Piper ARCHER II - Stall Warning

SECTION
7
PIPER
AIRCRAFT
CORPORATION
DESCRIPTION
&
OPERATION
PA-28-18],
ARCHER
II
Shoulder
harnesses
with
inertia
reels
are
provided
for
each
front
seat
occupant
and,
depending
on
the
model,
are
provided
as
standard
or
optional
equipment
for
the
occupants
of
the
rear
seats.
A
check
of
the
inertia
reel
mechanism
can
be
made
by
pulling
sharply
on
the
strap
and
checking
that
the
reel
will
lock
in
place
under
sudden
stress.
This
locking
feature
prevents
the
strap
from
extending,
and
holds
the
occupant
in
place.
Under
normal
movement
the
strap
will
extend
and
retract
as
required.
On
earlier
aircraft
provided
with
a
single
strap
adjustable
shoulder
harness
located
above
the
side
window
for
each
front
seat,
the
shoulder
strap
is
routed
over
the
shoulder
adjacent
to
the
window
and
attached
to
the
lap
belt
in
the
general
area
of
the
occupant’s
hip.
Adjust
this
fixed
Strap
so
that
all
controls
are
accessible
while
maintaining
adequate
restraint
for
the
occupant.
Optional
shoulder
straps
are
available
for
the
rear
occupants.
Shoulder
harnesses
should
be
routinely
worn
during
takeoff,
landing,
and
whenever
an
inflight
emergency
situation
occurs.
7.27 BAGGAGE AREA
A
24
cubic
foot
baggage
area,
located
behind
the
rear
seats,
is
accessible
either
from
the
cabin
or
through
an
outside
baggage
door
on
the
right
side
of
the
aircraft.
Maximum
capacity
is
200
pounds.
Tie-down
straps
are
provided
and
should
be
used
at
all
times.
_NOTE
it ts the pilot’s responsibility to be sure when
the baggage is loaded that the aircraft C.G. falls
within
the
allowable
C.G.
Range
(refer
to
Section 6 - Weight and Balance).
7.29 STALL WARNING
An
approaching
stall
is
indicated
by
a
stall
warning
horn
which
is
activated
between
five
and
ten
knots
above
stall
speed.
Mild
airframe
buffeting
and
gentle
pitching
may
also
precede
the
stall.
Stall
speeds
are
shown
on
graphs
in
the
Performance
Section.
The
stall
warning
horn
emits
a
continuous
sound
and
is
activated
by
a
lift
detector
installed
on
the
leading
edge
of
the
left
wing.
During
preflight,
the
stall
warning
system
should
be
checked
by
turning
the
master
switch
ON,
lifting
the
detector
and
checking
to
determine
if
the
horn
is
actuated.
REPORT:
VB-1120
ISSUED:
JULY
2,
1979
7-20
REVISED:
JULY
5,
1985