Mooney M20K - General Description and Operation; Interior Lights - Maintenance Practices

MOONEY
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
33-00-00
GENERAL
DESCRIPTION
AND
the
light
near
the
cc-pilots
head.
The
passenger/
OPERATION
baggage
compartment
lights
are
located
above
the
rear
seats
in
the
overhead
panel
and
are
activated
by
a
High
intensity
strobe
lights
are
standard
equipment
on
similar
three
position
switch
located
adjacent
to
the
M20K
aircraft.
The
lights
are
located
adjacent
to
the
wing
light.
The
rear
cabin
light
switch
is
accessible
from
the
tip
navigation
lights
and
incorporated
into
the
taillight
assembly.
Separate
power
supplies
are
utilhed
for
each
baggage
compartment
door
also.
strobe
light;
these
are
located
in
each
wing
outboard
CAUTION
section,
mounted
on
inspection
covers,
and
inside
the
These
cabin
ligMs
are
connected
directly
to
the
tallcone
adjacent
to
the
left
rear
inspection
cover.
The
battery
through
their
switches
and
will
system
is
actuated
by
a
10
amp
circuit
breaker/switch
illuminate
without
the
Master
Switch
ON.
located
on
the
instrument
panel
in
front
of the
pilot
Navigation
lights
are
located
on
each
wing
tip
and
in
SM
251225
thru
25-1999
aircraft
may
have
optional
rudder
trailing
edge
(25-0001
thru
25-0999).
S/N
251000
switches
on
both
cabin
door
and
baggage
door
frames
thru
25-TEA
aircraft
have
the
aft
facing
navigation
ligM
that
tum
applicable
interior
lights
ON
when
either
door
(clear3
located
on
each
wing tip
trailing
edge.
The
ligMs
is
opened.
The
fo~ward
cabin
interior
lights
are
are
activated
by
a
7.5
amp
circuit
breaker/switch
located
connected
to
cabin
door
switch
and
the
aft
on
the
instrument
panel
in
of the
pilot
door
SWifCh.cabinlbaggage
inten~or
lights
are
connected
to
baggage
On
SM
25-0001
thru
25-1224,
landing
lights
are
Rocker
switches,
located
overhead,
between
pilot
and
located
in
lower
engine
cowling.
Two
110,000
candle
co-pnot,
for
cabin
interior
lights
will
tum
selected
set
of
power
sealed
beam
bulbs
are
incorporated
and
lights
ON,
as
desired.
The
rocker
switch
light
circuits are
mounted
in
a
housing
designed
to
isolate
the
bulbs
muted
through
a
timer
and
the
Master
Switch
and
will
go
from
engine
heat
and
vibration.
The
lights
are
activated
OFF
when
Master
Switch
is
tumed
Off,
with
the
rocker
amp
circuit
breaker/switch
located
on
the
switch(es)
left
ON.
panel
in
front
of
the
pilot.
The
lights
will
go
OFF
in
appro~dmately
90-120
seconds
ON
25-1225
thru
25-TEA, landingAa>a’
lights
ate
after
door(s)
are
closed
when
Master
is
OFF
and
mcker
located
in
leading
edge
of
each
wing.
Two
110,000
switch(es)
are
left
ON.
Lights
will
go
OFF
when
door(s)
candle
power
sealed
beam
bulbs are
located
in
each
is(are)
closed
(timer
delay)
if Master
Switch
is
ON
or
OFF
wing.
The
lights
are
activate
by
two
25
amp
split
,,d if
light
rockerswitch(es)
are
OFF.
switches
located
on
the
pilots
instrument
panel.
The
switches
are
use
to
illuminate
both
landing
and
taxi
or
The
light
timer
box
is
located on
firewall
diagonal
tube
either
one,
as
desired.
ahead
of
pilot’s
right
foot;
it
is
a
non-reparable
unit.
Two
sets
of
interior
lights
are
located
on
the
overhead
CAUTION
panel.
The
forward
cabin
overhead
lights
are
located
LIGHTS
WILL
STAY
"ON"
IF
DOORS
ARE
OPEN.
between
the
pilot
and
co-pilot
seats
and
are
actuated
by
a
three
position
switch,
(dim,
off,
bn’ght)
adjacent
to
LAMP
BULB
APPLICATIONS
BULB
PART
NUMBER
14
VOLT
28
VOLT
Glareshield
Lights
GE
330
GE327
Post
Lights
GE
330
GE
327
Map
Light
GE
330
GE
327
Cabin
Inten’or
Lights
GE
1816
GE
1818
Trim
8
Flap
Indicator
(S/N
25-0002
thru
25-0575)
Wl-7046
N/A
(S/N
250576
8
ON)
GE
370
GE
327
Gear
Down
Light
(Floorboard
Indicator)
GE
327
GE327
Tail
Position
Light
(S.D.I.)
32-0228030-85*
NIA
ONHELEN)
A508-14
W1290
Wing
iip
Position
Light
(GRIMES)
A-7512-12
Wt
290
Landing
Light
(GE)
GE
4509
GE
4596
Recognition
LightlBulb
Assy
OM-iELEN)
01-0770303-00
Same
(use
resistor)
Use
S.D.I.
Tool
No.
203541
to
remove
lamp.
33-20-00
INTER(OR
LIGHTS
MAINTENANCE
33-21-01
LIGHT
BULB
REPLACEMENT
PRACTICES
(25-0001
thru
25-1999)
33-21-00
-CABIN
LIGHTS
-OVERHEAD
LIGHTS
1.
Remove
the
light
cover
panel
(2)
(Figure
33-1)
from
the
headliner
assembly
(1)
by
removing
screws
(3).
33-00-00
OLDWILLWAYNE