Mooney M20M - Page 22

MOONEY AIRCRAFT
CORPORATION
M20M SERVICE
AND
MAINTENANCE MANUAL
E.
Inspect
cabin
door
and door frames
for
damage,
H.
Inspect wing
interior
for
foreign
material,
corrosion,
nicks, dents,
hinge
security,
and lubrication.
corrosion,
and/or
evidence of
fuel
leakage.
F.
Inspect
cabin
door
lock mechanism
for
I.
Inspect
empennage
attachment
brackets
8
lubrication
and
proper
engagement.
See Section
hardware
for
corrosion.
52-11-00
for
rigging procedures.
8.
FLIGHT CONTROL INSPECTION.
G.
Inspect
the
baggage
door and
baggage
A.
Inspect
control column
and
control
wheels
for
compartment
for
damage,
corrosion,
warpage,
hinge
full
travel,
proper
rigging, free-play, binding,
security
of
security,
condition
to
door
frame
and door
seals,
mounting,
proper
lubrication,
and
direction of
control
condition and
operation
of
door
locking
mechanism,
surface
movement
with
relation
to
control
wheel
and condition of
cargo
restraints/tiedowns.
movement.
H.
Inspect
ventilating
system
drain line for obstruction.
CAUTION
I.
Inspect
landing
and
taxi
Tights
for
security,
All
flight
control
components
should be
condition and
proper
adjustment.
See Section
checked
to
verify
that all
moisture
drain
holes
33-43-00
for
adjustment
procedures.
are
free
of
obstructions.
J.
Inspect
Decals
8 Placards
for
condition and
B.
Inspect
elevator
system
for
rigging,
travel,
stop
proper
location.
adjustment,
condition
of
all
bearings,
bellcranks,
K. LIGHTNING
STRIKE INSPECT FOR:
hinges;
wear on
downspring
eyes,
cable
pulley
and
(1)
Seized
Bearings Engine
and
Airframe
fittings,
security
of
mounting,
damage,
corrosion,
(2)
Failed
Electronics
Radios, Instruments,
etc.
proper
lubrication
and
proper
relation
to
control
(3)
Bumed
(melted) Metal-trailing edges,antennas,
etc.
movement.
(4)
Burned
Wiring--throughout
aircraft
C.
Inspect
aileron
system
for
damage,
corrosion,
(5)
Burned marks
on
Propeller--Leading edges,
tips
iubrioation,
rigging,
travel,
stop
adjustment,
condition
of
6.
INTERIOR INSPECTION.
hinges,
bellcranks,
pivots
and rod
end
bearings,
and
A.
Inspect
seats,
seat
tracks,
and
upholstery
for
Ilin~
bolt
security.
cleanliness and
mounting
security;
check seats
for
D.
Inspect
rudder
system
for
damage,
corrosion,
condition
and
operation
of
position
locks;
inspect
seat
lubrication,
security
of
link
bolts,
rod
endbearings
and
structure
for
cracks,
deformation,
corrosion,
and
hinges;
check for
free
movement
of toe-brake
pedals
mechanism
lubrication,
and
proper
rudder
and
nose
wheel travel.
8.
Inspect
safety
belts,
hamesses and
attaching
E.
Inspect
stabilizer
~trim control
system
for
security
and
brackets
for
cleanliness, condition,
latch
operation,
and
proper
adjustment,
shaft and
stop
nuts
for
proper
rigging,
security
of
attachment. trim
coc~ol
wheel
for smooth
operzrtion, u-joints
for
freeplay
C.
Inspect
for
loose
equipment
that
might
restrict
and
good
working
order,
ac~ator
threads
for
lubrication,
controlmovement.
linkage
for
corrosion,
and
guide
blocks
for
looseness
or
excessive
wear.
See Section
27-42-00
for
inspection
D.
Inspect
Oxygen system
per
SECTION
35.
lubrication
of
bearing
block
for
pitch
trim
system.
E.
Inspect
Decals
8
Placards
for
condition
and
F.
Inspect flap
system
for
rigging,
travel,
and
stop
proper
location.
adjustment; flap
rods,
interconnects,
bellcranks
and
7.
INTERNAL INSPECTION. hinges
for
corrosion,
security,
and
lubrication.
A.
Open
access
panels
and
inspection
doors,
and
NOTE
remove
fairings
as
required.
All
control
rigging
checks
should
be
made
with
B.
Inspect
fuselage~uing attaching
bolts
for
proper
the aircraft
jacked
and
leveled
and with the
torque
and
sadetying
and evidence
of
damage
or
corrosion
(interior
side
panels
will
require
removal
to
accomplish
~tl7is
inspection).
Some
elevator
trim
tubes
have
poly
tape
wrapped
at
bulkhead
penetrations.
If
tape
C.
Inspect
forward side
of
firewall
for
damage.
shows
signs
of
wear,
rewrap
(1/2
lap)
tube
with
D.
Inspect
tubular
structure
for
corrosion
or
2"
wide Y9265
polyurethane
tape.
Trim
tubes,
damage
(interior
side
panels
will
require
removal).
without
tape,
which
show
signs
of
abrading
(Reference
Mooney
Service
Bulletin M20-208A
(or
grommet
should be
wrapped.
See
SE
M20-185.
current
revision)
forspecific
procedures) (annually).
MAX. TUBE
WEAR-.007
in.
wall
thickness
or
.014 in.
E.
Inspect
wing
ribs
and
stringers
for cracks
and
diameter
reduction.
evidence of
damage
or
corrosion.
9.
INSTRUMENT/AVIONICS
INSPECTION.
F.
Inspect
wing
spars
for
damage,
distortion,
A.
Inspect
all
instrument
wiring
and
plumbing
for
cracks,
or
corrosion.
condition
and
proper
connections.
G.
inspect
electrical
wiring,
fuel,
oil
and
hydraulic
B.
Clean
and
inspect
vacuum
filter.
Replace
garter
lines,
and
air
ducts
for
security,
damage,
interf~erence,
filter
on
vacuum
regulator.
chaffing,
or
de-bonding.
C.
Inspect
vacuum
regulator
at
vacuum
manifold.
NOTE
Check
operation
of
high-and
low-vacuum
waming
Seal
all
receptacles
and
plugs
outside cabin
lights
or
vacuum
gage.
Inspect
Stand-by
vacum
environment with Dow
Coming
#4.
System
per
Section
37-40-00.
5-20-06 4-99
OLDWILLWAYNE