Mooney M20B - Wing Component Installation

6.
Rudder
tubes
(7244).
7.
Elevator Tube
(7243).
8.
Elevator
andRu~lder
3rd Link
(7101)
(two
tubes).
9.
Remove
floorboard braces
(3937-9,
3937-10,
3937-113.
10.
Seat
Rail
Bracket
(3939-7,
3939-8 Six
bolts) (3941
two
bolts).
11.
Stringer
assembly
doubler
(3977-1).
.12.
Fourteen
bolts
from "Z"
rail.
13.
Sixteen
Attach bolts
iAN
3-5A).
14. Gas
lines
and
wires
from
wing
root.
15.
Airs_need
indicator
line,
Pitot
lines,
heated
pitot
lines
if
used.
16.
Front
mating
bolts
(two
AN
6-16A).
17.
Rear
mating (two_
AN
P15A and
two
AN
P17A).
18.
tension’
Bolts
(7H-16A).
NOTE:
Have suitable
cradle
ready
for
fuselage
before
last three
steps
of.wing
removal.
2.~
REMOVAL
OF
WING
FLAP
a
Remove
wing
flap
cover
plate
at
wing
root
(7274).
b.
Disconnect
the
flap
actuating
link
(7100).
c.
´•Remove..bir,ge
bolts
(4).
d.
Pull the
flap
straight
back ofT
the
wing.
3.
REMOVAL.OFAILERON
a.
Disconnect
the
Aileron
control tube
(7241)
at
the inboard
aileron
hinge
(2177
or
2178).
b.
Remove
three
hinge
bolts.
c.
Pull
the
aileron
straight’off
the
wing.
C.
INSTALLATION
OF
WING
COMPONENTS
1.
I~nstallation’of
Wing.
Installation of the
wing
asserhbly
is
a
direct
reversal of removal.
2..
Installation
of
Flap.
Installation
of
the
nap assembly
is
a
direct
reversal
of
removal.
3.
Installation
of
Aileron.
Installation
of Aileron
assembly
is
a
direct reversal
of
removal.
j
.~_.._.
OLDWILLWAYNE