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Cessna 177 SERIES Service Manual

Cessna 177 SERIES
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CARGO
TIEGh
CARGO
TIEN
LATCH
ASSEMBLY
CARGO
TIE-DOWN
DOWN
RING
\^^
\
Y^yLUG
SLIDE
ASSEMBLY
owby iB
<OLT
SEAT
RAIL
BEGINNING WITH
THRU
17701633
17701634
Figure
3-8.
Cargo
Tie-Downs
2
3
2
3
-. 1
THRU
17701530
BEGINNING
WITH
17701531
- -
\
. -
Detail
A
.....:. .. "
A
1.
Mirror
Assembly
4.
Knurled
Nut
2.
Bracket
5.
Cowl Deck
3.
Washer
Figure
3-9.
Rear
View
Mirror
Installation
ener
compound
applied
to
inner
surfaces
of
skin
in
d.
Remove
molding
from
fixed
windows
and
trim
most
areas
of
cabin
and
baggage
compartment.
All
strip
above
windshield.
soundproofing
material
should
be
replaced
in
its
e.
Remove
screws
from
the
aft
headliner
section
original
position
any
time
it
is
removed.
A
sound-
and
carefully
remove
section.
proofing
panel
is
placed
in
gap
between
wing
and
f.
Remove
screws
from
the
forward
headliner
sec-
fuselage
and
held
in
place
by
wing
root
fairings.
tion
and
carefully
remove
section.
g.
Remove
spun
glass
soundproofing
panels.
3-44.
CABIN
HEADLINER.
(Refer
to
figure
3-7.)
3-45.
DESCRIPTION.
The
cabin
headliner
is
con-
NOTE
structed
of
closed-cell
thermoformed
plastic,
in-
stalled
in two
sections.
One
section
extends
from
The
lightweight
soundproofing
panels
are
aft
of
the
main
spar
forward
and
the
other
section
held
in
place
with
industrial
rubber
cement.
from
the
main
spar
aft.
The
headliner
is
held
in
place
with
sheet
metal
screws.
h.
Reverse
preceding
steps
for
installation.
Be-
fore
installation,
check
all items
concealed
by
head-
3-46.
REMOVAL
AND
INSTALLATION.
liner
for
security.
Use
wide
cloth
tape
to
secure
a.
Remove
forward
air
inlet
controls
and
overhead
loose
wires
to
fuselage
and to
seal
openings
in
wing
console.
roots.
Straighten
any
supports
bent
during
removal
b.
Remove
rear
air
inlet
controls
and
escutcheons.
of
headliner.
c.
Remove
access
cover
aft
of
main
spar.
Change
4
3-19

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Cessna 177 SERIES Specifications

General IconGeneral
ManufacturerCessna
Engine TypePiston
Wingspan35 ft 6 in (10.82 m)
Seating Capacity4
Number Built4, 295
EngineLycoming O-360
Horsepower180 hp
Maximum Takeoff Weight2, 500 lb (1, 134 kg)

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