Piper Cherokee Arrow II Pilots Operating Manual page 42

ARROW I1
BAGGAGE AREA
A large baggage area, located behind the rear seats, is accessible either from the cabin or
through a large outside baggage door on the right side of the aircraft. Maximum capacity is 200
lbs. Tie-down straps are provided and should be used at all times.
NOTE
It is the pilot's responsibility to be sure when the baggage is
loaded that the aircraft C.G. falls within the allowable C.G.
Range. (See Weight and Balance Section.)
STALL WARNING
An approaching stall is indicated by a stall warning indicator which is activated between
five and ten miles per hour above stall speed. Mild airframe buffeting and gentle pitching may
also precede the stall. Stall speeds are shown on graphs in the Performance Charts Section. The
stall warning indicator is a red warning light on the left side of the instrument panel on earlier
models and a continuous sounding horn located behind the instrument panel on later models.
The landing gear horn is different in that it emits a 90 cycles per minute beeping sound on later
models. The stall warning indicator is activated by a lift detector installed on the leading edge of
the left wing. During preflight, the stall warning system should be checked by turning the
master switch "ON," lifting the detector and checking to determine if the indicator is actuated.
The exterior of the aircraft is finished with a durable acrylic lacquer in a variety of tasteful
I
colors to suit individual owners.
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 compartment. 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 to a 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.
*Optional Equipment
AIRPLANE AND SYSTEMS
REVISED: FEBRUARY 29,1984