Cessna T182 Series User Manual

MODEL
182
& T182
SERIES
SERVICE
MANUAL
19-7.
PREPRIMING.
19-8.
PRIMING.
a.
Apply
primer
in
one
wet
even
coat.
Dry
film
thickness
to
be
.
0003
to
.
0005
inches.
Do
not
top-
NOTE
coat until
sufficiently
cured. When
scratching
with
firm pressure
of the
fingernail
does
not penetrate
Enflex
III is standard on serials
18265781 thru
the coating, the primer
is cured. Primer
should be
18265784, 18265786 thru 18265806, 18265808, topcoated within four hours after application.
18265809,
18265815,
and
18265817.
a.
Above
serialized
aircraft
have
Enmar
Wash
19-9.
PREPAINTING.
primer
EX-ER-7,
Enflex
III
Enamel
for
overall
color
and
stripes,
which
has been
replaced
with
NOTE
484-684.
b.
Mix one
to
one, 484-684
primer
with
120-
Enflex
III is
standard
on
serials
18265781
thru
789Reducer
by volume.
Mix
in stainless
steel or
18265784,
18265786 thru
18265806,
18265808,
lined containers
only.
After
mixing,
allow pri-
18265809,
18265815
and 18265817.
mer
to
set
for
30
minutes
before
spraying.
Pot
life
of
the
mixed
primer
is
six
(6) hours.
All
mixed
material
should be
discarded
if not used
a.
On above
serialized
aircraft,
mix the
required
within
this time.
Pot
pressure
during
spraying
amount
of Enflex
III with
Enflex
III Adduct
in a
4 to 1
should
be approximately
10
± 1 psi.
Air pres-
ratio
by volume.
Mix
thoroughly,
and
allow
to stand
sure
should be
30 to 40
psi at the
gun.
Blow
for approximately
30 minutes
before
spraying.
loose
contanimant
of
the aircraft
with clean
dry
Enflex
III can
be thinned
with Jet
Glo thinner
86T-
air.
Check all
tapes
to make
sure it
adheres
10399 (110-655)
to obtain
spraying
viscosity,
which
properly.
Cover
the flap
tracks,
nose gear
should
be
checked
after
four
hours
and
adjusted
if
strut
tube,
wheels,
and shimmy
dampener
rod
necessary.
ends.
ABS
parts
and
other
preprimed
parts
do
not
receive
wash
primer.
NOTE
NOTE
Imron
is standard
on serials
18265785,
18265807,
Imron
is standard
on serials 18265785,
18265807,
18265810
thru 18265814,
18265816,
and 18265818.
.
18265810
thru
18265814,
18265816,
and
18265818.
c. Corrosion
proofed
and
standard
aircraft
will
b. On
standard
aircraft,
mix the
required
amount
of
receive
Sherwin
Williams Primer
P60G2,
DuPont
Imron
with Imron
192S Activator
in a
3 to 1 ratio
by
Imron
Enamel for
over all color,
and for stripes.
d.
Mix
1 part
P60G2
primer
with
1
1/2
parts
volume.
Mix
thoroughly,
and
begin
spraying
im-
R7K44
catalyst
reducer,
by
volume.
Mix
in
stain-
mediately,
because
there
is no
induction
time re-
less
steel
or lined
containers
only. Alter
mixing
quirement.
Imron
can
be thinned
to
spraying
less steel
or
allow
primer
to set
for
30 minutes
before
spraying.
viscosity
with
Y8485S
Imron
Reducer.
Viscosity
should
be checked
and
adjusted
after
four
hours
if
Pot
life
of
the
mixed
primer
is six
(6)
hours,
all
should
be
checked
and
adjusted
after
four
hours
if
mixed
materials
should
be discarded
if not
used
necessary.
within
that time
limit. Pot
pressure
during
spraying
painter
should
wear
an approved
respirator,
which
should be
should
be 40
to 50 psi
at the gun.
Blow
loose con-
taminant
off the airplane
with
clean,
dry air.
Chec
contain
some isocyanate,
which
may
cause ir-
all
tapes
to make
sure they
adhere
properly.
Cover
ritation
to
the respiratory
tract or
an allergic
reac-
the
flap
tracks,
nose
gear
strut
tube,
wheels,
and
ritation
to the
respiratory
tract
or
an allergic
reac-
the flap tracks,
nose
gear strut
tube,
wheels,
and
tion.
Individuals
may
become sensitized
to isocya-
shimmy
dampener
rod ends.
ABS parts
and other
preprimed
parts do
not receive
wash primer.
d. The
pot life of
the mixre
s approximately
6-8
should
be
40 to
50
psi.
AIRCRAFT
SHOULD BE
GROUNDED
PRIOR
e. Scuff
sand the primer
only
where runs
or dirt
TO PAINTING TO PREVENT
STATIC ELEC-
particles
are evident. Minor roughness
or grit may
TRICITY
BUILD-UP AND
DISCHARGE.
be removed by
rubbing the surface with
brown Kraft
19-5

Cessna T182 Series Specifications

General

Engine Type	Lycoming IO-540-AB1A5
Horsepower	230 hp
Seating Capacity	4
Service Ceiling	18, 100 feet
Takeoff Distance	1, 600 feet
Landing Distance	1, 350 ft
Type	Single-engine
Max Takeoff Weight	3, 100 lb
Wingspan	36 ft
Length	29 ft
Height	9 feet 3 inches
Fuel Capacity	92 US gal (348 L)