EasyManua.ls Logo

Piper ARCHER II - Page 157

Piper ARCHER II
286 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
PIPER
AIRCRAFT
CORPORATION
SECTION
7
PA-28-181,
ARCHER
II
DESCRIPTION
&
OPERATION
7.31
FINISH
All
exterior
surfaces
are
primed
with
etching
primer
and
finished
with
acrylic
lacquer.
An
optional
polyurethane
finish
is
available.
7.33
AIR
CONDITIONING*
The
air
conditioning
system
is
a
recirculating
air
system.
The major
items
include:
evaporator,
condenser,
compressor,
blower,
switches
and
temperature
controls.
The
evaporator
is
located
behind
the
left
rear
side
of
the
baggage
com-
partment.
This
cools
the
air
that
is
used
for
air
conditioning.
The
condenser
is
mounted
on
a
retractable
scoop
located
on
the
bottom
of
the
fuselage
and
to
the
rear
of
the
baggage
compartment
area.
The
scoop
extends
when
the
air
conditioner
is
ON
and
retracts
toa
flush
position
when
the
system
is
OFF.
The
compressor
is
mounted
on
the
forward
right
underside
of
the
engine.
It
has
an
electric
clutch
which
automatically
engages
or
disengages
the
compressor
to
the
belt
drive
system
of
the
compressor.
An
electrical
blower
is
mounted
on
the
aft
side
of
the
rear
cabin
panel.
Air
from
the
baggage
area
is
drawn
through
the
evaporator
by
the
blower
and
distributed
through
an
overhead
duct
to
individual
outlets
located
adjacent
to
each
occupant.
The
switches
and
temperature
control
are
located
on
the
lower
right
side
of
the
instrument
panel
in
the
climate
control
center
panel.
The
temperature
control
regulates
the
desired
temperature
of
the
cabin.
Turn
the
control
clockwise
for
increased
cooling,
counterclockwise
for
decreased
cooling.
*Optional
equipment
ISSUED:
JULY
2,
1979
REPORT:
VB-11290
REVISED:
JUNE
29,
1984
7-21

Table of Contents