CESSNA
MODEL
172R
SECTION
8
HANDLING,
SERVICE
&
MAINTENANCE
One
exception
to
this
can
be
encountered when
operating
under
rthe
combined
effect of: (1) use of
certain
fuels,
with
(2)
high
humidity
conditions on the
ground (3) followed by flight at high
altitude and low
temperature.
Under these unusual
conditions, small
amounts
of water
in
solution can
precipitate from
the
fuel
stream
and
freeze
in
sufficient
quantities to
induce
partial
icing of
the
engine fuel
system.
While
these
conditions are quite
rare
and will
not normally
pose
a
problem
to
owners
and
operators, they
do exist
in
certain
areas
of
the world
and
consequently
must
be
dealt
with,
when encountered.
Therefore, to
help alleviate the
possibility of fuel icing occurring
under these unusual
conditions,
it is
permissible to
add
isopropyl
alcohol or
diethylene glycol monomethyl
ether
(DiEGME) compound
to
the
fuel supply.
The
introduction
of
alcohol or DiEGME
compound
into the
fuel
provides
two
distinct
effects: (1)
it absorbs
the dissolved
water
from
the
gasoline
and
(2)
alcohol
has a
freezing temperature
depressant
effect.
NOTE
When
using fuel additives, it must
be remembered
that the
final
goal
is
to
obtain a
correct
fuel-to-additive
ratio
in
the
tank,
and
not
just with
fuel coming
out
of
the
refueling
nozzle.
For example,
adding 15
gallons of correctly
proportioned fuel
to
a
tank which
contains
20
gallons of
untreated
fuel will
result
in a
lower-than-acceptable
concentration level
to
the
35 gallons of
fuel
which now
reside
in
the tank.
Alcohol, if
used,
is
to
be blended
with
the
fuel in
a concentration
of
1%
by
volume. Concentrations
greater
than
1%
are
not
recommended
since
they
can
be detrimental
to
fuel
tank materials.
The
manner
in
which
the
alcohol
is
added
to
the
fuel
is
significant because
alcohol is
most
effective when it is completely
i#*'
dissolved
in
the
fuel. To
ensure
proper
mixing, the
following
is
recommended:
1.
For best
results,
the alcohol should be added
during
the
fueling
operation by pouring
the alcohol
directly
on
the
fuel
stream
issuing from the fueling
nozzle.
Feb
28/00
8-17
Содержание 172R
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