Piper PA 28-181 User Manual

Sf,CTION 7 PIPIR
DESCRIPTION
& OPf RATION
AIRCRAt.'T
CORPORATION
PA-2E-181,
ARCHER
II
:::
...:....
.-,.-.,,,,
t:,.-.,
.
L_.:..
FUEL
SILECTOR
Figure 7 7
th. fuel
df.rins
\hould
be opencd
dail\
prior
ro lirsr
flighr ro ch.ck Ior
wat€f of sedrment and
propertu€l
lach
tankhasan Indi\idurldruinal
th€
bottom. rnboard .elrr corner
,\ lucl \trarner. located on th. lo$er
lelr ltunr
ofrhe fire
qatl.
has a drain
\rhich is accc\sible lron1 outsidc
!he nose secrron. The
slraincr
shoutd ilso b.
drained beiore the firsl ilight ol th.
da!. Relir ro paragraph
8 2l fof
rhe
complete lüel drarning
procedurc.
fuel
quantit)
and
prc!!ure
arc indicatcd
on
!auge\
locared
in a.tuncr
on the left \ide of lhe inslrument pancl.
An cngine
priming
s\\tcm is
pro\idcd
to l!cililare
na
ing.Thep.imcl
punlp i!
localed 1o
rhc imInediare
lell ol rh. throlrlc
quadranr
(rctir
to
Fisufc
r'5).
REPORT: \'B-1120
7-8
ISSt.
ED: JUI-!
2 1979
REl ISF:D:
JLNI
29, 198,1

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