Cessna T188C - Page 73

MODEL
188 & T188
SERIES SERVICE
MANUAL
SECTION 4
WINGS AND EMPENNAGE
Page No.
TABLE OF CONTENTS Aerofiche/Manual
WINGS AND EMPENNAGE. ...... 1D1/4-1 Removal and Installation . . . 1D7/4-7
Wings
..............
1D1/4-1
Repair
...........
1D7/4-7
Description
.........
1D1/4-1
Horizontal
Stabilizer
.......
1D7/4-7
Removal . ..........
D1/4-1
Description .........
1D7/4-7
Repair
...........
1D3/4-3
Removal and
Installation
.. . 1D7/4-7
Installation
.........
1D3/4-3
Repair
...........
1D7/4-7
Adjustment
(Correcting
Wing-
Stabilizer
Abrasion Boots
.....
D7/4-7
Heavy Condition)
......
1D3/4-3
Description
.........
1D9/4-9
Wing Strut
...........
1D3/4-3
Removal
..........
1D9/4-9
Description
.........
1D3/4-3
Installation ..... ..
. 1D9/4-9
Removal
and Installation
...
1D3/4-3
Tailcone
............
ID9/4-9
Repair
....
......
D3/4-3
Description
.........
1D9/4-9
Stub Wing
Catwalk
. .
.... 1D7/4-7
Removal
..........
1D9/4-9
Fin
...............
1D7/4-7
Installation
.....
D10/4-10
Description.
.......
lD7/4-7
Repair
....
D10/4-10
4-1. WINGS
AND EMPENNAGE.
c. On models
with wing fuel cells, drain
fuel in
wing
being
removed.
Drain
reservoir
tank
and
4-2. WINGS.
(See figure 4-1.)
enough
fuel from
cell in opposite
wing to lower
fuel
level
below crossover
vent line.
Observe precau-
4-3. DESCRIPTION.
Each all-metal wing panel
is tions outlined
in Section 12.
a semicantilever, semimonocoque
type, with two
d. Disconnect electrical
wires at wing root.
main spars
and suitable
ribs for attachment
of the
e. Disconnect
fuel lines
and crossover
vent line,
skin. Skin panels are
riveted to the ribs, spars
and if installed, at
wing root and cap lines.
stringers to complete the structure.
Two versions
f. Disconnect pitot line (left wing
only) at wing root.
of
the Agwagon-Series
wing are
available. On car-
g.
Disconnect flap
and aileron cables
at the turn-
buretor
equipped aircraft,
and on standard
fuel in-
buckles
in the fuselage
and remove cable
guards and
jected aircraft with
fuel tanks installed in the forward
fairleads as necessary
to pull cables out to the wing
fuselage area, no fuel provisions are made in the root.
wings.
Optional
rubberized fuel
cells are available
h.
Thru aircraft
serial 18800832,
loosen strut
for installation
in the wings of fuel injected
aircraft. fairings and
slide fairings along strut for access
to
An
all-metal aileron, flap and a detachable
wing tip strut
fittings. Beginning with aircraft
serial 188-
are mounted on
each wing assembly.
Beginning
with
00833, remove
strut fairing
for access to strut
aircraft
serial 18800573,
a stall fence and an
aileron fitting on
the wing.
gap seal are installed
on each
wing assembly.
Thru i.
Support wing,
remove jury strut,
and disconnect
aircraft
serial 18800832
optional
landing and taxi
wing
strut at the
fuselage fitting
and wing fitting.
lights, and also,
colored navigation
lights are
avail-
j. Mark position
of wing attachment
eccentric
able for installation
on each wing assembly. Begin-
bushings; these bushings
are used to rig out "wing-
ning with
aircraft serial 18800833
the landing
lights heaviness."
are installed
on the lower nose
cap, and in
addition
to
the colored navigation light
a strobe light, wing tip
NOTE
turning light, and forward facing spray light may be
installed
on each wing assembly.
It is recommended to secure flap
in stream-
lined position with tape during wing removal,
4-4. REMOVAL.
Wing removal
is accomplished
to prevent
damage since
flap will swing
freely.
most easily if four men are available to handle the
wing. Otherwise, the
wing should be supported with
k. Remove nuts, washers,
bushings and bolts
a sling
or maintenance
stand when
fastenings
are
attaching wing
spars to stub
wing.
loosened.
NOTE
NOTE
It may be necessary
to use
a long drift
punch
Disconnect any agricultural
equipment as
to drive out wing attaching
bolts, or to rock
necessary
to remove
wings.
wing slightly
while pulling
bolts.
a. Remove wing
gap fairings.
1. Remove
wing and lay
on padded stand.
b. Remove
all wing
inspection
plates.
4-1