Cessna 182 1978 - Inspection Guidelines

MODEL 182 & T182 SERIES SERVICE MANUAL
D Inspection Guidelines.
(1) The Inspection Charts are to be used as a recommended inspection outline. Detailed informa-
tion of systems and components in the airplane will be found in various chapters of this Main-
tenance Manual and the pertinent
vendor publications. It is recommended
that reference be
made to the applicable portion
of this manual for service instructions,
installation instructions,
and to the vendor's
data or publications specifications for torque
values, clearances, settings.
tolerances, and other requirements.
(2) For the purpose
of this inspection, the term on condition
is defined as follows: The neces-
sary inspections and/or checks to determine that a malfunction or failure will not occur prior to
the next scheduled inspection.
(3) MOVABLE PARTS; Inspect for lubrication, servicing, security of attachment. binding, exces-
sive wear. safetying,
proper operation, proper adjustment, correct
travel, cracked fittings, se-
curity
of hinges, defective bearngs, cleanliness,
corrosion, deformation, sealing, and
tension.
(4) FLUID LINES AND HOSES: Inspect
for leaks, cracks, bulging, collapsed,
twisted, dents,
kinks, chafing, proper radius, security, discoloration, bleaching, detenoration, and proper rout-
ing; rubber hoses for stiffness and metal lines for corrosion.
(5)
METAL PARTS: Inspect for security of attachment,
cracks. metal distortion, broken
spotwelds,
condition
of paint (especially
chips at seams and
around fasteners
for onset of corrosion)
and
any other apparent damage.
(6) WIRING:
Inspect for security,
chafing, burning, arcing,
defective insulation,
loose or broken
terminals, heat deterioration, and corroded terminals.
(7) STRUCTURAL FASTENERS:
Inspect for correct torque in accordance
with applicable torque
values. Refer
to Bolt Torque Data
during installation
or when visual inspection
indicates the
need for a torque check.
NOTE
Torque values
listed are not to be used for checking
tightness of installed parts
during service.
(8) FILTERS,
SCREENS. AND FLUIDS:
Inspect for cleanliness
and the need
for replacement
at
specified intervals.
(9)
System check (operation
or function) requiring
electrical power
must be performed
using 28.5
±0.25 volts bus voltage.
This will ensure all components are
operating at their designed re-
quirements.
(a)
Airplane
file.
1 Miscellaneous
data. information. and licenses
are a part of the airplane file. Check
that the following
documents
are up-to-date and
in accordance
with current Federal
Aviation
Regulations. Most
of the items listed
are required
by the Federal
Aviation
Regulations. Since
the regulations
of other nations
may require other
documents
and data. owners
of exported
airplanes should
check with their
own aviation offi-
cials
to determine their
individual requirements.
a. To be displayed
in the airplane at
all times:
1) Standard
Airworthiness
Certificate
(FAA Form
8100-2).
2) Aircraft
Registration
Certificate
(FAA
Form 8050-3).
3) Aircraft Radio Station
License (Federal Communication
Commission Form
556 if transmitter is installed).
4) Radio Telephone
Station License (Federal Communication
Commission
Form 409 if Flitefone Radio Telephone is installed).
b
To be carried in
the airplane at all times:
1) Weight and Balance
Data Sheets and associated
papers (all copies of the
Repair and Alteration
Form. FAA Form
337. are applicable).
2) Equipment List
3) Pilot's Operating
Handbook and FAA-Approved
Airplane Flight Manual.
To be made available upon request:
1)
Airframe Engine. Propeller. and
Avionics Maintenance Records.
2 .26 Revision 2