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Piper PA 28-181 User Manual

Piper PA 28-181
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PIPTR AIRCRAFT CORPORATION
PA.28.I8I. ARCHER
II
s[( TloN
,t
)ORMAL PROCEDLRES
Po$cr should be .
pplied
slo\\l! Io slarr th. 1!xi
foll. Ia\i r lls
leel
lor$ard and appll
thc
bralcs
to
dctcrnrnc
therr
ellecri\ene\\
\\hlletasins.
mrke
slighl lurns to ascertarn the ellcctL\cness of th.
\reerinq.
Obser\
c wing clearances \ hen rariing near buildilg\
or orher stariona.!
objects lf
possible.
slalronlrn obser\er outsidc thc rifplxne.
A\oid holes and ruls \rhen laxrlng o\er une\en
ground
I)o
noroperalc rhc.ngin.
ar high RPM $ hcn
run njng uf o. r!xii.g
o\ cl
griNnd contarning loose srones.
gra!el
or an) loosr nratcrial
lhat a\ causc
d!mage
ro the
propeller
blades.
.I,I9
CROUND CHECK
Ser the
parklng
bmkc.
The magnetos should be chected at 2000 RP\l t)rop
oif on rLrh.l
nrägnero
shoLrld nol exceed ll5 RI'M and thc dillcfcncc
bel\e.n rhc
nragnelos should nor
cxcc.d
50
RPNI
Operaoon on one mrsncro
llrould
nol
cxcccd 10 seconds.
Check
the racuum
gaugci
thc Lndrcrtor should
reld 5.0"
I
l
Hg ar
t000 R PNt.
Ch.ck
the annunciator
panel
lighrs $irh th.
fr.5\
1o-test bulloD {lso
chcck thc nrr
condrlroner.
Crrbureror
hear should also be checked
prior
to rakcif
ro bc \urc rh.
control is operating
properl!
and ro clear rn) icc $hich
maf ha\i lormed
during taxiing A\oid
prolonScd gfourd
operarron \rth cafbu'ctor
hcar
''O\"
as lhe air
is unlilt.red
Thc cleclric
luel
pump
should be rurned
OFF afref narring
or Curirg
$arm-up
ro make \u.e thar the ensine dri\.n pump
is op.rrriDe.
l)rior ro
lakeoll
the elect.ic
pump
shoLr ld be turned O\.' a8rin
io
pre\enl
lo\\ of
fo$cf
during rakeoff should
rhc cnginc
dri,"n
punrp
lail
Chcck borh oil rcmpcr-
atüre and oil
prcssu.c. The
rcmperalur€ IIla\ be lo$ fof
\onre rimc il rhe
enginc
i\
bcrng
run lirr the 1ißr tint
of
rhc
dr\. lhe engrn! i. safm
enoLrsh
1or takcofl
uhen thc throttle can b0 opcned $ilhout
thc cnginc fallerin!.
ISSUID:
JtrLY 2, 1979
REVIStrD: JLNf 29,
1981
REPOR'I: VA-1120
.t-15

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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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