Cessna T182 Series User Manual

MODEL
182 &
T182 SERIES
SERVICE
MANUAL
CESSNA PROGRESSIVE
CARE
MODEL 182 & T182
OPERATION
NO.
1
Special
Inspections
Legends:
A. If the
airplane is flown
from surfaces
with mud,
snow, or ice, the
main gear
speed fairings
should be
checked that
there is no accumulation
which could
prevent normal
wheel rotation.
B. First 100
hours and each
500 hours thereafter.
More
often if operated
under prevailing
wet or dusty
conditions.
C. Each 600 hours
or 1 year, whichever
comes first.
D. Lubrication
of the actuator
is required
each 1000
hours or 3 years,
whichever
comes first. See
fig-
ure 2-5 for
grease specification.
E. Lubricate
each
100 hours
(except in
extreme
dusty conditions).
These
controls
are not
repairable
and should
be replaced
every
1500 hours
or whenever
maximum
linear
movement
exceeds
0.050
inch.
F. Clean filter
per Paragraph
2-24. Replace paper
filter at least
each 500 hours.
G. Inspect
each 500 hours.
H. For Prestolite starter
only, inspect the commutator and brushes
each 1500 hours.
I. After 500
hours of operation,
perform
the following
checks:
1. Inspect
contact
points
for condition
and adjust
or replace
as required.
2. Inspect
carbon brush,
high-tension
lead, and distributor
block
for condition
and clean or replace
as required.
3. Inspect
impulse coupling and
pawls for condition
and replace as required.
Use light pressure
only, do not force
pin (or drill bit) when
checking pawls.
4. Inspect
bearings
and lubricate,
replace bearings,
if required.
5. Lubricate contact point cam.
6. Completely
overhaul,
or replace existing
magneto
with a new
or rebuilt exchange
magneto,
at
every engine overhaul.
7. Overhaul
and Maintenance
Manual,
Publication No.
1037C1-13,
covering Model
4200/6200
se-
ries
magnetos,
is available
from
Cessna
Supply
Division.
J. Compliance with Bendix Service Bulletin 599D or latest revision is required.
K. At
the first 25
hours, first
50 hours,
first 100
hours, and
thereafter
at each
100 hours,
the contact
breaker
point compartment
and magneto-to-engine
timing should
be inspected and
checked. If
magneto-to-engine
timing
is correct within
plus zero
degrees to minus
two degrees,
internal
timing
need
not be checked.
If timing is
out of tolerance,
remove magneto
and set
internal timing,
then in-
stall and time
to the engine.
Refer to Section
11 or
11A and the magneto
manufacturers
service
instructions for magneto
timing procedures.
L. Replace
engine compartment
rubber
hoses (Cessna
installed
only) every
five years or
at engine
overhaul,
whichever occurs
first. This does
not include drain hoses.
Hoses which are
beyond these
limits and
are in a serviceable
condition,
must be placed
on order
immediately and
then be replaced
within
120 days after
receiving
the new hose(s)
from Cessna.
Replace
drain hoses on
condition.
Engine
flexible hoses
(Continental
or Lycoming
installed) (Refer
to Continental
or Lycoming
Main-
tenance Manual
and Continental
or Lycoming
Engine Service
Bulletins).
M. Replace
turbocharger
oil line check
valves every
1000 hours.
(Refer to Cessna
Single Engine
Ser-
vice Bulletin SEB92-7.)
N. Continental
engine (182): Add straight
grade mineral oil
if required. After 25
hours, drain and refill
with ashless
dispersant oil.
Lycoming engine (T182):
Add straight grade
mineral oil if required.
After
25 hours, drain
and refill with
straight grade
mineral oil
until a total of
50 hours have
accumulated
or
oil consumption
stabilizes, then
change to ashless
dispersant oil. Continental
and Lycoming
en-
gines:
After initial break-in
(25 or 50 hours).
If NOT equipped with
an external filter,
change oil and
clean screens
each 50 hours. If equipped
with SMALL
external filter. change
filter each 50 hours
and oil
each 100 hours. If equipped
with LARGE
external filter, change
oil and filter each
100 hours.
In all
cases, change oil
at least each 6
months regardless
of accumulated
hours.
O. Each 1000 hours.
P. If
leakage
is evident,
refer
to McCauley
Service
Manual.
Q. Replace
every 500
hours.
R.
Replace
filter
each
100
hours
S.
Check
electrolyte
level
and
clean
battery
box each
100 hours
or
90
days.
2-50 Revision 3

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)