Cessna T188C - Page 82

MODEL
188
&
T188
SERIES
SERVICE
MANUAL
4-27.
INSTALLATION.
to
forward
bulkhead
of
tailcone.
a.
Jack
aircraft
in
accordance
with
procedures
out-
g.
Remove
jacks
and
hoist
supporting
aircraft.
lined
in
paragraph
2-4
and
figure
2-1.
h.
Connect:
1. Elevator
cables
and check rigging.
See Sec-
CAUTION tion 8.
2.
Rudder
cables
and
check
rigging.
See
sec-
Support
front end
of aircraft
wich
hoist hooked
tion
10.
into
engine
lifting eye.
Loss
of tailcone
weight
3.
Elevator
trim
tab cables
and
check rigging.
will
allow
nose to drop.
See
Section 9.
i.
Route
static
line
through
forward
bulkhead
and
b. On
serials
prior
to 188-0048,
position
tailcone
connect
at
tee in
tailcone.
in proper
location
to be
fastened
to welded
tubular
j.
Connect optional
quick-loading
system
main
structure.
Beginning
with
serial
188-0048,
align
tube
at aft
end.
tailcone
with
attaching
studs
in tubular
structure.
Be
k.
Route radio
antenna
lead
through
front
tailcone
sure
tube for quick-loader
system is
properly
install-
bulkhead,
attach to
antenna,
and install
clamps sup-
ed
and that
it passes
through
forward
bulkhead
seal
porting
lead.
without
damage
to either
tube or
bulkhead.
1.
Connect
flashing
beacon
and
tail light
wires
at
c. On
serials
prior
to
188-0048,
install
four
bolts
quick-disconnect
forward
of
front
tailcone
bulkhead,
attaching
tailcone
to tubular
structure.
Beginning
if
installed.
with
serial
188-0048,
install
castle
nuts and
cotter
m. Connect
deflector
cable, tighten
to
15-20
pound-
pins
on
attaching
studs.
If shims
are
used,
be
sure
inches
and
resafety.
they
are
in
proper
location
as identified
at
removal
n.
Install
access
door
on tailcone
forward
bulkhead
d. Install
four
bolts
attaching
canopy
brace
to tail-
o. Install
side
panels on
tubular
structure
and
tail-
cone.
cone.
e.
Using
existing
holes
as
guides,
either
in
canopy
p. Install
upper
engine
cowling.
or
tailcone,
drill
and
rivet
canopy
to
tailcone.
f.
Using
existing
holes
as guides,
either
in bottom
4-28.
REPAIR.
Repair
of the tailcone
should
be
skin or
tailcone
bulkhead,
drill
and
rivet bottom
skin
accomplished
in
accordance
with
applicable
instruc-
tions
in
Section
17.
4-10
Revision
1