Piper PA 28-181 User Manual

sEcTtoN
5
PERFORMANCE
PIPER
AIRCRAFT CORPORATION
PA.2&TtT. ARCHER
II
I
Thc informar ion
provid€d
by
paragraph
5.5
(
FIigh I Planning
E xa mpte)
loutlines
a det8iled flight
plan
using
the
p€rforrnancc
chans
in this sccrion.
lEach
chart includ$ its own cxample
to show how ir is used.
WARNING
Performancc information
derivcd bv extraoo-
lation beyond rhc limirs
sho*n onihe ch;rt,
should not be uscd for
flight
planning
DUTDOSeS.
REPORT:
VE-U20
5-2
ISSUED:
JULY 2, 1979
REVISED
JUNE 25, I9tT

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