Mooney M20K - General; Wing Removal and Installation; Stall Strip Installation

MOONEY
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
5790-00
GENERAL
57-00-01
-WING
REMOVAL
AND
INSTALLATION
The
all
metal
wing
is
a
one
piece
assembly
attached
to
Major
subassemblies
of
wing
may
be
removed
the
fuselage
at
structural
hard
points
with
strudural
individually,
or
wing
may
be
removed
as
a
unit.
To
hardware.
(See
section
53-40-01).
The
full
span
main
remove
a
wing,
a
fuselage
supporting
cradle
needed.
spat
assembly
is
connected
to
the
stub
spar
and
rear
1.
Wing
removal:
spar
assembly
by
ribs,
doublers
and
skins.
The
main
landing
gear
forward
attach
assembly
is
an
integral
part
A.
Remove
wing-root
fairings
and bottom
fuselage
of
the
main
spar
and
the
rear
fitting
is
bolted
to
the
stub
access
panels.
spar
assembly.
The
spar
caps
are
7075-16
aluminum
B.
Drain
all
fuel
from
tanks.
and
webs,
ribs
and
doublers are
2024-T3,
T4
or
T42
C.
Drain
brake
lines
and
reservoir.
Disconnect
aluminum.
Repair
of
these
components
is
covered
in
hydraulic
lines
at
wing
main
spar.
Section
51-13-00.
D.
Remove
front
and
rear
seats.
Remove
two
The
wing
tips
are
fabn’cated
from
fiberglass
and
house
inspection
plates
under
rear
seat
area.
navigation
and
strobe
lights.
E.
Jack
aircraft
per
Chapter
7-10-00.
The
fuel
is
contained
in
wet
wing
type
fuel
cells
between
main
spar
and
baffles
forward
of
spar.
The
F.
Attach
A-frame
hoist
to
propeller,
or
support
with
tanks
are
sealed
dun’ng
manufacturing
with
current
a
propellerjack.
technology
sealant.
(See
Section
28
for
fuel
system
details).
sn
TABLE
FMI
LENGTHS
)F
~Y;o.
wn
B3SULL
SHI~CS
BEPYIW
SHEAR
loll
usHa
US)
NOT
UNDER
BOLT
HEAD OR
NUT.
319139-3
t
WQJ21
ANC~
BOLT
(4)
510131-9
~ns6M1Q
W3Q-~
AW96M1Q
)W#F~
AN960-S16
WASHER
J1O1JCU
UC(-CA
ANWD´•S1Q
IW18-)2~
AW6S-428
NUT
(4)
310131-11
UI(-(A
O
CTYPICK
~QR1
SIIiES-ACCESSIBLE
INSIDE
Auull
vlrs-lal
SHUR
U16-)6A, BOLTJ1UJ)AN~-1‘IA
BoLT
O)-
AcCFlWWF
THRu
~HIEn´•
ANs6O-6l6
WASHER
WELL
AI363-634
NUT
AN960-S16
WASHER
(3)
IloOOl-3
OR
-5
SPACER
(43)
NUT
(2)--
~IYP1CU
BOTH
SDES--
ACCESSIBLE
INSIDE
CAB~N)
ACCESSIBLE
~NSIDE
CABIN
BOL1
(I1--KMSSIBLE
O
CMYCU
BOTH
SIDES)
INSIDE
CABIN
Ai960o-16a
AN9S0-S16
WASHER
(5)~
AUs3-436
NUT
(5)--CCESSSBLE
RY
fbP
WNC
FURING
(NPlCAL
BOTH
SDES)
ca~
E~g
I
XY(PIEWUE
AN4-17A--
ACCESSIBLE
UNDER
WAR
WATS
ANB6PJ16
WASHER
(2)
I
39-33
AN36S-428
NUT
(2)-
ACCESSIBLE’THRU
WING
BOTTOLI
ACCESS
PWL;
SHIY
AS
NECESS~RY
W-4A
BOLT-ACCESSIBLE
By
WLKI~NG
U37H-17A
BOLT-ACCESSIBLE
THROUGH
ACCESS
TOP
WINC
FURW;
CO~R
UNDER
REAR
SEAT.
SAFRY
WIRE
BOLT
HEAD
AN060-1O
WASHER~(8)
TO
AnIYCENT
SPAR-~MB
SI~FFEWR
AN363-1633
NIII
(8)
ACCESSIBLE
THROUGH
ANObD-T1Q
WASHER
WHmrmL
(TYPICAL
BOTH
SDES)
CMPICK
BOTH
SIDES)
WING
ATTACHING
HARDWARE
FIGURE
57
1
57-00-00
OLDWILLWAYNE