Piper PA 28-181 User Manual

SECTION
4
NORMAL
PROCEDURES
PIPER
AIRCRAFT
CORPORATTON
PA-28.I8T.
ARCHER
II
4.1I
WEIGHT
AND BALANCE
It
is the responsibility
of rhe orvner
and
pilor
to delerminc
tha! the
airplane remarns within thc allowable
weighl !s cenrer
ofgravity
envelope
while
in
flight.
For weight and balance dara,
ref€r to Secrion
6
(Weigh!
and Ba1änce).
REPORT:
VB-1120
ISSUEDT
NOVEMBER 16.
l98l

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