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Cessna T188C - Page 43

Cessna T188C
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MODEL
188
&
T188
SERIES
SERVICE
MANUAL
2. IF
THE
AIRPLANE
IS
FLOWN
MORE
THAN
200
HOURS
ANNUALLY.
Whether
flown
for
hire
or
not,
it
is
recommended
that
airplanes
operating
in
this
category
be
placed
on
the
CESSNA
PROGRESSIVE
CARE
PROGRAM
However, if
not
placed
on
Progressive
Care, the
inspection
requirements
for
airplanes
in
the
category
are
the
same
as
those
defined
under
paragraph
III
1.
(a)
and
(b).
Cessna
Progressive
Care
may
be
utilized
as
a
total
concept
program
which
ensures
that
the
inspection
intervals
in
the
inspection
charts
are
not
exceeded.
Manuals
and
forms
which
are
required
for
conducting
Progressive Care
in-
spections
are
available
from
the
Cessna
Service
Parts
Center.
IV
INSPECTION
GUIDE
LINES.
(a)
MOVABLE
PARTS
for:
lubrication,
servicing,
security
of
attachment,
binding,
excessive
wear,
safetying,
proper
operation,
proper
adjustment,
correct
travel,
cracked
fittings,
security
of
hinges,
defective
bearings,
cleanliness,
corrosion,
deformation,
sealing
and
tension.
(b)
FLUID
LINES
AND
HOSES
for:
leaks,
cracks,
dents,
kinks,
chafing,
proper
radius,
security,
corrosion,
deterioration,
obstruction
and
foreign
matter.
(c)
METAL
PARTS
for:
security
of
attachment,
cracks,
metal
distortion,
broken
spotwelds,
corrosion, condition
of
paint
and
any
other
apparent
damage.
(d)
WIRING
for:
security,
chafing,
burning,
defective
insulation,
loose
or
broken
terminals,
heat
deterioration
and
corroded
terminals.
(e)
BOLTS
IN
CRITICAL
AREAS
for:
correct
torque
in
accordance
with
torque
values
given
in
the
chart
in
Section
1,
when
installed
or
when
visual
inspection
indicates
the
need
for
a
torque
check.
NOTE
Torque
values
listed
in
Section
1 are
derived
from
oil-free
cadmium-plated
threads,
and
are
recommended
for
all
installation
procedures
contained in
this
book
except
where
other values
are
stipulated.
They
are not
to
be
used
for
checking
tightness
of
installed
parts
during
service.
(f
FILTERS,
SCREENS
&
FLUIDS
for:
cleanliness,
contamination
and'or
replacement
at
specified
intervals.
(g)
PILOTS
RESTRAINT
SYSTEM
for:
fading,
sun
or
ultra-violet deterioration
(graying),
thinning,
fraying
or
cutting,
defective
latches,
and
broken
stitching.
(h)
AIRCRAFT
FILE.
Miscellaneous
data,
information
and
licenses
are
a
part
of
the
aircraft
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
United
States
Federal
Aviation
Regulations.
Since
the
regulations
of
other
nations
may
require
other
documents
and
data,
owners
of
exported
aircraft
should
check
with
their
own
aviation
officials
to
determine
their
individual requirements.
To be
displayed in
the
aircraft at
all
times:
1.
Aircraft
Airworthiness
Certificate
(FAA
Form
8100-2).
2.
Aircraft
Registration
Certificate
(FAA
Form
8050-3).
3.
Aircraft
Radio
Station
License,
if
transmitter
is
installed
(FCC
Form
556).
To be
carried
in
the
aircraft
at
all
times:
1. Weight and
Balance,
and associated
papers
(Latest
copy
of
the
Repair
and
Alteration
Form,
FAA
Form
337,
if
applicable).
2.
Aircraft
Equipment
List
3.
FAA
Approved
Flight
Manual
(Beginning
with
1979
Models).
To be
made
available
upon
request:
1.
Aircraft
Log
book
and
Engine
Log
Book.
Temporary
Revision
2
-
Oct
3/94
2-21

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