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Mooney M20K - Page 244

Mooney M20K
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MOONEY
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
The
bottom
attach
point
(4)
(Figure
53-5)
on
the
articulated
hinge
assembly
(2)
(Figure
53-6)
attached
empennage
assembly
secures
stabilizer
trim
jack
to
rear
bulkhead
(3)
(Figure
53-6)
of
tailcone.
The
screw
(5)
(Figure
53-5)
and
(4)
(Figure
53-6).
Lateral
hinge
attach
pin
(6)
(Figure
535)
is
held
in
place
with
stability
of
empennage
assembly
is
controlled
with
an
a
cotter
pin
at
each
end.
sns3-s
EMPENNAGE
ASSEMBLY
ATTACH
FITTINGS
FIGURE
53
5
53-40-02
OLDWILLWAYNE

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