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Cessna 182 1978 - Page 81

Cessna 182 1978
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MODEL
182
&
T182
SERIES
SERVICE
MANUAL
CESSNA
PROGRESSIVE
CARE
MODEL
182
&
T182
OPERATION
NO.
1
INSPECTION
SPECIAL
INSPECTION
AND
YEARLY
ITEMS
HOURS
YEARS
COMPLETED
BY
Please
review
each
of
these
items
for
required
compliance
B
I
Upholstery.
Headliner.
Trim,
and
Carpeting
-
Check
condition
EACH
EACH
and
clean
as
required.
400
1
D
3
Brake
Lines. Wheel
Cylinders.
Hoses,
Clamps,
and
Fittings
-
EACH
EACH
Check
for
leaks, condition,
and
security
and hoses
for
bulges
400
1
and
deterioration
Check
brake
lines
and
hoses
for
proper
routing and
support
D
6
Wheel
Fairings,
Strut
Fairings,
and
Cuffs
-
Check
for
cracks.
A
dents,
and
condition
of
paint.
D
11
Wheel
Bearings
-
Clean,
inspect
and
lube.
B
E
4
Autopilot
Rigging
-
Check
per
Avionics
Installation
Manual.
C
H
5
Elevator
Trim
Tab
Actuator
-
Clean,
lubricate..
D
J
3
Engine.
Propeller
Controls,
and
Linkage
-
Check
general
E
condition, freedom
of
movement
through
full
range. Check
for
proper
travel,
security
of attachment,
and
for
evidence
of
wear.
Check
friction
locks
for
proper
operation.
J
9
Induction
Air
Filter
-
Remove
and
clean.
Inspect
for
damage.
F
and
service per
paragraph
2-24.
J
12
Alternator
-
Check brushes,
leads,
commutator
or
slip
ring
for
G
wear.
J
14
Starter.
Starter Solenoid,
and
Electrical
Connections
-
Check
for
H
condition
of
starter
brushes,
brush
leads, and
commutator.
J
20
Magnetos
-
Inspection
lubrication
and
overhaul
procedures.
I
J
21
Magnetos
-
Check
external
condition,
security,
and
electrical
J
leads for
condition.
Check
timing
to
engine
and
internal
timing
if
engine
timing
requires
adjustment.
J
22
Magnetos
-
Timimg
Procedures and
intervals.
K
J
28 Hoses,
Metal
Lines,
and
Fittings
-
Inspect
for
signs
of
oil
and
L
fuel
leaks.
Check
for abrasions,
chafing.
security,
proper
routing
and
support
and
for
evidence
of
deterioration.
J
31
Turbocharger
(if
applicable)
-
M
a.
Inspect
turbocharger
mounting
bracket,
ducting.
linkage, and
attaching
parts
for
general
condition.
linkage
or
damage,
and
security
of
attachment.
b.
Check
waste
gate,
actuator,
controller,
oil
and.
vent
lines,
overboost
relief
valve,
and
compressor housing
for
leakage.
apparent
damage,
security
of
attachment.
and
evidence
of
wear.
Check
waste
gate
return
spring
for
condition
and
security
J
34
Engine
Oil
Change
-
N
Short Oil
Filter (approximately 4.8
inches)
a.
Replace
Filter.
b
Add
recommended
grade
aviation
oil
to
replace
oil
lost
in
existing
filter
Without
Oil
Filter
-
Drain
oil
sump
and
oil
cooler,
inspect
and
clean
screens.
and
refill with
recommended
grade
aviation
oil
J
35
Long
Oil
Filter
(approximately
5.8
inches)
-
Drain
oil
sump
and
N
oil
cooler,
replace
filter
element,
refill
with
recommended
grade
aviation
oil
K
1
Integral
Fuel
Tanks
-
Check
for
evidence
of
leakage
and
O
condition
of fuel
caps.
adapters.
and
placards
K
2
Fuel
Bladders
-
Check
for
leaks
and
security,
condition
of
fuel
O
caps.
adapters,
and
placards
2-48
Revision
3

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