Mooney M20R - Electrical Functional Test; Flight Control Inspection; Instrument;Avionics Inspection; Internal Inspection

MOONEY
AIRCRAFT
CORPORATION
M20R
SERVICE
AND
MAINTENANCE
MANUAL
C.
Inspect
for
loose
equipment,
etc,
that
n~igM
F.
Check
flap
system
for
rigging
actuator,
push/pull
restrict
control movements.
tubes for
rigging,
travel,
and
stop
adjustment.
Check
D.
Inspect Oxygen
system
(if
installed)
per
CHAP~ER
flap
posnion
indicator
for
proper
operation.
Inspect
35
of
this
S
M
manual.
actuator,
push-pull
tubes,
flap
rods,
interconnects,
I
E.
Inspect
interior
Decals/Placards
for
security,
bellcranks
and
hinges
for
corrosion,
security,
and
7.
INTERNAL
INSPECTION.
A.
Open
inspection
doors
and
remove acCess
NOTE
panels
and
fairings
as
required.
All
control
rigging
inspections
should
be
made
B.
Inspect
wing
attaching
bolts
for
proper
tot~ue
with the
aircraftjacked
and
leveled
(Per
Section
and
safetying,
and
evidence
of
damage
and
corro/sion
7)
and
landing
gear
retracted.
(interior
ABS side
panels/carpet
will
require
remov’al
to
adequately
accomplish
this
inspection).
NOTE
C.
Inspect
forward
side of
firewall
for
damage.
Some
elevator trim
tubes have
poly
tape
D.
Inspect
tubular
structure
for
corrosioniand
wrapped
at
bulkhead
penetrations.
lftape
damage
(interior
side
panels
will
require
remo~val),
shows;
signs
of
wear,
re-wrap
tube
with
2"
wide
I
(Reference
Mooney
Service
Bulletin M20-208Ai
for
V9265
polyurethane
tape
(1/2
tape
overlap).
specific procedures
required
annually).
Trim
tubes,
without
tape,
which
show
signs
of
E.
inspect
wing
ribs and
stringers
for
cracksiand
abrading
bulkhead
grommet
should be
evidence
of
damage
and corrosion.
wrapped.
See
SE
M20-185.
F.
Inspect wing
spars
for
damage,
distortion,
cracks,
and
corrosion.
MAX.
TUBE
V\fiAR-.00’1
in. wall thickness
or.014
in.
G.
Inspect
electrical
wiring,
fuel,
oil
and
hydraulic
diameter reduction.
lines
and air ducts for
security,
damage,
interferehce
9.
INSTRUMENTIAVIONICS
INSPECTION.
chaffing
and
de-bonding.
A.
Inspect
all instrument
wiring
and
plumbing
for
I
condition
and
proper
connections.
NOTE
B.
Clean
and
inspect
vacuum
finer.
Replace garter
Seal ah
receptacles
and
plugs
outside
cabir)
filter
on
vacuum
regulator.
environment
with Dow
Coming
#4.
C.
Inspect
vacuum
regulator
at
vacuum
manifold.
H.
inspect
wing
interior
for
foreign
mat$rial,
Check
operation
of
high-and
low-vacuum
warning
corrosion,
and evidence
of fuel
leakage.
lights
or
vacuum
gage.
Inspect
Stand-by
Vacuum
I.
Inspect
empennage
attachment brackets
´•and
System
(Ref.
Section
37-40-00)
hardware
for
corrosion.
D.
Inspect
all
instruments
for
proper
pointer
8.
FLIGHT
CONTROL
INSPECTION.
indication,
range
and
limit
markings,
condition of
A.
Inspect
control
column
and control
wheels
for
full
indicator
markings,
cracked
or
loose
glass,
slippage
or
marks,
and
security
of
installation.
trael,
proper
rigging,
fre~play,
binding,
fOF
proper
lighting,
mounting,
proper
lubrication
and
proper
direction
of
E.
Inspect
compass
surface
movement
wW
relation
to
control
compensation, security
of
mounting, liquid
leakage
and
movement.
discoloration.
Swing
compass
at
annual
inspection
and after
any
new
equipment
has
been
installed.
CAUTION
Degaussing
tubular
strudure
may
be
necessary
if
All
flight
control
components
should
be
_
compass
will
not
compensate
within
100.
See
Mooney
inspected
to
verify
that
ad
moisture drain
holds
Service
Instruction
M20-95.
are
free
of obstructions.
F.
Inspect
alimeter
for
scale
error,
discolored
B.
Inspect
elevator
system
for
damage,
markings,
proper
pointer
readings,
setting
knob
lubrication,
rigging,
travel,
stop
adjustment,
,,,u,.,y,,
Oi
freedom
and
synchronization
of
barometric
scale
with
reference markers.
all
bearings, pivots,
bellcranks,
hinges
wear
on
G.
Inspect flight
panel
for
security
of
mounting,
downspring
eyes,
cable
pulley
and
finings,
security
of
mounting
and
proper
relation
to
control
movement.;
condition
of
shock
mounts,
freedom
from
interference
with
structure
and
condition
of
ground
straps.
C.
Inspect
aileron
system
for
damage, corro$ion,
H.
Insped
Avionics
Equipment
for
proper
operation
lubrication,
rigging,
travel,
stop
adjustment, conditi(ln
of
8
security.
hinges,
bellcranks,
pivots
and rod
end
bearings,llink
I.
Inspect
Avionics
Antennas,
wiring, shielding
for
bolt
security
and
proper
relation
to
control
movemeClt.
D.
Inspect
rudder
system
for
damage,
corro$ion,
ObViOUS
damage
or
defects.
lubrication,
rigging,
condition
of
hinges,
bellcra:nks,
J.
Inspect
pitot
head
for
port
obstruction;
inspect
lines
pivots
and
rod-end
bearings,
link bolt
security
iand
for
cracks,
dents, kinks,
proper
bend radius and
security
of
proper
relation
to
control
movement.
Check for
ifree
Bttachment.
Drain
system
and
insped
for
leaks.
movement
of toe-brake
pedals
and
proper
rudderiand
K´•
I"sped
static
ports
for
obstruction
and
nose
wheel travel.
aerodynamic
smoothness
at
port
installations.
Inspect
E.
inspect
stabilizer trim
control
system
for
secClrity
lines for
bends,
cracks,
dents,
kinks,
and
security
of
and
proper
adjustment,
shaft and
stop
nuts
forf,,
pt~0per
8ttachment.
Drain
system
and
inspect
for
leaks. Check
rigging
trim
control
wheel for smooth
operation,
altemate
static
pressure
source
located
on
flight
panel
unlve~al
joints
for
free-play
and
good
working
older,
fo’
freedom of valve
movement.
actuator
threads
for
lubrication,
linkage
for
conogion,
io.
ELECTRICAL
FUNCTIONAL
TEST.
and
guide
blocks
for looseness
or
excessive
wear.
ISee
A. Check
operation
of
navigation
lights.
SECTION 27-42-00 for Electric Trim
System
be~ring
B.
Check
operation
of
landing
8
taxi
lights.
maintenance.
C.
Check
operation
of
dome
lights
and
cigar lighter.
520-06
i
REV.
10-98
14
Island Enterprises