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Cessna 182 1978 - Static System Test Equipment

Cessna 182 1978
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MODEL
182
&
T182
SERIES
SERVICE
MANUAL
NOTE
Air
bulb
with
check
valves
may
be
obtained
locally from
a
surgical
supply company.
This
is
the type
used
in
measuring
blood
pressure.
THICK-WALLED
PRESSURE
SURGICAL
HOSE
PRESSURE
BLEED-OFF
SCREW (CLOSED)-
AIR
BULB
WITH
CHECK
VALVES
CLAMP
THICK-WALLED
SURGICAL
HOSE
CHECK
VALVE
SUCTION
CHECK
VALVE
TO
APPLY
SUCTION:
1.
Squeeze
air
bulb
to
expel
as
much
air
as
possible.
2.
Hold
suction hose
firmly
against static
pressure
source
opening.
3.
Slowly
release
air
bulb
to
obtain
desired
suction, then
pinch
hose
shut
tightly
to
trap
suction
in
system.
4.
After
leak
test,
release
suction
slowly
by
intermittently
allowing
a small
amount
of
air
to
enter
static
system.
To
do
this, tilt
end
of
suction
hose
away
from
opening,
then
immediately
tilt
it
back
against
opening.
Wait
until
vertical
speed
indicator
approaches
zero,
then
repeat.
Con-
tinue
to
admit
this
small
amount
of
air
intermittently
until
all
suction
is
released,
then
remove
test
equipment.
TO
APPLY
PRESSURE:
Do
not
apply
positive
pressure
with
airspeed
indicator
or
vertical
speed
indicator
connected
into
static
system.
1.
Hold
pressure
hose
firmly
against static
pressure
source
opening.
2.
Slowly
squeeze
air
bulb
to
apply
desired
pressure
to
static
system. Desired
pressure
may
be
maintained
by
repeatedly
squeezing
bulb
to
replace
any
air
escaping
through
leaks.
3.
Release
pressure
by
slowly opening
pressure
bleed-off
screw,
then
remove
test
equipment.
Figure
15-5.
Static
System
Test
Equipment
15-10

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