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Piper PA-28-161 User Manual

Piper PA-28-161
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PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR
II
SECTION 4
SECTION 4
NORMAL PROCEDURES
NORMAL PROCEDURES
4.1 GENERAL
This
section describes the
recommended
procedures
for the
conduct
of
norma
1
operations
for the
Warrior
I I. All
of
the
rcqui red
(FAA
regulations)
procedures
and
those
necessary
for
operation
of
the
airplane
as determined
by the
operating
and
design features
of
the
airplane
are
presented.
Normal
procedures
associated
with
those
optional
systems
and
equip-
ment
which
require
handbook
supplements
are
provided by Section 9
(Supplements).
These
procedures
are
provided
to
present a
source
of
reference
and
review
and
to
supply
information
on
procedures
which
are
not
the
same
for
all
aircraft.
Pilots should familiarize themselves
with
the
procedures
given
in this section in
order
to
become
proficient
in
the
normal
operations
of
the
airplane.
The
first
portion
of
this section consists
of
a
short
form
checklist which
supplies
an
action
sequence
for
normal
operations
with little
emphasis
on
the
operation
of
the
systems.
The
remainder
of
the section is devoted
to
amplified
normal
procedures
which
provide
detailed
information
and
explanations
of
the
procedures
and
how
to
perform
them.
This
portion
of
the section
is
not
intended for
use
as
an
in-flight reference
due
to
the lengthy
explanations.
The
short
form
checklist
should
be used
for
this purpose.
ISSUED: AUGUST 13, 1982
REPORT:
VB-ll80
4-1

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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