Piper Cherokee Six - Page 31

PIPER
CHEROKEE
SIX
SERVICE
MANUAL
2-5.
ACCESS
AND
INSPECTION
PROVISIONS.
The
access
and
inspection
pro-
visions
for
the
airplane
are
shown
in
Figure
2-3.
The
component
to
be
serviced
or
inspected
through
each
opening
is
identified
in
the
illustration.
All
access
plates
and
panels
are
secured
by
eithermetal
fasteners
or
screws.
To
enter
the
aft
section
of
the
fuselage,
remove
the
rear
baggage
compartment
upholstery
panel
by
removing
the
attachment
screws.
CAUTION
Before
entering
the
aft
section
of
the
fuselage,
be
sure
the
airplane
is
supported
at
the
tail
skid.
2-6.
TOOLS
AND
TEST
EQUIPMENT.
Because
of
the
simplicity
and
easy
ac-
cessibility
of
components,
few
special
tools
outside
normal
shop
toolswill
be
re-
quired.
Tools
that
are
required
may
be
fabricated
from
dimensions
given
in
the
back
of
the
section
that
pertains
to
a
particular
component
or
are
listed
in
the
back
of
the
PA-32
Parts
Catalog.
2-7.
TORQUE
REQUIREMENTS.
The
torque
values
given
in
Table
II-II
are
derived
from
oil-free
cadmium-plated
threads
and
are
recommended
for
all
air-
frame
installation
procedures
where
torqueing
is
required,
unless
otherwise
noted
in
sections
where
other
values
are
stipulated.
Engine
torque
values
are
found
in
the
latest
revision
of
Avco-Lycoming
SSP
2070-3,
and
propeller
torque
values
are
found
in
Section
VII
or
VIIA
of
this
manual.
2-8.
STEP,
HANDHOLD,
AND
WALKWAYS.
A
fixed
handhold
is
located
on
the
right
side
of
the
fuselage,
above
and
aft
of
the
center
seat
window.
The
walkway
is
made
up
of
a
non-skid
compound
applied
to
the
wing
surface.
CAUTION
Walk
on
the
walkways
only
to
avoid
damage
to
the
wings.
Revised:
12/15/80
HANDLING
AND
SERVICING
1B7