Mooney M20K - Page 24

MOONEY
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
4.
Landing
Gear.
E.
Inspect
fuel
injector
and all
fuel
line
connections
for
security
and
condition.
A.
Inspect
tires
for
cuts,
blisters,
wear,
and
inflation.
F.
Remove,
inspect
and clean
gascolator
strainer,
reinstall
strainer.
Inspect
fuel
lines
and
connections:
B.
Inspect
shock
discs
for
proper
e>dension
at
pressure
check fuel
system
with
mi~dure
control
at
IDLE
aircraft
static
weight
per
Section
32-81-00.
CUTOFF
and
BOOST
PUMP
ON.
C.
Inspect
hydraulic
brakes
for
wear,
warpage
and
G.
Inspect
all
air
ducting
and
connections
in
the
proper
installation.
heating
and
induction
air
systems
for
leaks.
Remove
5.
Wings.
and clean
induction
air
filter
(replace
at
500
Hrs).
Leak
check
all
exhaust
manifold
connections,
engine
A.
Inspect
surfaces
and
tips
for
damage,
exhaust
manifolds
and
resonator
connections
(if
ailerons,
aileron
attachments,
and
equipped).
Inspect
turbochalger
housing
per
TCM
SE
damage
and
proper
operation.
C.
Inspect
flaps
and
attachments
for
damage
and
H´•
Inspect
altemate
air
door
and
magnet
for
proper
operation.
security
and
operation.
D.
Lubncate
controls
if
necessa~y.
i.
Check
magnetos
for
grounding
and
synchronization;
inspect
magneto
points
for
condition,
6.
Fuselage
and
Empennage.
cle~rance,
and
timing.
Inspect
distributor
block
for
A.
Inspect
stabilizer,
elevators,
fin,
and
rudder
for
erosion
and
cracks.
inspect
cam
follower
felt for
proper
damage
and
proper
attachment,
lubrication,
and
remove
excessive
oil from
breaker
compartment.
Inspect
magneto
pressurization.
Repair
B.
Lubn’cate
controls
if
necessary,
or
replace
components,if
required,
per
Bendix
SE
No.
7.
See
Section
5-20-07
for
any
repetitive
50
HOUF
612
500
hrs)
and
Slick
SL
1-84.
Inspections
and/or
Component
Senn’ce
Guide.
J.
Inspect
baffles
for
secure
anchorage,
cracks,
holes,
deformation,
and
for close
fn
around
cylinders.
5-20-06
-´•100-HOURiNSPECTION
(orANNUAL)
Inspect
cylinders
for
burned
paint
and
cracked
or
(Refer
to
Fig.
5-4)
broken
fins.
Inspect
baffle
sealant.
The
100-hour
(or
annual)
inspection
is
a
thorough,
K.
Check
engine
and
propeller
controls
for
free
searching
inspection
of the
entire
aircraft.
Preparation
operation,
proper
lubrication,
full
travel,
proper
for
the
inspection
includes
the
thorough
cleaning
of
connection
(security)
of cable
housing swage
at
head
aircraft
exten’or
and
engine
compartment,
removal
of
tube and
security
of
attachment.
fuselage,
wing,
and
empennage
inspection
doors,
cover
plates,
and
fain’ngs
at
all
systems
attach,
hinge,
NOTE
and
bean’ng
locations
(including
wing
and
empennage
Cablecraft
control
cables are
lubricated
for
life
to
fuselage
mating
points).
Operating
limit
replacement
of
control
cable.
DO
NOT
remove
seals
or
and
special
testing
of
components
is
to
be
included
at
lubricate
control
cable.
this
interval
when
applicable.
Comply
with
applicable
mount
for
cracks,
FAA
Directives,
AD
Notes,
and
applicable
Mooney
and
L.
Inspect
tubular
engine
Vendor
mandatory
Service
Bulletins
and
Instructions.
corrosion;
inspect
all
bolts
and
rubber
mounts
for
Check
for
aircraft
conformance
to
FAA
Specification
security
and
condition.
2A3.
Recommended
100-hour
and
special
inspection
M.
inspect
battery
cables,
electrical
win’ng,
and
requirements
are
outlined
in
the
following
paragraphs.
ignition
harness
for
condition,
secure
anchorage,
loose
1.
ENGINE
INSPECTION.
Prior
to
the
inspection,
terminals,
and
bumed
or
chaffed
insulation.
remove
the
engine
cowling
and
propeller
spinner.
Wash
N.
Check
engine
fuel
pump
pressure.
(See
T.C.M.
do~nm
the
engine
and
engine
compartment.
Then
perform
Service
info.
and
Section
71-00-50
for
this
procedure).
an
engine runup
In
accord
with
the
procedure
recommended
in
the
TCM
Maintenance
and
Operators
O.
inspect
battery,
battery
box
area,
and vent
system
Manual,
Section
VIII. To
verify
correction
of
ma~fundions
for
condition,
corrosion.
inspect
Mast
tube
for
obstruction.
and
abnormalaies,
perform
a
second
runup
and
fight
test
Flush
battery
box
and
battery
case
with
soda
if
necessary.
after
the
1GO-hour
inspection
engine
set-up.
P.
Inspect
accessory
case,
starter,
altemator,
A.
Complete
a
differential
(hot
engine)
compression
standby generator
(if
installed)
(SM
25-0001
thru
check:
clean
and
gap
or
rep)acespark
plugs
if
necessary.
25-0999)
or
No.
2
altemator
(25-1000
and
ON
,if
installed),
vacuum
pump,
hose,
firewall
and
frttings
for
B.
Inspect
engine
for
evidence
of
excessive
fuel
or
security
or
damage.
oil
leakage.
Inspect
oil
cooler.
Inspect
oil
3
fuel
hoses
Q.
Inspect
for
condition
per
T~C.M.
Service
for
condition
3
security.
Bulletin
No.M833
orlaterinformation
(Ref.AD
82-07-03).
C.
Drain
engine
oil
sump;
remove,
inspect,
g
dean
R~
Inspect
turi~charger
control
components
for
oil
suction
screens;
reinstall
and
safety.
Remove
damage
and
condition.
full-flow
oil filter
cartridge; replace
with
new
cartridge
and
safety,
inspect
crank
case
breather
lines
for S.
inspect
intercooler
for
damage
or
obstrudions.
obstruction.
Safety
wire
oil filter
installation.
T.
inspect
exhaust
system
for
cracks,
looseness
D.
Refill
engine
oil
sump
with
the
proper
type,
and
for
evidence
of
leakage.
Replace
or
repair
grade,
and
quantity
of
lubn’cating
oil,
damaged
components.
5-20-06
13
OLDWILLWAYNE