Cessna 182 1978 - Page 87

MODEL 182 & T182 SERIES SERVICE MANUAL
CESSNA PROGRESSIVE CARE
MODEL
182
& T182
OPERATION
NO.
2
INSPECTION
SPECIAL INSPECTION AND YEARLY ITEMS HOURS YEARS COMPLETED BY
Please review
each of these items for
required compliance
B 11 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.
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, leakage 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.
2-54
Revision
3