Mooney M20K - Elevator; Elevator - Removal

SERVICE
AND
MAINTENANCE
MANUAL
M20K
MOONC/
AIRCRAFT
CORPORATION
55-10-02
HORIZONTAL
STABILIZER
The elevator
control
hom
(2)
is connected
to
inboard
INSTALLATION
leading edge
of each elevator
(R.H.
and
L.H~.
Both
control
hems
are
then
connected
to
elevator
flight
Refer
to
Section
53-40-02
for
installation.
control
bellcrank.
The full
length
trim
tab
(3)
may
not
be
55-20-00
-ELEVATOR
re-adjusted
from
factory
installed
configuration.
This is
factory
set
at
70
down.
The
elevators
on
the M20K
consist of
a
left
and
n’ght
The
elevator
skins
(4)
are
stretch
formed
for
upper
and
hand
assembly
attached
through
ball
bean’ng fttings
lower
surface
of
elevator.
There
are no
ribs
in the
(1)
to
rear
spar
of
the horizontal
stabilizer
(reference
elevator
between
inboard
and
outboard
ribs.
Figure 55-2).
7 1 i r4
3
6
1-
5
2
e~
1
DETAIL
A
Al:
ELEVATOR
FIGURE
55 -2
The
skins
are
attached
to
leading
edge
e~drusion
(5)
55-20-01
-ELEVATOR-REMOVAL
and
n’bs
(6)
with
blind n’vets.
Each
formed
corrogation
Remove
AN3
bolts
from
each
control
horn
and
is
matched
on
top
and
bottom
skins
and rivets
are
push-pull
tube
bean’ng,
then
remove
AN3
bolts
and
installed
for
strength
and
n’gidity through
each
hardware
from
each
hinge
fitting
on
both
elevators.
corrogation.
A
lead
balance
weight O
is
installed
in each elevator
55-20-02
ELRIATOR
INsTAUATION
tip
with
iron
n’vets
(8).
(Reference
Figure 55-2).
See
CAUTION
Section
27-91-00
for
balancing
procedures
on
the
Each
new,
repaired
or
repainted
elevator
elevators.
should
be
checked
for
balance
per
Section
27-91-00.
The elevators
are
installed
in
reverse
order
of removal.
Nominal
torque
values
for
AN3
bolts
are
to
be
used
(see
section
5-20-01 for
torque
table.)
55-1
0-02
OLDWILLWAYNE