Trio Avionics Pro Pilot - Page 78

Trio Pro
P
The serv
force - th
Engage
t
operate i
train. Th
end wre
n
be diffic
u
When se
servo di
s
extremel
y
change i
n
mitigate
t
should t
h
operatio
n
1.
P
pressure
elevator
s
position
a
2.
P
trim con
d
HOLD m
should b
e
seconds,
3. I
f
then the
point wh
e
4.
T
level tha
t
obtained
ensure a
is discon
Adjust
m
A
fter ins
t
“one tim
e
never ha
v
settings
t
N
t
o
s


P
ilot Manual
4
o
Torque Co
n
e force you
w
t
he servo by
p
nside the ser
v
en push the
c
n
ch set the o
v
lt to override
tting servo fo
s
connect in a
y
pitch sensit
n
pitch attitu
d
t
his risk it is r
e
h
en be condu
c
n
al airspeeds
P
rior to flight,
of about 2 lb
s
o that there
a
nd engage t
h
P
erform a lo
w
d
ition and the
n
ode, the airc
r
e
observed f
o
the pilot sho
f
the CLUTC
H
c
lutch force
s
e
re the aircra
f
T
he objective
t
will not cau
s
at the low fli
g
release at a
n
nected with
a
m
ent of Serv
o
t
allation wirin
g
e
" setting tha
t
v
e to be cha
n
t
o the factory
N
OTE: This i
o
the servo
m
s
ystem is eng

The
V
N
A
control el
e

The H N
A
trim error
4
.1
n
trol nut (the
a
w
ill feel at the
p
ressing the
a
v
o housing a
n
c
ontrol stick
h
v
erride force
t
with the con
t
rce override
a
moderate to
e
ive. A servo
e and in extr
e
e
commende
d
c
ted to deter
m
.
A recomme
n
using a sprin
s results in a
is no initial lo
h
e servo in t
h
w
speed flight
n
the servo e
r
aft should b
e
o
r a CLUTCH
uld disconne
c
H
SLIP mess
s
hould be red
f
t excursion
a
of this test is
s
e an excessi
v
g
ht speed, te
s
n
y operation
a
a
n out-of-trim
o
Rotation D
g
is complete
t
must be acc
n
ged unless
y
defaults.
s a CRITICA
m
otor is not c
o
aged.
AV
servo is s
e
e
ctronics.
AV
servo will
b
compensatio
a
djustment n
stick when t
h
a
ppropriate
H
n
d the servo
h
ard enough
t
t
o a value tha
t
rol stick.
W
a
djustment o
n
e
xtreme out-
o
disconnect
w
e
me cases it
d
that the clut
c
m
ine an appr
o
n
ded adjust
m
g scale on th
clutch slip.
O
ad force on t
h
h
e ALTITUD
E
test. During
ngaged in th
e
e
slightly mis-
t
SLIP messa
c
t the servo
w
age does no
t
uced and the
a
t release is
n
to have a C
L
v
e pitch excu
s
ting should
b
a
l airspeed wi
l
condition.
irection
the system
s
omplished w
h
y
ou replace a
L setting and
o
rrect the air
c
e
lf centering
d
b
e centered
m
n.
ut inside the
s
h
e servo clut
c
H
NA
V
or
V
N
A
c
rank arm sh
t
o override th
e
t will give go
o
W
ARNIN
G
n
the pitch s
e
o
f-trim condit
i
w
hile in an ou
t
is possible t
o
c
h be set at
a
o
priate adjus
t
m
ent scenario
e control stic
k
O
n some airc
r
h
e servo. To
E
HOLD mod
e
this test the
a
e
A
LTITUDE
t
rimmed. W
h
ge. If no CL
U
w
hile maintai
n
t
appear and
t
test re-run u
n
ot excessive
.
L
UTCH SLIP
rsion when t
h
b
e accomplis
h
l
l not result i
n
s
ervo directio
n
h
ile the aircr
a
control head
MUST be v
e
c
raft will be fo
d
ue to the abi
l
m
anually in t
h
s
ervo on the
c
h begins to
s
A
V switch.
Y
ould becom
e
e
servo. Usi
n
o
d control au
t
G
e
rvo, be awar
e
i
on. Newer, l
t
of trim condi
o
cause struc
t
a
very low for
c
t
ment point f
o
is as follows
:
k
, set the clu
t
raft it may be
do this, plac
e
e
.
a
ircraft shoul
d
HOLD mode
h
ile in this co
n
U
TCH SLIP
m
n
ing manual
p
the pitch exc
u
ntil the CLU
T
.
message oc
c
h
e servo is re
h
ed at progr
e
n
a significant
n
check mus
t
a
ft is on the g
r
, or perform
a
e
rified before
f
rced into a di
lity to provid
e
h
e steps belo
w
output shaft)
s
lip.
Y
ou should h
e
e
firmly held i
n
n
g an 11/16 “
t
hority, but n
o
e
of the cons
e
ight aircraft
d
i
tion could re
s
t
ural damage
ce level initia
o
r your partic
u
:
t
ch force so t
h
necessary t
o
e
the elevato
r
d
be placed i
n
. While in th
e
n
dition the au
t
m
essage app
p
itch control
d
u
rsion is exc
e
T
CH SLIP m
e
c
ur at a serv
o
leased. Onc
e
e
ssively high
e
pitch excurs
i
t
be accompli
r
ound. Once
a
“default res
e
flight. If the
c
i
vergent man
e
e
its angular
p
w
to facilitate
sets the ove
r
e
ar the solen
o
n
place by th
e
or 17mm op
e
o
t so strong a
e
quence of a
d
esigns can b
s
ult in an abr
u
. In order to
lly. Flight te
s
u
lar aircraft a
t
h
at a stick
o
balance the
r
in a flight n
e
n
a neutral pi
t
e
ALTITUDE
t
opilot displa
y
ears after 15
d
uring the rel
e
e
ssive on rel
e
e
ssage occur
s
o
force overri
d
e
this setting
e
r flight spee
d
i
on when the
shed. This i
s
done, it sho
u
e
t” that retur
n
c
ommand dir
e
e
uver when t
h
p
osition back
the automati
c
78
r
ride
o
id
e
gear
e
n
s to
pitch
e
u
pt
s
ting
t
the
e
utral
t
ch
y
e
ase.
e
ase,
s
at a
d
e
is
d
s to
servo
s
a
u
ld
n
s all
e
ction
h
e
to the
c
roll