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CESSNA
MODEL
172R
SECTION 3
EMERGENCY PROCEDURES
INSUFFICIENT RATE OF CHARGE
NOTE
The low
voltage
annunciator (VOLTS) may
come on and
I
ammeter discharge
indications
may
occur
during
low RPM
conditions with
an
electrical
load
on
the
system,
such
as
during
a
low RPM taxi. Under
these
conditions, the
■
annuciator
will go
off at higher
RPM.
I
If
the
overvoltage
sensor should shut down the alternator
and
trip
the
alternator
circuit breaker
(ALT FLD),
or
if
the alternator
output
is|
low,
a
discharge rate
will
be
shown
on
the
ammeter
followed by
illumination
of
the
low
voltage annunciator (VOLTS).
Since
thisl
may
be a "nuisance"
trip
out,
an
attempt
should
be made
to
reactivate the
alternator
system.
To reactivate,
set
the
avionics!
master
switch to
the OFF position,
check
that the alternator
circuit!
breaker
(ALT FLD) is in,
then
set
both
sides
of
the
master
switch
tol
the
OFF position and then
to
the ON
position. If
the
problem
no|
longer exists, normal alternator charging will
resume
and the low
voltage
annunciator
(VOLTS) will go off. The avionics
master
switch
I
may
then be returned
to
the
ON position.
|
If
the
annunciator
illuminates
again,
a
malfunction
is
confirmed.!
In
this
event,
the flight should
be
terminated
and/or
the
current
drain
on the
battery
minimized
because the battery
can
supply
the
electrical
system
for only a
limited
period
of
time. Battery power
must be
conserved for later operation
of
the
wing flaps
and, if
the
emergency
occurs
at
night,
for
possible
use
of the landing
lights
during landing.
OTHER
EMERGENCIES
WINDSHIELD DAMAGE
If
a
bird strike
or other
incident
should damage
the windshield
in
flight to
the
point of
creating
an
opening,
a
significant
loss
in
performance may be
expected.
This loss
may
be
minimized
in
some
cases
(depending
on
amount
of damage, altitude,
etc.) by
opening
the
side
windows while the airplane is maneuvered
for
a
landing at
the
nearest
airport.
If
airplane performance or other
adverse
conditions
preclude
landing
at
an airport, prepare for
an
"off
airport"
landing
in accordance
with
the
Precautionary
Landing
With
Engine
Power
or
Ditching
checklists.
Revision
7
3-23/3-24
Summary of Contents for 172R
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