Mooney M20K - Plates;Skins; Flight Surfaces; Flaps; Flap Removal and Installation

MOONEl
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
5730-00
-PLATES-SKIN
plumbing
and
control
bellcranks
enclosed
within
wing.
They
are
flush
mounted covers
and when
installed
Wing
access
and
inspection
covers
shown
in
(Figure
continue
the
aerodynamic
contour
of
wing.
575)
provide
maintenance
access
to
components,
LEGEND
FOR
FIGURE
57-5.
1.
Wing
skin
.050
thickness
(Fuel
Tank).
11.
OAT
probe,
n~ght
wing
only.
2.
Wing
skin
.040
thickness
(Fuel
Tank).
12.
Control
tube
guide
blocks
and
flight
timer.
3.
Wing
skin
.040
thickness.
13.
Pitot
post
left
wing
only.
4.
Wing
skin
.032
thickness.
14.
Strobe
light
power
supply.
5.
Wing
skin
.025
thickness.
15.
Aileron
bellcrank
and
control
rods.
6.
Wing
skin
.025
thickness.
16.
Auto
pilot
servos.
7.
Fuel
tank
access.
17.
Gym
compass
flux
valve
tone
of
these,
depending
on
installed
equipment),
(left
wing
only).
8.
Fuel
tank
filler.
18.
Main
landing
gerar
retraction
spring.
9.
Control
tube
guide
blocks.
19.
Elevator
and
rudder
controls
rod
end
bean’ngs,
10.
Wing
fuselage
attach
points,
bellcranks.
NOTE
5750-00
FUGHT
SURFACES
Access
covers
on
bottom
of
wing
that
require
Refer
to
Section
27-90-00
for
flight
control
surface’s
removal
for
inspection
intervals are
secured
with
screws.
Any
access
covers
that
are
riveted
balancing
procedures.
in
place
are
required
for
manufacturing
only
and
NOT
for
routine
inspections.
5750-1
0
FLAPS
Refer
to
Section
27-50-00
for
maintenance
and
rigging
57-40-00
-A~TACHFITnNGS
procedures.
Refer
to
Section
57-00-01
for
wing
fuselage
attachment.
4
8
76
FLAP
ASSEMBLY
FIGURE
57
6
57-30-00
OLDWILLWAYNE