Piper PA 28-181 User Manual

PIPER AIRCRAFT CORPORATION
PA.28.181. ARCHER
II
Sf,CTION
4
NORMAI,
PROCEDURfS
Tre do$ns can be securcd !o nngs
provided
undcr
each w;)g and
ro the
tail skid. l
he
rudder
is held in position
by irs connecrions
!o the nose whecl
sreering and
nornally
does
not have to be
secured.
4.37 STALLS
The slall characlerisrics ofthe Archer llarc con!entional. An
approach-
ing s1all is indicated
by
a stall
w.trnins horn
which is acri\ ated
bclween li!e
änd ten knots above srall speed. Mrld arrlrane buffeting
and
genrle
pitching
may also
precede
the slal1.
The
gross
weiCht slalling speed of lhe Archer II with powcr
olT and full
flaps
is 49 KIAS. With the llaps üp thrs
spced
is increased
6 KTS t-oss
of
altilude
during sralls varies lrom 100 to 150 ieet,
depcnding on conlrgurarion
\O-I
E
The stall $arning 5,"-stem is inoperative $ irh rhc
ma(er swilch OFF.
During
prefli8h1.
the slall $afnine sysrem should be chcckcd
br rLrrning
the maner
switch
ON. liliing the detcclor and checking
ro determinc if
rhe
horn is actualed The masrer swilch should be rerurned to
the OFF
posirion
afler the check
is
complelc.
4.39 TURBULENT AIR OPERATION
ln keeping \ruh
good
.'perarrng
pracrice
used
in
all ai.crah, ir is rccom,
mended that when turbulcn! air is encountered or expccted.
lhe ai.speed bc
rcduced
to
maneulering spced 1o reducc
thc strucru.al loads
caus€d b!
gusrs
and
to
allo\! for inad\ertent speed
build-ups $ hich ma\ occuf
as a result ol
lhe lurbulence
or
ol dinractions caused by the condirrcns.
(See
Subsecrion
2.l)
ISSUfD:
JULY 2. 1979
RfvlSED:
NOvtrMB[R
16, l98l
RtrPORT: vB-1120

Piper PA 28-181 Specifications

General

Manufacturer	Piper Aircraft
Engine	Lycoming O-360-A4M
Horsepower	180 hp
Wingspan	35 ft 6 in (10.82 m)
Height	7 ft 3 in (2.21 m)
Maximum Takeoff Weight	2, 550 lb (1, 157 kg)
Seating	4
Service Ceiling	14, 100 ft
Fuel Capacity	50 US gal (190 L)
Propeller	Fixed Pitch