Piper PA-32RT-300T User Manual

LANCE
II
SERVICE
MANUAL
SECTION
III
INSPECTION
3-1.
INTRODUCTION.
This
section
provides
instructions
for
conducting
inspections.
These
inspections
are
described
in
Paragraphs
3-4
and
3-5.
Repair
or
replacement
instructions
for
those
components
found
to
be
unserviceable
at
inspection
may
be
found
in
the
section
covering
the
applicable
aircraft
system.
CAUTION
When
working
on
engines.
ground
the
magneto
primary
circuit
before
performing
any
operation.
3-2.
RECOMMENDED
LUBRICANTS.
Refer
to
Recommended
Lubricants.
Section
II
for
Lubrication
Servicing
Instructions.
3-3.
INSPECTION
PERIODS.
3-4.
INSPECTION
REQUIREMENTS.
The
required
inspection
procedures
are
listed
in
Table
III-I.
The
inspection
procedure
is
broken
down
into
major
groups
which
are
Propeller.
Engine.
Turbocharger.
Cabin.
Fuselage
and
Empennage.
Wing.
Landing
Gear.
Operational
Inspection
and
General.
The
first
column
in
each
group
lists
the
inspection
or procedure
to
be
performed.
The
second
column
is
divided
into
four
columns
indicating
the
required
inspection
intervals
of
50
hours.
100
hours.
500
hours
and
1000
hours.
Each
inspection
or
operation
is
required
at
each
of
the
inspection
intervals
as
indicated
by
a circle
(O).
If
an
item
is
not
entirely
accessible
or
must
be
removed.
refer
to
the
applicable
section
of
this
manual
for
instructions
on
how
to
gain
access
to
remove
the
item.
When
performing
inspections.
use
the
Annual
inspection
form
P N
230
953
furnished
by
the
Piper
Factory
Service
Department.
available
through
Piper
Dealers
or
Distributors.
NOTE
In
addition
to
inspection
intervals
required
in
Table
III-I
a
preflight
check
must
be
performed
as
described
in
Paragraph
3-5.
Revised:
11/1/83
INSPECTION
1D6

Piper PA-32RT-300T Specifications

General

Brand	Piper
Model	PA-32RT-300T
Category	Aircrafts
Language	English