Piper PA 28-181 User Manual

PIPER AIRCRAFT CORPORATION
PA,28.18I. ARCHf,R II
SECTION 4
NORMAL
PROCf,DURf,S
SECTION 4
NORMAL PROCEDURES
.I.I
GENERAL
Ihis seciion describes the recommended
procedures
for the
conduct of
normrL operations for the Archer IL AII ofthe
fequired
(FAA
r€gularions)
procedures
and lhose necessary lbr operation ofthe
airpiane as d etermined
bv the operating and drsign features of the airplane are present€d.
\ornal
procedures
associated wilh those optional
syslems and equip-
ment
which require handbook
supplcments are
provided
by
Section 9
These
procedures
a.e
provided
ro
presenl
a source of reference
and
re\iew and ro suppl!- information on
procedures
$hich are nor rhe
same
fo.
all aifcraft. Pilots \hould familiarize thenselves
with lhe
procedures
Civen
in this section in order to become
proficien!
in lhe normal operations
of the
The firsl
poftion
ofthissectionconsists ofa shon fofm
check Iisl which
supplies an action sequence fo. normal operalions with litlle
emphasis on
lhe operation of !he svstem!.
The rernainder oftheseclion is devoted to amplilied
no rmal
procedures
qhrch
pro!ide
delailEd information and explanarions ol the procedu.es
and
how to pcrturm then Thi\ portion
of the section is no1 inlended for use as
an in Ilight relerenceduetothelengrhl!explanations.Theshorlformcheck
list should be used for this
purpose.
.1.3
AIRSPE[DS FOR SAFE OPERATIONS
the follo{ins ar.speeds are those
which
are signilicant to the safe
operalion of the airplane I hese ligufes arc for
slandard airplanes nown at
grcj\ \!cight under standard conditions at
sea level.
ISSUED: JLLY 2, 1979
REVISED: JULY 21, 1982
REPORTT VB-1120
+l

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