Inclinometer for Measuring Control Surface Travel; Ailerons; Cables and Pulleys

AVAILABLE
FROM
THE
CESSNA
SUPPLY
DIVISION
(TOOL
NO.
SE
716)
Figure 6-4. Inclinometer
for Measuring Control Surface
Travel
NOTE
d. Remove
cable guards
and pulleys
as necessary
to work cables
free of aircraft.
Brass
washers (11) may
be used as shims
between
lower end of
bellcrank and wing
NOTE
structure. Retain these shims. Tape
open
ends of
bellcrank
to prevent
dust
and
To
ease routing
of cables,
a
length of
wire
dirt
from
entering
bellcrank
needle
bearings
may
be
attached
to
end of
cable
before
(13).
being
withdrawn
from
aircraft.
Leave
wire
in
place,
routed
through
structure;
then
6-10.
REPAIR.
Repair
of
bellcranks
consists
of
attach cable
being
installed
and use
to pull
replacement
of defective
parts.
If needle
bearings
cable
into
position.
are dirty
or in need
of lubrication,
clean
thoroughly
and
lubricate
as outlined
in
Section
2.
e. After
cable
is routed
in
position,
install
pulleys
and cable
guards. Ensure
cable
is positioned
in pul-
6-11.
INSTALLATION.
ley
groove
before
installing
guard.
a. Place
bushing
(14) and
stop bushing
(7) in
bell-
f. Re-rig
aileron
system
in accordance
with para-
crank
(8) and
position
bellcrank
in wing.
graph
6-18, safety
turnbuckles
and
install
access
b.
Install
brass washers
(11) between
lower
end
of
plates,
fairings
and upholstery
removed
in step
"a."
bellcrank
(8) and
wing structure
to shim
out excess
clearance.
6-14. AILERONS.
(See figure
6-3.)
c. Install
bellcrank
pivot bolt (4).
d. Position
bellcrank
stop-bushing
(7)
and install
6-15.
REMOVAL.
attaching
bolt (6).
a.
Disconnect
push-pull
rod (12) at
aileron.
e. Connect
control
cables to
bellcrank.
b. Remove
screws
and nuts
attaching aileron
hinges
f. Connect push-pull rod (12) to bellcrank. (1) to trailing edge of wing.
g. Re-rig
aileron system
in accordance
with para-
c. Using care,
pull aileron
out and down
to slide
graph 6-18, safety
turnbuckle
(5) and reinstall
all hinges
from under
wing skin and
auxiliary spar rein-
items removed
for access.
forcements.
6-12.
CABLES
AND
PULLEYS.
(See
figure
6-16.
INSTALLATION.
6-1.)
a.
Position
aileron
hinges between
skin
and auxil-
iary spar
reinforcements
and
install screws
and nuts
6-13. REMOVAL AND INSTALLATION. attaching hinges to trailing edge of wing.
a. Remove access plates, wing
root fairings and b. Attach
push-pull rod (12) to aileron.
upholstery
as
required.
b. Remove
safety wire
and relieve
cable tension
at
NOTE
turnbuckles
(8).
c. Disconnect
cables from
aileron bellcranks
(7)
If rigging
was correct
and push-pull
rod
and quadrants
(index
24,
figure 6-2).
adjustment
was
not disturbed,
it should
not be
necessary
to re-rig
system.
6-8