Piper PA 28-181 User Manual

SECTION
2
I,IMI'TdI'IONS
PIPIJR
AIRCRAI.'1' CORPORA'TI0N
PA.2II-IIiI.
ARCTIIiR
II
2.9 POWI'R
P[,ANT INS'I'RTJMENT
]\TARKINCS
(!)
lich(nrcter
Green Arc
(N('rmal
Openting
Rangc)
Yclk)w
Arc
(5
Mrnurc Limir)
Rcd 1-irc
(Takeolf
Powcr)
(b)
OllTcmpcrrturc
G.cen Arc
(Norm.rl
Ol'eraling
Rrngc)
Red Lrne
(Miximum)
(c)
oi1 Prcssurc
Crccn,\rc
(Nomal
Operatrng
Rangc)
Yellow Arc
(Caulion
Range)
(Idlc)
Yellow Afc
(Cround
warm
Up)
Red L,nc
(Minimunt
Red l.ine
(Maximun)
(d)
Fucl
Pressure
Orccn Arc
iNormal Operating
Rangc)
Red t.'ne
(M'n'm'rm)
Red L,ne
(Mlximuul)
2.II WEIGHT LIMITS
500 ro
1650
RIrNI
2650 to 270i)
Rl,N4
t7m
RPI,I
75'
lo 2.1i'l:
215"t:
60
l'SI to 90 l,SI
25 PSI
lo 60 PSI
None
or 90l,Sl
to 100
PSI
25 PSI
90
(,f
100 PSI
0.5 PSI
lo 8 PSI
0,5 PSI
II
ISI
(a)
(c)
Mrii,rum Rlmp
(lbs.)
Maxinlun Weight
(lbs.)
Maximunr BdggrSe
(lbs
)
NO,t.u
Refer ro Scction
5
(Pcfionrränc.)
weight as limrred
by
pcrlorman.c.
Nornul
255IJ
2550
200
Llnlirv
2l
llJ
2ll0
0
REITORT: Vß-1120
ISSUED:
JTJLY
2, 1979

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