Cessna T182 Series User Manual

MODEL
182
& T182 SERIES
SERVICE
MANUAL
WING LOOKING
DOWN
AT TOP OF LOWER
(10
REOD)
LOWER WING SKIN (REF)
5.062
DIA-
S-225-4F
COVER
\,A | 4-
~ MS20426AD3
RIVETS
NOTE
PARTS
ARE AVAILABLE
FROM
THE
CESSNA
SUPPLY
DIVISION.
S-1022Z-8-6
SCREWS
PRECAUTIONS
1. Add
the minimum number of
access holes necessary.
2. Any circular or
rectangular access hole
which is used with
approved optional equipment
installa-
tions
may be
added in lieu
of the access
hole illustrated.
3. Use
landing light installations
instead of adding
access holes where
possible. Do not add
access
holes at outboard
end
of wing; remove
wing tip
instead.
4.
Do not add an
access hole in the
same bay where
one is already
located.
5. Locate new access holes
near the center of a bay
(spanwise).
6. Locate
new access holes forward of the front
spars as close to the front spar as
practicable.
7. Locate new
access holes aft of
the front spar between
the first and second
stringers aft of the
spar. When
installing
the doubler,
rotate
it so the
two straight
edges
are closest
to the stringers.
8. Alternate
bays, with new
access holes
staggered
forward and
aft of the front
spar, are pre-
ferable.
9. A maximum
of five new
access holes
in each wing
is permissible;
if more are
required, contact
the
Cessna
Service
Department.
10. When
a complete
leading edge
skin is being
replaced, the
wing should
be supported
in such a
manner
so that
wing alignment
is maintained.
a. Establish
exact
loca'ton
for inspection
cover
and inscribe
centerlines.
b. Determine
position
of doubler
on wing skin
and center over
centerlines.
Mark the
ten rivet
hole
locations
and
drill to
size shown.
c. Cutout
access hole,
using
dimension
shown.
d.
Flex doubler
and
insert
through
access
hole,
and
rivet in
place.
e.
Position
cover
and secure,
using
screws
as
shown.
Figure
18-13.
Access
Hole
Installation
18-34

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)