Piper PA 28-181 User Manual

PIPER AIRCRAFT CORPORATION
PA.28-T8T, ARCHER II
sEcTtoN 2
LIMITATIONS
SECTION 2
LIMITATIONS
2.1 GENERAL
This section
provides
rhe "FAA Approved"
operating limitarions,
instrument markings. cotor
coding and basic
placards
necessary for
opera-
don of the airplane and its sysiems.
This airplane must bc operated as a normal or utility
cat€gory airplane
in compliance
with
the
operaring limitalions
stated in the form
of
placards
and markings and those
given
in this section and this
complele handbook.
Limitations associated wirh those opiional sysrems
and equipmenr
which require handbook suppienents
can be found in
Section 9
(Supplemen!s).
2.3 AIRSPEED LIMIlATIONS
SPEEI)
Never
Exceed Speed
(VNE)'Do
not exceed
this speed in any operation.
Maximum Structural Cruising Speed
(VNO)'Do
not exceed this speed exccpt
rn
smooth air and lhen only uilh caurion.
KIAS
15,1
KCAS
118
ISSUED: JULY 2. 1979
REVISED:
JULY 21. 198?
l2l
REPORT:
vB-1120
125

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