Mooney M20R - Jack Points; Stall Strip Installation

SERVICE
AND
MAINTENANCE
MANUAL
M20R
MOONEY
AIRCRAFT
CORPORATION
(e)
Rudder
control
tubes.
flies
to
criteria
in
paragraph
57-00-02,
1,A,
B
and
C.
Se-
lf)
Elevator
control
tube.
cure
stall
strip
per
installation
instructions
in
Figure
57-2.
(0)
Elevator
and
rudder
push-pull
tubes.
57-10-00
MAIN
FRAME
(h)
Flap
control
linkages.
(i)
Floorboards
at
rear
attach
points.
The
integral
fuel
cells,
shaded
area
(1)
start
at
wing
sta-
tion
24.5
and
continue
to
rib,
station
88.75
(LH/RH)
on
(j)
Belly
skin
stringer
splice
angles.
wing.
(Figure
57-3).
Sealer
is
applied
to
all
joints
on
ribs,
(k)
Airspeed
indicator
line,
pitot
lines
and
ipitot
spar
and
baffle
plates.
(See
Section
28-11-00
for
reseal-
heater
wires
(if
installed).
ing
procedures).
(I)
Electrical
connections
for: The
wing
is
manufactured
in
three
sections;
center
sec-
Nav/Strobe
Lights;
Fuel
Qty.
system;
Speedbrak$s
8
tion
(2),
left
outboard
section
(3)
and
an
opposite
right
TKS
system
if
installed
outboard
section
(not
shown)
(Figure
57-3).
These
three
(m)
Hardware
shown
in
(Figure
57-1).
sections
are
then
assembled
into
one
full
span
wing
as-
sembly
as
final
two,
LH/RH,
skins
are
installed.
CAUTION
LH
8
RH
spares
configuration,
wing
tip
assembly,
are
Have
suitable
cradle
ready
to
carry
fuselage
beifore
available.
Each
includes
completed
section,
from
Wing
removing
all
mating
hardware.
Station
103.50
and
outboard.
The
assembly
includes
stringers
(4)
required
to
complete
splice
to
old
center
2.
W~ng
installation:
Installation
of
the
wing
assehnbly
section.
A
spar
splice
plate
is
required
to
reinforce
spar
I
is
direct
reversal
of
removal.
Center.(5)
at
it’s attachment
location.
These
components,wah
3.
Verify
rigging
of
all
flight
controls
per
SECTION
i27.
instructions,
are
available
through
any
Mooney
Service
57-00-02
STALL
STRIP
INSTALLATION
57-20-00
AUXILIARY
STRUCTURES
1.
Position
stall
strips
on
wing
leading
edge
so
that,
during
stall
recovery,
normal
use
of
flight
controls
s~ould
57-20-01
JACK
POINTS
prevent:
A. More
than
15"
roll.
Wing
jack points
are
located
on
LH
8
RH
lowerwing.
The
threaded
wing
tie
down
eyebolt
fittings
are
designed
to
B.
More
than
150
yaw.
accept
non-threaded
jack
points.
These are
located
out-
C.
More
than
300
pitch
below
flight
level.
board of
each
main
gear.
The
nose
jack
point
is
located
2.
Place
stall
strips
on
leading edge
at
stations
shown
aft
of left
hand
cowl
flap
at
Pus.
Sta.
-5.51. See
SECTION
on
Figure
57-2,
attach
securely
with
duct
tape
fol
test
7-10-00
for
complete
jacking
procedures.
flights.
Reposition
stall
strips,
up
or
down,
until
ai~raft
LEFT
WING
SHOWN
RIGHT
WING
OPPOSITE
j
j
I
W
SKIN
,V~ii
icSTA
60,1e
,06/,10
DEEPC’BORE
,406
SKIN
STALL
STRIP
kSTA
43.5
DRILL
,189/,193
DIA,
RIB
RIVET
LINE
AN515-bR10
USE
A6-75
RIVNUf
SCREW
USE
LOCKTITE
LYPE
CV
FMID
A
AN520-6-7
SCREW
AN345-6
NUT
A
MID
AN960-6
WASHER STALL
STRIP
TYF~CAL
I[MSn
ALTERNATE
PI~STC
SMM57-2
STALL
STRIP
INSTALLATION
-FIGURE
57-2
57-00-02
´•REV.10-98
Island Enterprises