Mooney M20M - Page 20

MOONEY
AIRCRAFT
CORPORATION
M20M
SERVICE
AND
MAINTENANCE MANUAL
F.
Inspect
oxygen
system
(tf
installed).
C. Drain
engine
oil
sump;
remove,
inspect
and
4.
Landing
Gear.
clean
oil
suction
screens;
reinstall
and
safety.
Remove
full-flow
oil
filter
cartridge;
replace
with
new
cartridge
A.
Inspect
´•tires for
cuts,
blisters,
wear,
and
proper
and
safety.
Inspect
crank
case
breather
lines for
inflation.
obstruction.
Safety
wire
oil filter
installation.
B.
Inspect
shock
discs
for
proper
extension
at
D.
Refill
engine
oil
sump
with
the
proper
type,
aircraft
static
weight.
grade,
and
quantity
of
lubricating
oil.
C.
Inspect hydraulic
brakes for
wear,
warpage
and
E.
Inspect
fuel
injector
and all
fuel
line connections
proper
installation.
for
security
and
condition.
5.
Wings.
F.
Remove and
inspect
gascolator
strainer,
A.
Inspect
surfaces
and
tips
for
damage.
reinstall
strainer.
Inspect
fuel lines
and
connections:
B.
pressure
check
fuel
system
with mixture control
at
Inspect
ailerons,
aileron
attachments,
and
IDLE
CUTOFF
and
BO~ST
PUMP
ON.
bellcranks
for
damage
and
proper
operation.
G.
Inspect
all
air
ducting
and connections
in the
C.
Inspect flaps
and attachments
for
damage
and
heating
and
induction
air
systems
for leaks.
Remove and
proper
operation.
clean
induction
air
filter
(replace
at
500
Hrs). Inspect
D.
Lubricate
controls
per
Section
5-20-07
if
altemate
air door
and
magnet
for
security
and
operation.
necessary,
Leak
check ail
exhaust
manifold
connections,
engine
6.
Fuselage
and
Empennage.
exhaust
manifolds.
Inspect
for
security.
A.
Inspect
stabilizer,
elevators,
fin,
and rudder for
H´•
I"spect magnetos
for
grounding
and
damage
and
proper
attachment.
synchronization;
Inspect magneto
points
for
condition,
clearance,
and
timing.
Inspect
distributor
block
for
B.
Lubricate
controls
per
Section
5-20-07
if
erosion
and cracks.
Inspect
cam
follower
felt for
proper
necessary.
lubrication,
and
remove
excessive
oil
from breaker
C.
Inspect
Trim
System
for
proper
operation.
compartment.
Inspect
magneto
pressurization
per
Slick
magneto
maintenance
manual.
Repair
or
replace
7. See
Section
5-20-07
for
any
repetitive
50
hour
components,
if
required.
inspections
and
component
service
guide.
I.
Inspect
baffles for
secure
anchorage,
cracks,
5-20-06
100-HOUR
or
ANNUAL
holes,
deformation,
and
for close
fit
around
cylinders.
INSPECTION
Inspect
cylinders
for
burned
paint
and
cracked
or
(Refer
to
Fig. 54)
broken
fins.
Inspect
baffle sealant.
The
100-hour
(or annual)
inspection
is
a
thorough,
J.
inspect
accessory
case,
starter,
aitemators,
vacuum
searching inspection
of
the entire
aircraft.
Preparation
pumps
hose,
firewall
and
fittings
for
security
or
damage.
for
the
inspection
includes
the
thorough
cleaning
of
K.
Inspect
turbocharger
for cracks
or
damage.
exterior
and
engine
compartment,
removal
of all
Inspect
turbocharger
control
components
for
obvious
fuselage,
wing,
and
empennage
inspection
doors,
damage.
Inspect
intercooler
for
damage
or
obstruction.
cover
plates,
and
fairings
at
all
systems
attach,
hinge,
and
bearing
locations
(including
wing
and
empennage
L.
Inspect
tubular
engine
mount
for
cracks,
to
fuselage
mating
points).
Operating
limit
replacement
damage
or
corrosion;
check
all bolts
and
rubber
(See
Section
5-10-01)
and
special
testing
of
isolation
mounts
for
security
and
condition.
components
is
to
be
included
at
this interval
when
M.
inspect engine
and
propeller
controls
for
free
applicable.
Comply
with
applicable
FAA
Directives,
AD
operation,
full
travel,
proper
connection
(security)
of
Notes,
and
applicable
Mooney
or
Vendor
mandatory
cable
housing
swage
at
the
HEAD tube and
security
of
Service
Bulletins
and
Instrudions.
Check
for
aircraft
attachment.
conformance
to
FAA
Specification
2A3.
NOTE
Recommended
100-hour/annual
and
special
inspection
Cablecraft control
cables
are
lubricated
for
the
requirements
are
outlined
in
the
following
paragraphs:
life
of
the
control cable. DO
NOT
REMOVE seals
1.
ENGINE
INSPECTION.
Prior
to
the
inspection,
or
lubricate
control
cable.
remove
the
engine
cowling
and
propeller
spinner.
N.
Inspect
enaine
fuel
pump
pressure.
(See
Wash
down
the
engine
and
engine
compartment.
Then
Textron-Lycoming
Service
information
and
Section
perform
an
engine
runup
in
accord
with the
procedure
71-00-50
for
this
procedure).
recommended
in
the
Engine
Maintenance and
Operators
Manual.
To
verify
correction
of
malfunctions
O.
Inspect
and
reinstall
cowling.
Check cowl
flap’s
and
abnormalities,
perform
a
second
runup
and
flight
for
operation,
condition,
proper
opening
and
position
test
after
the
100-hour/annual
inspection
engine
indication.
set-up.
P.
Inspect
battery
cables,
electrical
wiring,
and
A.
Complete
a
differential
(hot
engine)
ignition
harness
for
condition,
secure
anchorage,
loose
compression
check:
clean
and
gap
or
replace spark
tenninals,
and burned
or
chaffed insulation.
plugs
if
necessary.
Q.
Inspect
batteries,
battery
mount
areas,
and
vent
B.
Inspect
engine
for evidence
of
excessive
fuel
or
system
for
condition and
corrosion.
Inspect
blast tube
oil
leakage.
Inspect
oil cooler.
Inspect
oil fuel
hoses
for obstruction.
Flush
battery
mount
areas
with
soda
for
condition
security. Repair
as
required.
solution
to
neutralize
corrosive action
if
necessary.
5-20-06
4-99
12
OLDWILLWAYNE