Mooney M20K - Power Distribution System

MOONEY
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
24-60-00
ELECTRICAL
LOAD
DISTRIBUTION
STANDBY
GENERATOR
Optional
(25-0001
thru
25-0999)
When attemator
failure
occurs,
the altemator
24Si-00
POWER
DISTRIBUTION
SYSTEM
output
and
battery
circuit
breakers must
be
pulled
to
The
power
bus
distributes
direct
current
power
to
the
de-energize
the
control
relay
and
connect
the
standby
electn’cal
system
from
the aitemator
and
from the
generator
to
the
standby generator
bus.
This
will allow
battery
through
the
battery
relay.
The
negative
battery
limited
equipment
to
be
operated
until
aircraft
can
be
lead
attaches
to
a
structural
ground
on
the airframe,
landed
and the alternator
system
repaired.
Master
Switch
"ON"
closes
the
relay
and
supplies
power
to
the
aircraft
electrical
system.
CAUTION
Do
not
reset
a
circuit
breaker
after
it has
tripped
a
second
time.
If
necessary
to
do
so
to
locate the
malfunction,
be
alert for
a
possible
electrical fire. Breakers are
Yn’p
Free"
type
and
cannot
be
held
in
the
closed
position.
24-50-00
24
OLDWILLWAYNE