Mooney M20K - Page 27

SERVICE
AND
MAINTENANCE
MANUAL
M20K
MOONC/
AIRCRAFT
CORPORATION
movement
of
toe-brake
pedals
and
proper
rudder
and
freedom,
and
syncronization
of
barometric
scale
with
nose
wheel
travel.
reference
markers.
E.
Inspect
stabilizer
tn’m
control
system
for
security
G.
inspect
flight
panel
for
security
of
mounting,
and
proper
adjustment,
shaft
and
stop
nuts
for
proper
condition
of
shock
mounts,
freedom
from
interference
rigging,
trim
control
wheel
for
smooth
operation,
with
structure,
and
condition
of
ground
straps.
universal
joints
for
free-play
and
good
working
order,
H.
Inspect
Avionics
Euipment
for
proper
operation
actuator
threads
for
lubrication,
linkage
for
corosion,
g,,,urity.
and
guide
blocks
for
looseness or
excessive
wear.
I.
Inspect
Avionics
Antennas,
wiring
6
shielding
for
F.
Inspect
flap
system
for
rigging,
travel,
and
stop
obvious
damage
or
defects.
adjustment;
flap
tubes,
interconnects,
bellcranks
8
hinges
for
corrosion,
security,
and
lubn‘cation.
J.
inspect
pitot
head
for
port
obstruction;
Inspect
lines
for
cracks,
dents,
kinks,
proper
bend
radius,
and
security
NOTE
of attachment.
Drain
system
and
check
for
leaks.
All
control
rigging
checks
should
be
made
with
for
obstruction
and
the
aircraft
jacked
and leveled
and
with
the
K.
inspect
static
ports
landing
gear
retracted,
aerodynamic
smoothness
at
port
installations.
Inspect
NOTE
lines for
bends,
cracks,
dents,
kinks,
and
security
of
Some
elevator
trim
tubes
have
poly
tape
attachment.
Drain
system
and
check
for
leaks.
Inspect
wrapped
at
bulkhead
penetrations.
If
tape
aitemate
static
pressure
source
located
on
left
flight
shows
signs
of
wear, rerap
(1/2
lap)
tube
with
pa"el.
2"
wide
Y9265
polyurethane
tape.
Trim
tubes,
10.
ELECTRICAL
FUNCTIONAL
TEST.
vvithout
tape,
which
show
signs
of
abrading
A.
Check
operation
of
navigation
lights.
grommet
should
be
wrapped.
See
SE
M20-185.
B.
Check
operation
of
landing
lights.
MAX.
TUBE
WEAR
.007
in,
per
wall
or
.014
in.
diameter
reduction.
C.
Check
operation
of
dome
lights
and
cigar
lighter.
Inspect
Speedbrake
Cartn~dge
every
1000
hours
per
D´•
Check
operation
of
anticollision
lights.
the
following:
E.
Check
operation
of
instrument
and
placard
G.
Remove
Speedbrake
Cartn’dge
from
access
lights.
Check meostat.
cover
beneath
LH
6 RH
side
ofwing.
F.
Check
operation
of
pitot
head
heater.
1.
Visually
Inspect
doubler
and
mounting
G.
Check
operation
of
cluster
gauge.
hardware
for
structrual
integrity.
H.
Check
operation
of
fuel
gauges.
2.
Visually
Inspect
for
chafing
on
all
moving parts.
I.
Check
operation
of
annunciator
light press-to-test
3.
Manually operatae
speedbrake
doors
an
feel
switch.
forsmooth
operation.
J.
Check
operation
of
ignition
switch,
and
starter
4.
Inspect
cable
ton
Vacuum
Units)
expecially
solenoid.
around
pulleys
for
fraying.
K.
Flight
check
operation
of
landing
gear
position
H.
Report
any
deficjences
Cdany)
to
Precise
FliSM,
Inc.
lights
and
warning
hem.
I.
Relnstall
Speedbrake
Cartn’dges
through
access
L.
Flight
check
operation
of
stall
warning
hem.
panels
in
bottom
of
LH
8
RH
side of
wing.
M.
Check
operation
of
"Prop
De-ice"
(if
installed).
9.
INSTRUMENT/
AVIONICS
INSPECTION.
Push
switch
"ON",
observe
prop
de-ice
ammeter
for:
A.
Inspect
all
instrument
win’ng
and
plumbing
for
(1)
needle
in
green
are
(8
to
12
amps),
and
(2)
condition
and
proper
connections.
fluctuation
every
90
seconds
as
heating
elements are
switched.
(S/N
25-0001
thru
25-0999).
Observe
ship
B.
Clean
and
inspect
vacuum
filter.
Replace
garter
ammeter
on
S/N 251000
thru
25TBA
for
a
flicker
as
filter
on
vacuum
regulator.
each
blade
boot
cycles.
C.
inspect
vacuum
regulator
at
vacuum
manifold.
N.
Inspect
battery
8
battery
connection
for
proper
Check
ope~ation
of
high-and
low-vacuum
waming
lights
installation
and
cleanliness.
or vacuum
gage.
11.
MISCELLANEOUSIOPnONAL
EQUIPMENT
D.
Inspect
all
instruments
for
proper
pointer
indication,
range
and
limit
markings,
condition
of
A.
Inspect
any
installed
equipment
not
covered
by
indicator
markings,
cracked
or
loose
glass,
slippage
previous
paragraphs
for
proper
operation,
attachment
marks,
and
security
of
installation.
and
obvious
defects.
E.
Inspect
compass
for
proper
lighting,
12.
POST
INSPECTION
FUGHT
TEST..
Flight
test
compensation,
security
of
mounting,
liquid
leakage,
and the
aircraft
to
ven’fy
correction
of
all
malfunctions
and
discoloration.
Swing
compass
at
annual
inspection
and
abnormalities.
Make
proper
entn’es
in
aircraft
log
book.
after
any
new
equipment
has
geen
installed.
Wing
access
covers
may vaiy
to
some
degree
between
F.
Inspect
altimeter
for
scale
error,
discolored
model
year
aircraft.
markings,
proper
pointer
readings,
setting
knob
Component
locations
remain
basically
unchanged.
5-20-06
16
OLDWILLWAYNE