Specifications

CHEROKEE
SIX.3OO
An optioncl
electric
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
temperature
of
the cabin.
Turning the
control
clockwise increases
cooling;counterclockwise
decreases
cooling.
The
fan
speed
switch and
the air conditioning
ON-OFF
switch are inboard of
the
temperature control. The
fan
can
be operated
independently
of
the
air
conditioning;however,
the
fan
must
be
on for
air
conditioner operation. Turning
either
switch off
will
disengage
the
compresso!
clutch and retract
the condenser door.
Cooling air
should
be felt within one
minute
after the air
conditioner is turned on.
NOTE
If
the
system is
not
operating
in
5 minutes,
turn the system OFF
until the
fault is corrected.
The
fan
switch
alldws operation
of
the fan with
the air
conditioner
turned OFF to
aid
in
cabin
air circulation.
"LOW,"
"MED"
or
"HIGH"
can
be
selected
to direct a flow
of air through
the air conditioner outlets
in
the
overhead
duct.
These outlets can be adiusted or
turned off
individuallly.
The condenser
door
light
is located
to the rieht
of
the
engine
instrument
cluster
in front of
the
pilot.
The
door
light illuminates when the door is
open and is
off
when the
door is closed.
A circuit breaker
on
the circuit breaker
panel
protects
the
air conditioning
electrical
system.
Whenever
the
throttle is
in the
full
forward
position,
it
actuates a
micro
switch which
disengages the compressor and
retracts the
scoop.
This
allows
maximum
power
and
maximum
rate
of
climb. The fan continues to operate
and
the
air
will
remain
cool
for about
one minute.
When
the
throttle
is retarded approximately
ll4
inch, the
clutch
will engage, the
scoop
will
extend, and the system
will
again
supply cool, dry
air.
PIPER EXTERNAL POWERI
An optional starting installation known
as Piper
External Power
(PEP)
is
accessible
through
a
receptacle located
on
the left side
of
the
nose section
aft
of the
cowling.
An external battery
can
be
connected
to
the
socket, thus
allowing
the operator
to
crank
the
engine
without
having
to
gain
access to the airplane's
battery.
*Optional
equipment
AIRPLANE AND SYSTEMS
ISSUED:
JULY
12,1973
2-r9