EasyManua.ls Logo

Cessna 150K - Stall Warning System Operation

Cessna 150K
358 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
3
7-+---""'"
Detail
B
NOTE
Bug
screen
(7)
should
be
inspected
and
cleaned
periodically.
1.
Doorpost
Cover
2.
Horn
Assembly
3.
Scoop
4.
Adapter
5.
Felt
Seal
6.
Adjustable
Plate
7.
Screen
Figure
15-7.
Stall
Warning
System
15-48.
ACCELEROMETER.
15-49.
DESCRIPTION.
The
Aerobat
offers
an
accelerometer
to
assist
pilot
in
performing
precision
aerobatics.
The
accelerometer
continuously
indi-
cates
g
forces
being
imposed
on
aircraft.
The
dial
display
utilizes
three
pointers;
one
pointer
indicates
instantaneous
acceleration,
another
records
maxi-
mum
positive
acceleration
and
the
third
records
maximum
negative
acceleration.
Maximum
instru-
ment
markings
range
from
lOG
to
5G. A
"PUSH
TO
SET"
knob,
located
on
lower
left
corner
of
instru-
ment,
is
used
to
reset
"Maximum
Positive"
and
"Maximum
Negative"
pOinters.
If
dual
Nav/Coms
are
installed,
the
accelerometer
is
installed
in
a
housing
above
instrument
panel
on
pilot's
side.
When
aircraft
is
equipped
with
single
Nav/Com,
accelero-
meter
is
installed
in
the
vacant
Omni
indicator
instru-
ment
space.
15-18
15-50.
STALL
WARNING SYSTEM.
(Refer
to
figure
15-7.
)
15-51.
DESCRIPTION.
The
system
is
composed
of
an
adjustable
plate
on
left
wing
leading
edge,
con-
nected
to
a
reed
type
horn
by
means
of
plastic
tubing.
The
horn
is
actuated
approximately
5
to
10
miles
per
hour
above
stalling
speed
as
a
negative
air
pressure
area
at
wing
leading
edge
causes
a
reverse
flow of
air
through
horn.
By
moving
adjustable
plate
(6)
up,
actuation
of
horn
will
occur
at
a
higher
speed
and
moving
plate
down
causes
actuation
to
occur
at
a
slower
speed.
Center
adjustable
plate
opening
in
wing
leading
edge
upon
installation,
then
flight
test
aircraft,
observing
horn
actuation
during
stall.
Re-
adjust
plate
to
obtain
deSired
results
if
necessary.
Approximately
3/32
inch
adjustment
of
plate
will
change
speed
at
which
horn
actuation
occurs
by 5
miles
per
hour.
To
test
horn
operation,
cover
opening
in
plate
(6)
with
a
clean
cloth,
such
as
a
handkerchief
and
apply
a
slight
suction
by
mouth
to
draw
air
through
horn.

Table of Contents

Other manuals for Cessna 150K

Related product manuals