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Cessna 182 1978 - Page 90

Cessna 182 1978
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MODEL
182
&
T182
SERIES
SERVICE
MANUAL
CESSNA
PROGRESSIVE
CARE
MODEL
182
&
T182
OPERATION
NO.
3
Registration
No.
Airplane
Model
and
SN
Airplane
Time
INSPECTION
COMPLETED
BY
B
15
Seat
Tracks
and Stops
-
Inspect
seat
tracks
for
condition
and
security
of
installation.
Check
seat
track
stops
for
damage
and
correct
location.
Ensure
inspection
of
seat
rails
for
cracks
EACH
50
HOURS.
Refer
to
Section
3.
C
1
Wing
Surfaces
and
Tips
-
Inspect
for
skin
damage,
loose
rivets,
and
condition
of
paint.
C
2
Wing
Struts
and
Strut
Fairings
-
Check
for
dents,
cracks.
loose
screws
and
rivets,
and
condition
of
paint.
C 3
Wing
Spar
and
Wing
Strut
Fittings
-
Check
for
evidence
of
wear.
Check
attach
bolts
for indications
of looseness
and
retorque
as
required.
C 4
Wing
Structure
-
Inspect
spars.
ribs,
skins,
and
stringers
for
cracks,
wrinkles,
loose
rivets,
corrosion,
or
other damage.
C 5
Metal
Lines,
Hoses.
Clamps,
and
Fittings
-
Check
for
leaks.
condition.
and
security.
Check
for
proper
routing
and
support.
C
6
Wing
Access
Plates
-
Check for damage
and
security
of
installation.
C
7
Vertical
and
Horizontal
Stabilizers.
Tips
and
Tailcone
-
Inspect
externally
for
skin
damage
and
condition
of
paint
C
8
Vertical
and
Horizontal
Stabilizers
and
Tailcone Structure
-
Inspect
bulkheads.
spars,
ribs.
and
skins
for
cracks.
wrinkles,
loose
rivets,
corrosion,
or
other
damage.
Inspect
vertical
and
horizontal
stabilizer
attach
bolts
for
looseness.
Retorque
as
necessary.
Check security
of
inspection
covers,
fairings.
and
tips.
E
1
Ailerons
and
Hinges
-
Check
condition.
security
and
operation
E 2
Aileron
Structure.
Control
Rods.
Hinges.
Balance
Weights.
Bellcranks.
Linkage.
Bolts.
Pulleys,
and
Pulley
Brackets
-
Check
condition,
operation.
and
security
of
attachment
E
3
Ailerons
and Cables
-
Check
operation
and
security
of
stops.
Check
cables
for
tension.
routing,
fraying,
corrosion.
and
turnbuckle
safety
Check
travel
if
cable
tension
requires
adjustment
or
if
stops
are
damaged.
Check
fairleads
and
rub
strips
for
condition
E
5
Aileron
Controls
-
Check
freedom
of
movement
and
proper
operation
through
full
travel
with
and
without
flaps
extended.
F 1
Flaps
-
Check
tracks.
rollers,
and
control
rods
for
security
of
attachment
Check
operation
F
2
Flap
Actuator
Threads
-
Clean
and
lubricate.
Refer
to
paragraph
2-46
for
detailed
instructions.
F
3
Flap
Structure.
Linkage.
Bellcranks.
Pulleys,
and
Pulley
Brackets
-
Check
for
condition.
operation
and
security
F
4
Wing
Flap
Control
-
Check
operation
through
full
travel
and
observe
Flap
Position
indicator
for
proper
indication
F
5
Flaps
and
Cables
-
Check
cables
for
proper
tension.
routing,
fraying.
corrosion.
and
turnbuckle
safety
Check
travel
if
cable
tension
requires
adjustment
F 7
Flap
Motor.
Actuator.
and
Limit
Switches
(electric
flaps)
-
Check
wiring
and
terminals
for
condition
and
security.
Check
actuator
for
condition
and security
Revision
3
2-57

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