Mooney M20M - Page 21

SERVICE
AND
MAINTENANCE
MANUAL
M20M
MOONEY
AIRCRAFT
CORPORATION
R.
Inspect
exhaust
system
for
cracks,
looseness
and
J.
Inspect
nose
wheel
steering
mechanism
for
for
evidence
of
leakage.
Replace
or
repair
damaged
adjustment,
alignment,
corrosion,
and
lubrication.
components.
Reference
(G)
50
hour
inspection.
K.
Inspect
main
gear
for cleanliness
and
damage.
S.
Inspect
exhaust
stacks
for
burned
areas,
cracks,
L.
Inspect
landing
gear
retraction
linkage,
bdlcranks,
distortion
and
looseness.
pivots,
and
bearings
for
wear,
damage,
distortion,
T.
Inspect
exhaust
couplings,
seals,
clamps
and
misalignment,
corrosion,
cleanliness,
and
lubrication.
slip-joints
for
cracks,
deformation,
leaks
and
security.
M.
Inspect
landing
gear
actuator
for
security
of
U.
Inspect
studs,
nuts,
bolts,
etc.
for
damage
and
mounting,
deanliness,and
indication
of
overheating,
proper
torque.
damage,
and
operation.
Inspect
motor
brushes
for
wear.
V.
Inspect
re-install
cowling.
Check
cowl
flaps
for
N.
Perform
landing
gear
operational
Inspection
per
proper
operation,
condition
and
proper
position
indication.
Section
32-30-01.
2.
PROPELLER
INSPECTION.
4.
FUEL
SYSTEM
INSPECTION.
A. Remove
spinner
(if
not
already
removed).
A.
Inspect
fuel
tank
exterior
for evidence
of
fuel
B.
Inspect
security
of
propeller
installation.
seepage
or
stain.
8.
Drain
tank and
inspect
tank
interior
when
C.
Inspect
hub
bolts
for
proper
torque
(61-00-20)
seepage
is
evident.
security
and
damage.
D.
Inspect
hub
components
for
damage
or
leaks
and
C.
Inspect
fuel
tank
drains
for
leakage,
sediment,
or
water
contamination.
blades
for cracks and
nicks.
Repair prior
to
next
flight.
D.
Inspect
fuel-tank
vents
for obstruction.
E.
Inspect
Anti-ice
boots
for
security
and
operation.
F.
Inspect
spinner
and
bulkhead
for
cracks
and
E.
Inspect
fuel selector
valve
for
proper
tank
smooth
operation,
or
any
leakage
when
in
OFF
position.
G.
Inspect spinner
bulkhead
for
snug
fit be~veen
F.
Inspect gascolator
for
leakage;
check
sump
for
propeller
cylinder
spinner
support.
Use
shims
as
sediment,
water
or
other
contamination.
necessary
to
obtain
correct
snug
frt.
3.
LANDING
GEAR
and
RETRACTION
SYSTEM
G.
Inspect
electric
boost
pump
for
leaks,
security
of
INSPECTION.
mounting,
adequate
fuel
pressure,
switch
operation,
and
condition
of
wiring
and
electrical
connections.
A.
Inspect
tires
for
proper
inflation,
cuts,
blisters,
electric
boost
pump
for
proper
slippage,
and
excessive
wear.
Replace
with
new,
(1) Inspect
operation
by
"T
ing"
into
the line
with
a
calibrated
fuel
approved,
tire
if
necessary.
pressure
gauge.
Boost
operation
should
result
in
a
45-
CAUTION
55
P.S.I.
reading
(mixture
full
RICH,
throttle-IDLE).
Always
run
at
least
5
Landing
Gear
Retraction
(2) Adjust
relief
setting
on
pump
if
needed.
Cycle
checks
after
any
tire
has
been
removed
H.
Inspect
fuel
quantity
gauges
and
transmitters
for
and/or
replaced
before
flying
the
aircraft.
security
of
mounting
and
condition
of
wiring
and
B.
Inspect
wheels
for
cracks,
distortion,
electrical
connections.
misalignment,
corrosion
or
bolt
failure.
Inspect
I.
Inspect
fuel tank
filler
port
for
cleanliness,
cap
condition
of felt seals
and
bearings;
repack
bearings
at
security,
and condition
of
servicing
placards.
Inspect
250
hour
intervals,
fuel
filler
cap
O’rings
for
condition
and
replace
if
C.
Inspect
brake
pads
discs
for
warpage
or wear
needed
(Reference
SECTION
23-00-01).
(Ref.
Section
32-40-04).
5.
EXTERIOR
INSPECTION.
D.
Inspect
hydraulic
reservoir
for
proper
fluid level.
A.
Inspect
fuselage
exterior
surfaces
for
corrosion,
E.
Inspect
hydraulic
brake
lines
and hoses
for
damage,
loose
or
popped
rivets,
dents,
leakage,
dents,
cracks
chafing,
kinks,
and
security.
oilcans(stretched
skins),
scratches,
cracks,
or
deteriorated
paint.
F.
~lnspect
parking
brake
system
for
proper
engagement
and
release.
8.
Inspect
windshields
and
windows
for
cracks,
crazing,
scratches,
condition
of
sealant,
and
security
of
G.
Check
shock
disc
gap
on
main
6
nose
landing
installation.
gear.
(See
32-81-00)
C.
Inspect
wings,
flaps,
and
ailerons
for
corrosion,
H.
Conduct
Hard/Overweight
Landing
Inspection
damage,
loose
or
popped
rivets,
dents,
scratches,
per
SECTION
32-32-00.
cracks,
condition
of
attaching
points,
lubrication,
Jack
aircraft
as
recommended
in
paragraph
7-10-00
for freedom
of
operation,
free-play,
travel,
and
balance
the
following
inspections:.
weight
attachment.
Inspect
speedbrake
cartridges
for
I.
Inspect
nose
gear
for
cleanliness
and
damage.
damage
or
wear.
Check
for
proper
operation.
Every
200
Check
nose
gear
retraction
tube
bungees
for sheared
hours
remove
speedbrake
cartridges
per
27-96-01.
or
broken
roll
pins.
D.
Inspect
empennage
for
corrosion,
damage,
loose
or
popped
rCvets,
free-play,
dents,
scratches,
NOTE
cracks,
condition
and
lubrication
of
hinge
points,
Maximum
allowable
towing
damage
on
leg
attachment
of
balance
weights,
and
freedom
of
assembly
is
1/32
inch
dent.
No
repair
allowed
operation,
manually
and
electrically.
on
heat
treated
landing
gear
components
4-99
5-20-06
13
OLDWILLWAYNE