Piper CHEROKEE ARCHER II Pilot Operating Handbook page 49

PIPER AIRCRAFT CORPORATION
PA.28.I8I,
CHEROKEE ARCHER
II
SECTTON 4
NORMAL
PROCEDURES
SECTION 4
NORMAL
PROCEDURES
4,1
GENERAL
This section clearly describes the recommended procedures
for
the conduct of normal
operations
for
the
Cherokee
Archer
II. All of
the required
(FAA
regulations) procedures and those
necessary
for
the
safe
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 equipment 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 sttould 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 strort
form
check
list which
zupplies an
action
sequence
for normal operations with
little
emphasis
on the operation
of
the systems.
The remainder
of
the
sction 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 lengthly explanations. The short
form
check list
should be used
for
this purpose.
4.3
AIRSPEEDS FOR SAFE OPERATIONS
The following
airspeeds
are thoce which are significant
to
the safe operation
of
the airplane.
These
figures are
for
standard airplanes
flown
at
gros
wEight under standard conditions at
sea
level.
Performance
for a specific airplane may vary from
publistred figures depending upon the equipment
installed,
the condition
of
the
engine, airplane and equipment, atmospheric conditions and piloting
technique.
(a)
Best Rate
of Climb
Speed
(b)
Best
fuigle of Climb
Speed
(c)
Turbulent Air Operating Speed (See Submction 2.3)
(d)
Maximum Flap
Speed
(e)
Landing Final Approach
Speed
(Flaps 40o)
(0
Ma:cimum Demonstrated Crosswind
Velocity
76
KIAS
64
KIAS
I 13
KIAS
I02 KIAS
66 KIAS
I7
KTS
REFORT:
V8790
+t
ISSUED:
IIJNE
18, 1976