Cessna 182 1978 - Tie-Down; Flyable Storage; Leveling; Hoisting

MODEL
182 & T182
SERIES
SERVICE
MANUAL
2-3.
HOISTING. The aircraft
may be lifted with
a 2-9. FLYABLE
STORAGE. (Airplanes
with a
hoist of two-ton
capacity by using hoisting
rings,
Lycoming engine). Flyable
storage is defined
which are
optional equipment,
or by means of suit-
as a maxmum of
30 days non-operational
storage
able slings.
The front sling should
be hooked to
and/or the first 25
hours of intermittent engine
each upper engine mount at the firewall, and the aft operation.
sling should
be positioned around
the fuselage at the
first bulkhead forward
of the leading edge of the
NOTE
stabilizer.
If the
optional
hoisting
rings
are
used,
a minimum
cable length
of 60 inches
for each
cable
Lycoming
0-540
Series
aircraft
engines
is required
to prevent bending
of the eyebolt-type
used in the
T182 series aircraft
are de-
hoisting rings.
If desired,
a spreader
jig may be
livered
from Cessna
with MIL-L-6082
fabricated
to apply vertical
force
to the eyebolts.
Aviation
Grade
Mineral
Oil. This
engine
oil should
be used to replenish
the oil
2-4.
JACKING.
See figure
2-2
for jacking
proced-
supply
during
the first
25 hours
of engine
ures.
operation at the
first 25 hour
oil change
and until a total
of 50 hours have
accumu-
2-5.
LEVELING.
Corresponding
points
on both
lated
or oil
consumption
has
stabilized.
upper
door sills
may be
used to level
the aircraft
Then
use Ashless
Dispersant
Oil conform-
laterally.
Reference
point
for leveling
the aircraft
ing to MIL-L-22851
in accordance
with the
longitudinally
is the top
of the
tailcone
between
the
oil
chart in
figure 2-4.
rear window
and the vertical
fin. Beginning with
Serials
18266076 &
ON, F18200065
& ON, and T182-
During
the 30 day non-operational
storage
or the first
67717
ON,
leveling
points
have
been
added
to
the left
25 hours
of
intermittent
engine
operation,
every
sev-
side
of tailcone
at
Sta.
139.65
and
171. 65.
Remove
enth
day the
propeller
shall
be rotated
by
hand
without
NAS221-7 screws
and install suitable
studs to
support running
the engine.
After rotating
the engine five
rev-
a level.
olutions, stop
the propeller
45 to 90 from
the posi-
tion it was in. If the aircraft is stored outside, tie-
2-6. WEIGHING
AIRCRAFT.
Refer to Pilot's
down
in accordance
with paragraph
2-8.
In addition,
Operating
Handbook.
the
pitot tube,
static
air vents,
air vents,
openings
in the engine cowling, and other similar openings
2-7.
PARKING.
Parking
precautions
depend
prin-
shall
have
protective
covers
installed
to prevent
entry
cipally
on local conditions.
As a
general precaution,
of foreign
material.
If at the end of
thirty (30) days
set parking
brake or chock
the wheels and install
the
aircraft will not
be removed from
storage, the
engine
controls lock.
In sever weather
conditions and
high shall
be started and
run. The preferred
method would
wind, tie
down
the aircraft
as outlined
in paragraph
be to
fly the
aircraft
for thirty
(30)
minutes,
and up
to
2-8
i a
hangar
is
not
available.
but
not
exceeding
normal
oil
and
cylinder
temperatures.
2-8.
TIE-DOWN.
When
mooring
the aircraft
in the
open.
head into the
wind if possible.
Secure
control
surfaces with the internal
control lock and set
brakes. Excessive
ground operation
shall be avoided.
Do not set parking brakes when they are NOTES
overheated
or during
cold weather
when
accumulated
moisture may freeze
them.
Preservation
date
should
be
written
on pro-
a. Tie
ropes, cables,
or chains to the
wing tie-
peller
tag.
down fittings
located
at the upper
end of
each wing
strut. Secure the opposite ends
of ropes, cables, Maintain complete
and accurate engine pre-
or chains
b. Secure a
tie-down rope (no chains or cables) to
vationof the engine cylinders can be docu-
upper strut
of the nose gear,
and secure opposite
end
of rope to a ground
anchor.necessary.
c. Secure the middle
of a rope to the
tail tie-down
ring.
Pull each
end of rope away
at a 45 degreeThe
airplane is
delivered from
Cessna with
a
angle
and secure to
ground anchors
at each side of
Corrosion
Preventive
Aircraft Engine
Oil mix
tail.
ture. This engine
oil is a blend of aviation
d. Secure
control lock
on pilot control
column.
If
grade
straight
mineral oil
and corrosion
pre-
control lock
is not available,
tie pilot control
wheel
ventive compound.
This
oil should be used
for
back with front
seat belt.
the first
25 hours
of engine
operation.
In the
e. These aircraft are equipped with a spring-loaded
event it necessary
to add oil during the
steering bungee
which affords
protection
against nor-
aviation
grade straight
mineral oil of
the cor-
mal wind gusts.
However, if extremely
high wind
gusts are
anticipated, additional external
locks may be
installed.
Flyable
storage
is
defined
as a maximum
of 30
days
2-4
Revision
1