Cessna T188C - Page 122

MODEL
188
&
T188
SERIES
SERVICE
MANUAL
6-3.
TROUBLE
SHOOTING
(Cont).
TROUBLE
PROBABLE
CAUSE
REMEDY
RESISTANCE
TO
CONTROL
Cables
too
tight.
Adjust
cables
to
proper
tension.
STICK
MOVEMENT.
STICK
MOVEMENT,
Pulleys
binding
or
cable
off.
Replace
defective
pulleys.
Install
cables
correctly.
Bellcranks
distorted
or
Replace
bellcranks.
damaged.
Defective
bearings
in
torque
Replace
defective
parts.
tube
assembly.
Clevis
bolts
in
system
too
Loosen,
then
tighten
properly.
tight.
Aileron-rudder
interconnect
Install
springs
properly.
springs
improperly
installed
Replace
damaged
springs.
or
damaged.
CONTROL
STICK
NOT
Improper
adjustment
of
Adjust
in
accordance
with
CENTERED
WITH
AIL-
cables.
paragraph
6-16.
ERONS
IN
NEUTRAL
(DROOPED)
POSITION.
Improper
adjustment
of
Adjust
push-pull
rods
to
obtain
aileron
push-pull
rods.
proper
alignment.
INCORRECT
AILERON
Push-pull
rods
not
adjusted
Adjust
in
accordance
with
TRAVEL.
properly.
paragraph
6-16.
Incorrect
adjustment
of
travel
Adjust
in
accordance
with
stop
bolts.
paragraph
6-16.
6-4.
CONTROL
STICK
AND
TORQUE
TUBE
ASSEM-
not
to
drop
bushing
(9).
SLY.
6.
Reverse
the
preceding
steps
for
reinstalla-
tion.
Rig
elevator
control
system
in
accordance
with
6-5.
DESCRIPTION.
The
control
stick
serves
a
paragraph
6-16,
safety
turnbuckles
and
reinstall
all
dual
purpose.
When
moved
fore-and-aft,
the
stick
items
removed
for
access.
pivots
in
a
bracket
at
the
aft
end
of
the
torque
tube
b.
TORQUE
TUBE
ASSEMBLY.
assembly
providing
elevator
control.
When
moved
1.
Complete
steps
1,
2
and
3
of
subparagraph
laterally,
the
stick
rotates
the
torque
tube
assembly
"a.
"
providing
aileron
control.
The
standard
stick
con-
2.
(See
figure
8-1.)
Remove
pully
(19)
figuration
is
shown
in
figure
6-2
(sheet
1).
The
and
pull
cable
(18)
free
of
torque
tube
(14).
electric
stick
configuration
is
shown
in
figure
6-2
3.
(See
figure
6-1.)
Remove
safety
wire
(sheet
2).
and
relieve
cable
tension
at
turnbuckles
(3.
5
and
8).
4.
On
aircraft
equipped
with
electrical
control
6-6.
REMOVAL
AND
INSTALLATION.
stick,
disconnect
control
stick
cable
from
socket
(23)
a.
CONTROL
STICK.
located
at
aft
end
of
LH
kick
plate.
(Refer
to
figure
1.
Remove
fuselage
access
panels
below
left
6-2.)
and
right
doors.
5.
(See
figure
6-2.)
Remove
pivot
bolt
2.
Remove
safety
wire
and
relieve
elevator
securing
control
(5)
to
torque
tube
assembly
(18).
cable
tension
at
turnbuckles
(index
17
and
20,
figure
6.
Lift
control
stick
out
of
aircraft
using
care
8-1).
not
to
drop
bushing
(9).
3.
Disconnect
turnbuckle
(index
17,
figure
8-1)
7.
Reverse
the
preceding
steps
for
reinstalla-
at
lower
end
of
control
stick.
tion.
Rig
elevator
control
system
in
accordance
with
4.
(See
figure
6-2.)
Remove
pivot
bolt
se-
paragraph
6-16,
safety
turnbuckles
and
reinstall
curing
control
stick
(5)
to
torque
tube
assembly
(18).
items
removed
for
access.
5.
Lift
control
stick
out
of
aircraft
using
care
6-2