Piper PA 28-181 User Manual

PIPTR AIRCRAFT CORPORATION
PA.28.I8I. ARCHER II
SECTION I
G [\ERAI,
I.3 ENGINES
(a)
Numbcr of Engincs
(b)
Engine Vanuiaclufef
(c)
Engine Vodel \umber
(d)
Takeoff Poller
-
5 Minutc Limir
(BHP)
lc) lakeofi F:n8inc
Spccd 5 Nlinule
Limir
(
RPM)
(f)
\4aximum
Conrinuous
Po$er
(BHP)
(g)
Mäximunr Conrrnuous Engine
Specd
(
RPM)
(h)
Bore
(inches)
(i)
Srroke
(inch€s)
l-t) Displacemenr
(cublc
inch€s)
(k)
Compfc\sion Rario
(l)
Engrne Tlpe
PROPELLERS
(a)
\umbcf ol Prop.llcß
(b)
Propell.r M!nulacturcr
(c)
\.4 od el
(d)
Numb€r oi Alades
(c)
Prop.llc, Dianrer€f
(rnches)
(l)
Maximum
(ll
\.4inimum
(l)
I,ropeller Ilpe
t
titiL
AVGAS
ONI.Y
(a)
Fuel
Capacir)
ltr
S.
gal
)
(oral)
(b)
Usable Fucl
(U
S
gal
)(loral)
(c)
Fuel
(
1)
Minimum
Ocranc
(2)
Alternale
Fuel
I
Lrconlrng
0-160 A:lN4
or
o-160
A.1A
l8t)
tt00
ITIJ
2650
5.t25
.1.175
-16t.0
E.5:l
Four
Cvlindcr. Direct
Dri\e, H
orizontallv
Opposed.
Air Coohd
1.7
ISSLED: JLL\'2, 1979
REVISED:
Jt
\E
29, l9E4
I
l6EM8S5-0-62
2
76
50
48
100
creen o.
t00Lt_
Blue
A!ralron
crade
Refer
ro
laresl issue
of
LJ"comrng
lnsrruciion
No.
t070.
REPORT:
VA-1120
l"l

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