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Piper PA 28-181 User Manual

Piper PA 28-181
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7.3I FINISH
All cxterior surfaccs
are primed wilh etching pfimcr
and linished
wilh
An optional
polyurelhäne lin;sh rs a!aihble.
?.33 AIR CONDITIONING+
The air condilioning syslcm
is
a fccirculating air slsrem. The ma.Jor
items
include: e\aporator. condenser, compressor. blower, ssrlchcs
and
lcmperatu.e
controls.
Thc c\aporator is locared behind the left reaf side ol the bägsage
com-
partment. This cools the air that
is
used for air condirioning.
I hecondenscr
is nounred on a retractable scoop locatcd onthebotlom
of the iuselage
and to the rear ot the baggage comparlment a.ea. The
scoop
extends
when
thc air
conditioner is
ON
:t nd retracls ro a Ilush position
when
the slstenr
is
OFF
The conpressor is mounled on the
forward
right undeßide ol rhc
engine. It has an
clcct.ic clutch {hich automalicrllr enSagcs
or disengages
lhc
compressor to the belt dri\e svs!em of the compressor
An electrical blowcr
i\ n1ounlcd
on
the
aft
side
ol
rhc
rcaf cabin
panel.
Air from the baggagc arca
is
drawn
rhrou!h the
c!apor!ror bv the blo*er
and distfibulcd
through an o\erherd duct 1o indivrdurl oullcrs
located
adjacenl 10
cach occupant.
The \$itches and tempe'aturr controlafc
localed
on the lo\ver right side
of rhe
insrrument
panel
in lhe climäte control center
panel.
The temperature
conrrcl
regulates rhe desircd lcmpefaturc of lhe cabin Turn the conl.ol
clockuise
lor increased cooling, counrerclock\rise for
decreased cooling.
PIPf,R
AIRCRAFT CORPORATION
SICTION
7
PA.28-ItI. ARCHER II DESCRIPTION
& OPf,RATION
*OprLonal
equrpmcnt
ISSLED: JULY
2, 1979
RfvlsfD: JUNE
29, l9E4
RIPORT: VB-1120
7-21

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Piper PA 28-181 Specifications

General IconGeneral
ManufacturerPiper Aircraft
EngineLycoming O-360-A4M
Horsepower180 hp
Wingspan35 ft 6 in (10.82 m)
Height7 ft 3 in (2.21 m)
Maximum Takeoff Weight2, 550 lb (1, 157 kg)
Seating4
Service Ceiling14, 100 ft
Fuel Capacity50 US gal (190 L)
PropellerFixed Pitch

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