Piper PA 28-181 User Manual

PIPER AIRCRAFT CORPORATION
P4.28.18I. ARCHf,R II
Sf,CTION
6
WEICHT
AND BALANCE
(2)
lhc
basic empiy
including oprional
can be deternlined
CC Arm:N(A)
$eighr cenler
of
gravirr (as
$ciShed
equipmenr.
lull oil
and unusable
fuel)
br rhc following
formuhl
+
(R
+
L)
(B)
inchcs
T
where T:N+R+L
6.5 WtrIGHT AND BALANCE DATA
AND RICORD
The Basic En1pr) Weight.
Ccnrcr ofCravity Locatrcn
and UsefulLord
lisred in Figure 6-5 are lor rhe äirplane
as licensed al thc lacior!.
Thesc
ligLr.. dpnl) onlt ro rhe.oec||rJ JIt ,rc
.er,al
rumo.
.rrJ
r.g:'rr".ror
The basic cmprr'seighr oI the
airplanc as hcenscd at
the iäclor, ha\
been enlefed 1n the
weighr
and Balance
Rcco.d
(Figu.e
6-l). This
form is
p.o!rded
lo
present
the currenl stalus ol
thc aifplane bäsic emplf
weight and
a complere hrsror! o1
pre!ious
nrodrfication!
Anf.hanee
to rhc
permanentlt
Innalled equipmenl or modilcilion {hich
aillcts $eighl
or
momenl must be eDtcred in rhc WeiSht
and Balance Rccofd
ISSUED: JULY 2, 1979
REVISEDT JUNE 29, 198'l
120
REPORT: VB-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