Then,
very
and
cente
edge
of
th
wing
as
clo
so
you
can
Then,
afte
the
cover
NOTE:
In
s
surface
of
wing
to
th
the
fit
of
s
cyanoacry
secure
the
installatio
Next,
sele
center
on
existing
ho
SHARP
NO
CAREFULL
THE
Z
‐
BEN
holes
mor
resulting
i
flight.
Of
c
holes
(the
y
carefully
er
the
cove
he
wing
and
osely
as
po
n
possibly
r
er
confirmin
to
the
win
some
cases
f
the
wing.
he
fuselage
some
parts
ylate
(CA)
g
e
edges.
Ke
n
of
the
wi
ct
a
two
‐
si
either
side
oles
in
the
O.11
BLADE
LY
ENLARG
NDS
CAN
P
re
than
nec
in
‘slop/pla
course
it’s
e
pushrods
line
up
the
r
before
pr
d
slowly
pr
ossible
unti
remove
an
ng
the
fit
a
g.
s
it
may
no
This
is
not
e
will
help
h
s
it
may
be
glue
(we
re
eep
in
mind
ing
cover.
ded
servo
e.
Check
to
servo
arm
E,
OR
A
PIN
GE
THE
HOL
PASS
THRO
cessary
oth
ay’
that
ma
also
impo
s
should
rot
e
trailing
ed
ressing
it
do
ress
the
cov
il
you
reach
d
reinstall
and
alignme
ot
be
possib
typically
a
hold
the
ed
helpful
to
commend
d
that
the
u
arm
that
h
o
see
if
the
.
If
not
USE
N
VISE/DRI
LES
IN
THE
UGH
THEM
herwise
th
ay
make
it
rtant
that
tate
freely
9
dge
of
the
c
own
agains
ver
down
w
h
the
leadi
the
cover
i
ent
are
goo
ble
for
all
e
problem
a
dges
of
the
apply
tran
Medium/G
use
of
glue
has
holes
at
‘Z
‐
bends’
o
E
EXTREME
ILL
WITH
A
POSITION
M.
It’s
very
e
pushrod
difficult
to
the
pushro
y
but
witho
cover
with
st
the
wing
with
light
p
ng
(front)
e
if
the
fit/al
od,
apply
m
edges
of
the
as
the
rubb
cover
in
p
sparent
‘pa
Gap
‐
Filling
will
result
t
least
7/16
of
the
push
E
CARE
AN
A
3/64”
(1.2
S
YOU
PLA
y
important
s
will
be
to
o
properly
ods
are
not
out
slop/pl
the
trailin
g
panels.
St
pressure
so
edge.
Apply
ignment
is
more
press
e
cover
to
ber
bands
u
lace.
Howe
acking’
tap
or
Thick
vi
in
a
more
6”–1/2”
(11
hrods
fit/pa
D
A
HOBBY
2mm)
DRIL
AN
TO
USE
t
that
you
oo
loose
in
trim
and
c
t
installed
ay).
g
edge
of
t
tart
from
th
o
it
fits
agai
y
only
light
s
not
correc
ure
to
bett
fit
flush
ag
used
to
atta
ever,
depen
pe
and/or
scosity)
to
‘permanen
1–13mm)
f
ass
through
Y
KNIFE
W
LL
BIT,
TO
V
JUST
ENOU
DO
NOT
en
n
the
holes
control
the
too
tightly
the
wing
he
trailing
nst
the
t
pressure
ct.
ter
secure
gainst
the
ach
the
nding
on
better
nt’
from
the
h
the
ITH
A
VERY
UGH
SO
nlarge
the
potentiall
e
ailerons
in
y
in
the
y
n
