Cessna 182 1978 - Page 61

MODEL
182
& T182
SERIES
SERVICE
MANUAL
SPECIAL
EACH
EACH
EACH
INSPECTIONS
2-50
INSPECTION
TIME
LIMITS.
(MODEL
182
50
100
200
&
T182
AIRPLANES.)
HOURS
HOURS
HOURS
HOURS
YEARS
D
4
Wheels.
Brake
Discs,
and
Linings
- Inspect
for
wear.
cracks,
warps,
dents,
or other
damage.
Check
wheel
through-bolts
and
nuts
for
looseness.
D
5 Tires
- Check
tread
wear
and
general
condition.
Check
for
proper
inflation.
D
6 Wheel
Fairings,
Strut
Fairings,
and
Cuffs
- Check
for
A
cracks,
dents,
and
condition
of
paint.
D
7 Main
Landing
Gear
Attachment
Structure
- Check
for
damage,
cracks,
loose
rivets,
bolts
and
nuts
and
security
of
attachment.
D
8
Nose
Gear
Steering
Mechanism
- Check
for
wear,
security,
and
proper
rigging.
D
9 Nose
Gear
-
Inspect
torque
links,
steering
rods,
and
boots
for
condition
and
security
of attachment.
Check
strut
for
evidence
of
leakage
and
proper
extension.
Check
strut
barrel
for
corrosion,
piing,
and
cleanliness.
Check
shimmy
damper
and/or
bungees
for
operation,
leakage,
and
attach
points
for
wear
and
security.
D
10
Nose
Gear
Fork
- Inspect
for
cracks,
general
condition.,
and
security
of
attachment.
D
11
Wheel
Bearings
- Clean,
inspect
and
lube.
B
D
12
Nose
Gear
Attachment
Structure
- Inspect
for
cracks,
corrosion,
or
other
damage
and
security
of
attachment.
E
Aileron
Control
System
(Section
6)
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
it
stops
are
damaged.
Check
fairleads
and
rub
strips
for
condition.
E
4
Autopilot
Rigging
- Check
per
Avionics
Installation
Manual.
C
E
5
Aileron
Controls
- Check
freedom
of
movement
and
proper
operation
through
full
travel
with
and
without
flaps
extended
F
Wing
Flap
Control
System
(Section
7)
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
safely
Check
travel
if cable
tension
requires
adjustment.
2
30
Revision
2