Piper PA 28-181 User Manual

SECTION 6 PITER AIRCRAFT
CORPORATION
WEIGHT AND BALANCE PA.28-181. ARCHER II
Bdsic Empty weighr
Pilot and Front Passenger
Passengers (Rear
Seäß)*
Fuel
(48
Cällon Maximum)
Baggage
(200
Lbs. Maximurn)*
Wcigbt Datum Momcnl
0-bt
(Inches) (In-Lbs)
ISSUED:
JULY
2, 1979
REVISED:
FEBRUARY
2, 1990
Touls musr be within approved weight
and C.c. limits. i1 is rhe responsi
bilily
of the airplane owner and üc
pilot
to insure that the
airplane
is loaded
properly.
The Basic Empry Weighr
C.G.
is noted
on the Wcight änd Balance
Datä
Forrn
(Figure
6-5). If
the
airplane has
been älrered, refer
to üe
Weight
andBalance Re.ord for this informalion.
*Ulilily
Catcgory Opcrätion
-
No baggage
or
rcar
passengers
allowed.
Ramp weighr
(2558
Lbs. Normal,
2138
Lbs. Ulility Maximum)
Fuel Allowancc
ForEngine
SDn, Taxi and Run Up
Takmff Weight
(2550
Lbs- Normal,
2130 Lbs.
Uliliry
llIaximurn)
REPORTT
VI}-U20
6-10
WEIGH'I' AND ßALANCE
LOADING FORM
Figure
6, t I

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