Piper PA 28-181 User Manual

SECTION 6
WEIGHT AND
BALANCE
PIPEN
AIRCRAFT
CORPORATION
PA.2&I6I,
ARCHER
II
Scale
Position and Symbol
Scale
Reading
Net
Tare
Wcight
Nosc
Wheel (N)
Right Main Whccl
(R)
l,eft Main Wheel (L)
Bssic Empty Weight,
as Weighed
(T)
WEIGHINC
FORM
Figure
Gl
(d)
Basic
Enpty Weighr
Cenrer of
cravity
(l)
The following
geomerry
applies to
the
pA-28-l8l
airplane
when it is
level. Refer
to L€veling
paragraph
6.1
(b).
tl
*^-l
The
datum
is
?8.4
inches
ahead
of rl
wing leading
edge
at the intersection
of the stdiSht
and tapeled
section.
B
=
3l.0
=
109.1
LEVELING
DIAGRAM
Figure
6-3
REPORT:
VBll20
G4
CG.
ISSUED:
JULY
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