Mooney M20K - Page 26

MOONEY
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
D.
Inspect
fuel-tank
vents
for
obstruction.
6.
INTERIOR
INSPECTION.
E.
Check
fuel selector
valve
for
proper
tank
selection,
A.
Inspect
seats,
seat
t~acks,
and
upholstery
for
smooth
operation,
and
leakage
in
OFF
position.
cleanliness
and
mounting
security;
check
seats
for
condition
and
operation
of
position
locks;
inspect
seat
F.
Inspect
gascolator
for
leakage;
check
sump
for
structure
for
c~acks,
deformation,
corrosion,
and
sediment,
water
or
other
contamination.
mechanism
lubrication.
G.
Inspect
boost
pump
for
leaks,
security
of
B.
inspect
safety
bets,
harnesses,
and
att~fiing
bad(ets
for
mounting,
adequate
fuel
pressure,
switch
operation,
deanhess, operation,
and
securi~j
dbdac~hment
and
condition
of
wiring
and
electrical
connections.
C.
Inspect
for
loose
equipment
that
might
restn’ct
(1)
Check
eledn’e
fuel
boost
pump
for
proper
controlmovement.
operation
by’T’
ing
into
the line
with
a
calibrated
fuel
D.
Inspect
Oxygen system
ginstaCed3.
Referto
Chapeer35.
pressure
gauge.
(a)
High
boost
operation
should
result
in
a
23.5
7-
INTERNAL
INsPECT1ON.
to
24.5
P.S.I.
reading (mixture
full
RICH,
throttle-IDLE).
A.
Open
access
panels
and
inspection
doors,
and
(b)
Low
Boost
pump
pressure
check
6-8
P.S.I.
’emove
fain’ngs
as
required.
See
Se~lon
24-37-00
for
adjustment
procedures.
B.
Inspect
wing
attaching
bolts
for
proper~torque
H.
Inspect
fuel
quantity gages
and
transmitters
for
and
safetying
and evidence
of
damage
or
corrosion.
secun’ty
of
mounting
and
condition
of
win’ng
and
C.
Inspect
forward
side
of
firewall for
damage.
electrical
connections.
D.
Inspect
tubular
structure
for
corrosion
or
I.
Inspect
fuel
tank filler
port
for
cleanliness,
cap
damage
(interior
panels
may
require
removal).
secun’ty,
and
condition
of
servicing
placards.
Inspect
Reference
Mooney
Service
Bulletin
M20-2088
or
cap
O’n’ngs
for
condition
and
replace
if needed.
subsequent
revisions.
5.
EXTERIOR
INSPECTION.
E.
inspect
wing
n’bs
and
stringers
for
cracks
and
evidence
of
damage
or
corrosion.
A.
Thoroughly
clean aircraft
e>derior
F.
hsped~ng
spanrw~m;ge,
cCsbrtig
aacks,
orcarosicn
B.
Inspect
fuselage
exten’or
surfaces
for
corrosion,
damage,
loose
or
popped
rivets,
dents,
cans,
G.
Inspect
wires,
lines,
and ducts
for
security,
scratches,
cracks,
and
deten’orated
paint.
damage,
interference,
chaffing,
and
bonding.
C.
Inspect
windshields
and
windows
for
cracks,
NOTE
crazing,
scratches,
condition
of
seals,
and
security
of
Seal
all
receptacles
and
plugs
outside
cabin
installation,
environment
with
Dow
Coming
#4.
D.
Inspect
wings, flaps,
and
ailerons
for
corrosion,
H.
Inspect wing
inten’or
for
foreign
material,
damage,
loose
or
popped
rivets,
dents,
scratches,
corrosion,
and
evidence
of
fuel
leakage.
cracks,
condition
of
attaching
points,
lubn’cation,
i.
Inspect
empennage
attachment
brackets
and
freedom
of
operation,
free-play,
travel,
and balance
hardware
for corrosion.
weight
attachment
J.
Inspect
empennage
attaching
brackets
and
E.
Inspect
speedbrake
cartridges
for
damage
and
hardware
for
corrosion.
wear.
Check
for
proper
operation.
Every
1000
hour
inspections
see
27-96-02.
8.
FLIGHT
CONTROL
INSPECTION.
F.
Inspect
empennage
for
corrosion,
damage,
loose
A.
Inspect
control
column
and
control
wheels
for
or
popped
rivets,
ftee-playt
dents,
scratches,
cracks,
full
travel,
proper
rigging,
free-play,
binding,
security
of
condition
and
lubrication
of
hinge points,
attachment
of
mounting,
proper
lubrication,
and
direction
of
control
balance
weights,
and freedom
of
operation.
surface movement
with
relation
to
control
movement.
G.
Inspect
cabin
door
and door
frames
for
damage,
CAUTION
corrosion,
nicks,
dents,
hinge
security,
and
lubn’cation.
All
flight
control
components
should
be
H.
Inspect
cabin
door
lock
mechanism
for
inspected
to
verify
that
all
moisture
drain
holes
are
free
of
obstructions.
lubn’cation
and
proper
engagement.
See
Section
52-11-00
for
rigging
procedures.
8.
Inspect
elevator
system
for
rigging,
travel,
stop
I.
Inspect
the
baggage
door
and
baggage
adjustment,
condition
of
bearings,
bellcranks,
and
hinges,
compartment
for
damage,
corrosion,
warpage,
hinge
wear
on
downspn‘ng
eyes,
cable
pulley
and
frttings,
secun’ty,
condition to
door
frame
and
door
seals,
Security
of
mounti~g,
damage,
corrosion,
proper
condition
and
operation
of
door
locking
mechanism,
lubn’cation
and
proper
relation
to
control
movement.
and
condition
of
cargo
tiedowns.
C.
Inspect
aileron
system
for
damage,
corrosion,
J.
Inspect
ventilating
system
drain
line
for
lubn’cation,
rigging,
travel,
stop
adjustment,
condition
of
bellcranks
8
hinges,
pivots
and
rod
end
bean’ngs,
and
obstruction.
link bolt
security.
K.
Inspect
landing
and
taxi
lights
for
security,
D.
Inspect
rudder
system
for
damage,
corrosion,
condition
and
proper
adjustment.
See
Section
33-43-00
lubrication,rigging,
condition
of
hinges,
bellcranks,
for
adjustment
procedures,
security
of link
bolts,
rod
end
bean’ngs,
and
proper
relationship
to
control
movement.
Check
for
free
5´•20-06
15
OLDWILLWAYNE