Cessna 182 1978 - Page 38

MODEL
182
& T182
SERIES
SERVICE
MANUAL
g.
Install
spark
plugs
or solid
plugs
into
the
lower
a.
Drain
engine
oil
and
refill
with
MIL-C-6529
Type
spark
plug
holes
and
install
dehydrator
plugs
in
the
II.
The
aircraft
should
be
flown
for
thirty
(30)
min-
upper
spark
plug
holes.
Be sure
that
dehydrator
utes,
reaching,
but
not
exceeding
normal
oil and
cyl-
plugs
are
blue
in
color
when
installed.
inder
temperatures.
Allow
engine
to
cool
to ambient
h.
Cover
spark
plug
lead
terminals
with
shipping
temperature.
plugs
(AN4060-1).
or
other
suitable
covers.
b.
Remove
top
spark
plug
and
spray
preservative
i.
With
throttle
in full
open
position,
place
a
bag
oil
(Lubrication
Oil
- Contact
and
Volatile
Corrosion
-
of
desiccant
in the
induction
air
intake
and
seal
Inhibited,
MIL-L-46002.
Grade
1)
at room
tempera-
opening
with
moisture
resistant
paper
and
tape.
ture.
through
upper
spark
plug
hole
of each
cylinder
j.
Place
a bag
of
desiccant
in
the exhaust
tailpipe
with
piston
in
approximately
bottom
dead
center
posi-
and
seal
openings
with
moisture
resistant
tape.
tion.
Rotate
crankshaft
as
each
pair
of
opposite
cylin-
k.
Seal
cold
air
inlet
to
the
heater
muff
with
mois-
ders
is sprayed.
Stop
crankshaft
with
no
piston
at top
ture
resistant
tape.
dead
center.
A
pressure
pot
or pump-up
type
garden
1.
Seal
engine
breather
tube
by inserting
a
protex
pressure
sprayer
may
be used.
The spray
head
should
plug
in the
breather
hose
and clamping
in place.
have
ports
around
circumference
to allow
complete
m.
Seal
all
other
engine
openings
exposed
to
at-
coverage
of cylinder
walls.
mosphere
using
suitable
plugs
or
non-hygrosoopic
tape.
NOTE
NOTE
NOTE
The
preservative
oil
must
be
MIL-L-46002.
Attach
a red streamer
to each
location
where
grade
1, at room
temperature.
Two
preserva-
plugs
or
tapes
are installed.
Either
attach
tive
oils recommended
for use
in
Teledyne
red
streamers
outside
th sealed
area
with
Continental
engines
for temporary
and
tape
or
to the
inside
of the
sealed
area
with
safety
wire to prevent
wicking
of moisture
vania
Refining
Company,
Butler.
PA).
n.
Drain corrosion-prventive
mixture
from
en-
gine
sump
and
reinstall
drain
plug
or
close
drain
To.
Respray
each
cylinder
without
rotating
crank.
move
nozzle
or spray
gun
from top
to bottom
of
cyl-
inder.
The
corrosion-preventive
mixture
is harm-
NOTE
ful to paint and
should be wiped from
Type
II may be
painted
surfaces
immediately.
thoroughly
mixin
one part
compound
MIL-
C-6529
Type
I
(Esso
RustBan
628, Cos-
o. Attach
a warning
placard on the
throttle control
moline No. 1223
or equivalent)
with three
knob
to the
effect that
the engine
contains
no lubricat-
parts
new lubricating
oil of the
grade recom-
ing oil.
Placard
the propeller
to the
effect that
it
mended
for service
(all at room
temperature).
should
not be moved while
the engine is in storage.
Single
grade oil is recommended.
p.
Prepare
airframe
for storage
as outlined
in
paragraph
2-11 thru step "f".
d. Apply preservative
to engine
interior by
spray-
ing
MIL-L-46002,
Grade
1 oil
(approximately
two
NOTE
ounces)
through oil filler tube.
e.
Install
dehydrator
plugs
MS27215-1
or-2,
in
As an
alternate
method
of indefinite
storage,
each
of the
top spark
plug holes,
making
sure
that
the aircraft
may be serviced
in accordance
each plug is
blue in color
when installed.
Protect
and
with paragraph
2-11,
providing
the aircraft
support
spark plug
leads with
AN-4060 protectors.
is run
up at maximum
intervals
of
90 days
f. DO
NOT rotate
propeller
after completing
and
then reserviced
per paragraph
2-11.
step
e".
g.
If engine
is
equipped
with
a pressure
type
car-
2-14A.
INDEFINITE
STORAGE.
(Airplanes
with
a
buretor,
preserve
this
component
by
the
following
Continental
engine.)
Indefinite
storage
is
defined
as
method.
Drain
carburetor
by
removing
the
drain
and
aircraft
in
a non-operational
status
for
an
indef-
vapor
vent
plugs
from
regulator
and
fuel
control
inite
period
of
time.
Engines
treated
in accordance
unit.
With
mixture
control
in
"Rich"
position,
inject
with
the
following
may
be considered
protected
lubricating
oil,
grade
1010.
into
fuel
inlet
at a
pres-
against
normal
atmosphere
corrosion,
provided
pro-
sure
not
to
exceed
10 psi
until
oil flows
from
vapor
cedures
outlined
in paragraph
2-15
are performed
at
vent
opening.
Allow
excess
oil
to
drain,
plug
inlet
and
intervals
specified.
tighten
and
safety
the
drain
and
vapor
vent
plugs.
Wire
throttle
in
open
position,
place
bags
of
desiccant
in
the
intake
and
seal
opening
with
moisture
resis-
tant
paper
and
tape
or
a cover
plate.
Revision
1
2-7