Piper PA 28-181 User Manual

PIPER AIRCRAI'T CORPORÄ'I'I()N
lä-211-18t, ^RCHER tl
SI']CTION 2
I,IN,IITATIONS
2,?
POW}.:R PI,AN'I' I,IMITATIONS
1a)
Nun)bcr ol tingrnct
(b)
linrrnc Manuhcturer
(c)
Enrinc Modcl No
I
l-ycoming
O :16(l A4M or
O-:l6UA,lA with
l0-3878
(d)
Enrrne OperatinS
I-imits
(1)
T.rkeoll P{,wer
5 Minulc
Lrnrt
(BIIP)
(21
Txkcoll E
gine Stecd 5
Minutc I-inrn
(RPM)
(-l)
Maximunr Conrrnuous
Power
(BHP)
(4)
Maxinmm C0nlinuous
E'rgrne
Spccd
(RPMI
(5)
Maximum Orl
Tcmpcrature
({t
oilPrcssure
Minimum
(red
lrne)
Maximunr
(red
l,ne)
(7)
Fucl Prcssure
Minimum
(rcd
lrne)
Mrximünr
(rcd
line)
(8)
Fucl(AVCAS ONLY)
(minimum
grade)
(9)
Nunrber ol Propellers
(
l0) I'ropcll.r Manulacturer
(ll)ProfellerModcl
(
l2)Propcller D'amcle.
I
l.l)I'lol)ellcr lnlcrxncc
(slatrc
RPM
rr m.xinru r
penni\srblc
lhrottlc
sctlrng, ser level,
ISÄ)
IIJO
2tu)
l]8
2650
245'l:
:5 PSt
90
or lm PSI
0.5 PSI
13
PSI
Iin or ltnll-
I
la M8s5 0 62
?6IN.
?6 tN
Not
abole 2340 RPM
Nor hcl,)w
224{)RPM
NOTE
R. f'
.
rl.r
r.rtlJn"
rurnrc',.,n!(
n,dn r.'l li{ r.
l
tr
.LJ If
r.',lfrLrmrnL,ttr.'!c,l
.1.'lr.
rllr
undcr nor
slrnda.d eordttx,ns
ISS(lnl):
JTJLY
2, 1979
REVISBDT APRIL
2' 1998
vB-1120REPORT:

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