Trio Avionics Pro Pilot - Page 74

Trio Pro
P
You will
m
crank ar
m
movem
e
conditio
crank ar
The serv
control s
y
your par
t
The serv
existing
s
doublers
operatio
Trio Avio
In your i
n
neutral (
s
The serv
crank ar
m
If the s
c
Choose
a
control s
t
An over
-
result of
When in
system
f
Close is
qualified
When
s
installa
pre-ap
p
P
ilot Manual
4
m
ount the se
r
m
is at mid p
o
e
nt is availa
b
n can exist.
m hits its “s
t
o
crank arm
u
y
stem. The
p
t
icular install
a
o
must be m
o
s
upport. It is
and some ot
n. If you do
n
nics for guid
a
n
stallation, it
m
s
ervo center
p
o
crank arm i
m
in 90 degr
e
c
rews need t
o
mu
s
a
n operating
r
t
op) without
d
Note:
preser
v
arm m
o
travel
f
progra
chang
e
be cer
t
-
center condi
t
this is that y
o
stalling the s
e
f
lexing, airfra
m
IT IS CRITIC
not good en
o
technical co
u
s
hipped, the
c
t
ion of the cr
a
p
lied to the s
c
4
.1
r
vo and push
r
o
sition. That’
s
b
le within th
e
Also, assur
e
t
ops”.
u
ses a pushr
o
p
ushrod provi
d
a
tion.
o
unted on a
s
recommend
e
her additiona
n
ot have the
e
a
nce.
m
ay be more
p
osition) at +
/
s secured to
e
e increment
s
o
be remove
d
s
t be reapplie
d
r
adius on the
d
riving the se
r
It is importa
n
v
ed when m
o
o
unting by 1
8
f
or the servo
a
mmed to rev
e
e
s occur in th
t
ain the serv
o
t
ion will resul
t
o
u will lose al
e
rvo, ensure
t
m
e flexing, e
x
AL TO ENS
U
o
ugh in this c
a
u
nselor or ca
c
rank arm an
d
a
nk arm for e
a
c
rews accom
p
r
od so that th
s
it, aside fro
m
e
limits of th
e
e
that the ai
r
o
d terminate
d
d
ed in the in
s
s
olid platform
e
d that the se
r
l support. Ri
e
xperience r
e
convenient t
o
/
- 90 degrees
a flange by f
o
s
.
d
to repositio
n
d
(very spari
n
servo crank
r
vo crank ar
m
n
t to assure t
h
o
difying the c
r
8
0 degrees w
i
a
rm. In such
e
rse the driv
e
e first flight, t
o
direction of
t
OVER-C
E
t
in a comple
t
l
control of th
e
t
hat under a
n
x
treme turbul
e
U
RE NO PO
S
a
se. If you
h
ll Trio Avioni
c
d
screws are
a
ch particula
r
p
anying the
c
e control sur
f
m
carefully c
h
e
servo trav
e
r
craft contro
d
by rod end
b
s
tallation kit s
that will not
b
r
vo platform
n
g
idity of the
e
quired to fa
b
o
rotate the c
r
or 180 degr
e
o
ur machine
s
n
the crank a
r
n
gly) to preve
a
rm that allo
w
m
into its limit
s
h
at the prope
r
r
ank arm orie
n
i
ll essentially
a case the
P
e
signal. In th
e
he first chec
k
t
ravel is corr
e
E
NTER TE
S
t
e locking of t
e
airplane.
ny
flight condi
e
nce or any
o
S
SIBILITY T
H
OCCUR.
h
ave any qu
e
c
s for consult
a
not attached
r
installation.
rank arm.
f
ace is in a n
e
h
ecking that t
e
l range, an
d
l system hit
s
b
earings to li
n
hould be tri
m
b
uckle or “oil
c
n
ot be mount
e
servo mou
n
b
ricate the re
q
rank arm to
a
e
es from that
s
crews that c
a
r
m, after rep
o
nt loosening
w
s full elevat
o
s
. Most aircr
a
r
direction of
t
n
tation. Cha
n
reverse the
d
P
ro Pilot must
e
event unus
u
k
on the grou
n
e
ct.
S
TING
he control sy
s
i
tions, includi
n
o
ther abnorm
a
H
AT AN OVE
e
stions of do
u
a
tion.
to the servo.
The approp
r
e
utral positio
n
t
he required
d
that no “o
v
s
its “stops”
n
k the servo
a
m
med to the c
o
c
an” and atta
c
e
d to the airc
n
t is critical
t
q
uired brack
e
a
new orienta
t
as supplied
f
an be remov
e
o
sitioning, Lo
c
of the screw
s
o
r movement
a
ft get best p
e
t
ravel is
n
ging the cra
d
irection of
be
u
al pitch
n
d should be
s
tem during
o
n
g inverted fl
i
a
l flight condi
RCENTER
C
u
bts, please
c
This allows
r
iate Loctite c
n
when the s
e
range of co
n
v
er center”
before the
s
a
rm to the air
c
o
rrect length
c
hed to a fir
m
raft “skin” wit
h
t
o proper se
r
e
t please con
t
t
ion that will
g
f
rom the fact
o
e
d for indexi
n
c
tite Number
s
.
(control stop
e
rformance i
n
nk
to
o
peration. T
h
i
ght, control
tions,
C
ONDITION
C
c
onsult a
easy
ompound is
74
e
rvo
n
trol
s
ervo
c
raft
for
m
hout
r
vo
t
act
g
ive a
o
ry.
n
g the
222
to
n
the
h
e
C
AN