Mooney M20K - Ailerons; Aileron Removal and Installation

SERVICE AND
MAINTENANCE
MANUAL
M20K
MOONN
AIRCRAFT
CORPORATION
The
flap
actuatorjack
shaft
is
connected
by
a
push-pull
Refer
to
Section
27-10-00
for
maintenance
and
n’gging
rod
end
bean’ng
to
actuator
bracket
(1)
(Figure
57-6)
procedures.
located
just
inboard
of inboard
hinge
(2).
The
ailerons
are
of
all metal
construction.
The
main
All three
hinges (2)
and
(3)
are
faired
(4)
to
reduce
spar
(1), (Figure 57-7),
is attached
to
the
rear
spar
(2)
drag
(excluding
231 Lean
Machines).
through
n’bs
(3).
These
components
are
n’veted
together
and
a
top
and
bottom
skin
(4)
and
(5)
riveted
The internal
structure
of
flaps
consists
of
a
leading
to
this
sub-assembly.
To
complete
control
surface,
edge
extrusion
(5), trailing
edge
stiffener
(8),
n’bs
O
hinges
(6)
and
balance
weights
O
are
installed.
The
and
top
and bottom skins
(8).
These
components
are
weights
O
are
bolted
bolted
(10)
through
an
outboard
riveted
together
into
a
left
hand
and
n’ght
hand
rib
(8)
and
bracket
(9)
on
each
aileron
assembly.
assembly.
5730-21
AILERON
REMOVAL
AND
57-50-11
FLAP
REMOVAL
AND
INSTALLATION
INSTALLATION
Refer
to
Section
27-50-00
for
removal and
installation
Refer
to
Section
27-10-00 for
removal,
installation
8
procedures.
balancing
procedures.
5750-20
-AILERONS
3
3
6~
5
~P
1
~2
4
1
~e
oP
3J
gC
6
DETAIL
A
3
7~-CI
1
o"1r
91
8
6
DETAIL
B
DETAIL
C
SMX57-7
AILERON
ASSEMBLY
FIGURE
57
7
57-50-11
OLDWILLWAYNE