Cessna 182 1978 - Rigging-Flap Control Lever and Follow-Up

MODEL
182
& T182
SERIES
SERVICE
MANUAL
7-19.
RIGGING-FLAP
CONTROL
LEVER
AND
NOTE
FOLLOW-UP.
(See
figure
7-3.)
a.
Run
flaps
to
full
UP
position.
An
inclinometer
for
measuring
control
sur-
b.
Remove
upholstery
and
headliner
as
necessary.
face
travel
is
available
from
the
Cessna
c.
Secure
follow-up
cable
(29)
to
retract
cable
(1)
Service
Parts
Center.
See
figure
6-4.
with
clamp
assembly
(6).
Torque
clamp
nut
(27)
to
40-50
inch-pounds
and
lock
with
a
second
nut.
i.
Repeat
step
"h"
for
20°
flap
position
(flap
travel:
d.
Pull
all
slack
from
follow-up
control
20±2°).
cable
and
with
position
indicator
(21)
in full
UP
j.
Adjust
flaps
UP
operating
switch
(23)
in
slotted
position,
connect
turnbuckle
(18)
to follow-up
cable.
holes
for .062
inch
clearance
between
switch
roller
e.
Connect
spring
(19)
to
arm
assembly
(20).
and
cam
(13)
when
the
flaps
DOWN
operating
switch
f.
Make
minor
cable
length
adjustments
using
has
just
opened
in
the
10
°
and
20
°
position.
turnbuckle
(18)
to
position
indicator
at 0
°
flaps.
g.
With
control
lever
(14) in
full
up position,
adjust
NOTE
switches
(23
and
25)
in
slotted
holes
until
cam
(13)
is
centered
between
switch
rollers.
Be
sure
control
Flap
travel
on
UP
cycle
may
deviate
a
maxi-
lever
(14)
is
in full
up position
during
this
adjustment.
mum
of 4
°
from
indicated
position.
h.
Mount
an
inclinometer
on
trailing
edge
of one
flap
and
set to
0
°
.
Turn
master
switch
ON
and
move
k. Turn
master
switch
ON
and run
flaps
through
control
lever
to 10
°
position.
If flap
travel
is more
several
cycles,
stopping
at
various
mid-range
set-
than
10±2
°
,
adjust
flaps
DOWN
operating
switch
(25)
tings
and
checking
that
cable
tension
is within
limits.
away
from
cam (13)
and
recycle
flaps.
If
flap travel
Retract
cable
tension
may
increase
to 90
pounds
when
is
less
than
10±2
°
,
adjust
flaps
DOWN
operating
flaps
are fully
retracted.
switch
(25)
closer
to
cam
(13) and
recycle
flaps.
1.
Check
all
rod
ends
and clevis
ends
for sufficient
thread
engagement,
all
jam
nuts
are
tight
and
reinstall
all
items
removed
for
access.
m.
Flight
test
aircraft
and
check
that
follow-up
con-
trol operates
smoothly
in flight.
SHOP
NOTES:
7-10