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Raytheon Beech Baron E55 - Page 143

Raytheon Beech Baron E55
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RBYtheoll
Aircraft
Company
BARON
55
AND
58
SHOP
MANUAL
ICE
REMOVAL
Moderate
or
heavy
ice
and
residual
snow
deposits
should
be
removed
using
heated
water
or
deicing
fluid.
No
attempt
should
be
made
to
remove
ice
deposits
or
break
an
ice
bond
by
force.
If
heated
water
is
used
to
remove
ice
and
snow
deposits,
allow
adequate
time
for
water
to
drain
from
the
airplane
or
dry
the
airplane
with
a
soft
cloth
before
exposing
the
airplane
to
subfreezing
temperatures
in
order
to
prevent
refreezing.
After
completing
the
deicing
process,
the
airplane
should
be
inspected
to
ensure
that
its
condition
is
satisfactory
for
flight.
All
external
surfaces
should
be
examined
for
residual
ice,
snow,
or
frost.
Particular
attention
should
be
paid
to
control
surfaces
gaps
and
hinges.
Carefully
inspect
static
ports
and
vents
for
any
signs
of
obstruction.
Control
surfaces
should
be
moved
to
ascertain
they
have
full
and
free
movement.
Landing
gear
mechanism,
doors,
wheel
wells,
uplocks
and
microswitches
should
be
checked
for
ice
deposits
that
may
impair
function.
When
the
airplane
is
hangared
to
melt
ice,
any
melted
ice
may
freeze
again
if
the
airplane
is
subsequently
moved
into
freezing
temperatures.
Any
measures
taken
to
remove
frozen
deposits
while
the
airplane
is
on
the
ground
must
also
prevent
the
possible
refreezing
of
the
liquid.
Should
freezing
precipitation
continue
following
ice
removal,
treat
the
airplane
surfaces
for
anti-icing.
WARNING:
If
icing
exists
on
the
airplane
after
surface
treatment
for
anti-icing,
complete
deicing
and
the
sur-
face
treatment
for
anti-icing
must
be
completed
prior
to
flight.
SAE
TYPE
I
ANTI-ICING
FLUIDS
(UNTHICKENED-TYPE
FLUIDS)
SAE
Type
I
fluids
mainly
provide
protection
against
refreezing
when
there
is
no
precipitation.
All
approved
Type
I
fluids
may
be
used
for
either
deicing
or
anti-icing
at
any
dilution
as
allowed
by
the
fluid
manufacturer’s
recommendations.
DEICING
Deicing
is
a
procedure
by
which
frost,
ice
or
snow
are
removed
from
the
airplane.
To
preserve
holdover
time,
the
process
should
be
continuous
and
as
brief
as
possible.
In
active
precipitation,
deicing
should
be
performed
at
the
last
practicable
moment.
The
deicing
agent
should
be
applied
in
a
heated
state
to
assure
maximum
efficiency.
ONE
STEP
DEICING
One
step
deicing
is
done
with
a
heated
mixture
of
anti-icing
fluid/water
formulated
to
provide
a
freezing
point
buffer
at
least
10"
C
below
the
ambient
temperature.
TWO-STEP
DEICINC
The
first
step
of
deicing
is
done
with
hot
water
or
a
hot
mixture
of
anti-icing
fluid/water
formulated
to
provide
a
fluid
freezing
point
of
no
more
than
7xC
above
ambient
temperature.
This
is
followed
by
the
second
step
of
anti-icing:
an
overspray
with
a
mixture
of
anti-icing
fluid/water
or
of
100%
anti-icing
fluid
formulated
to
provide
a
fluid
freezing
point
of
at
least
10xC
below
ambient
temperature.
The
second
step
MUST
BE
performed
within
three
minutes
of
the
beginning
of
step
1
and,
if
necessary,
area-by-area.
ANTI-ICING
Anti-icing
is
a
precautionary
measure
which
prevents
frost,
ice
or
snow
from
forming
or
accumulating
on
the
protected
surface
of
the
airplane.
CAUTION:
If
an
additional
treatment
after
deicing/anti-icing
is
required
before
the
next
flight,
anti-icing
alone
is
not
recommended.
ALWAYS
PERFORM
A
COMPLETE
DEICING.
Page
SECTION
2

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