Raytheon Anschütz Pilotstar D, Manual

Page: 93 / 166

Autopilot
PILOTST
A
R
D
2-
-5
1
Edition:
March
13,
2009
3060.DOC012
No.
Indication
Signification
Possible
C
ause
Effects
o
n
O
peration
Measures
1
AUT
O
FA
IL
Internal
disturbance
in
the
PILOTST
A
R
D
system.
W
ith
a
C
entral
A
larm
System
the
relay
output
’AUT
O
FAIL
’is
summarised
in
acoustical
and
optical
alarms.

Program
trouble

CPU
P
CB
disturbed
or
defective
see
C
entral
A
larm
S
ystem
System
is
no
longer
ready
for
opera-
tion. see
C
entral
A
larm
System

Switch
off/on
the
system
via
the
steering
mode
selector

Set
the
steering
mode
selector
to
position
HAND

Check
the
LED
display
on
the
CPU
P
CB
(see
Chapter
3.4)

Exch
an
ge
th
e
C
PU
PCB
(see
Chapter
3.3.3)

see
C
entral
A
larm
S
ystem
section
1.6.3
2
PA
N
E
L
FA
IL
Operator
unit
not
operating
faultlessly
.

Connecting
cable
brok
en

Supply
voltage
failure
operator
unit

Operator
unit
defective
System
is
no
longer
ready
for
opera-
tion.

Set
the
steering
mode
selector
to
position
HAND

Check
the
LED
display
on
the
CPU
P
CB
(see
Chapter
3.4)

Check
connecting
cable

Check
supply
voltage

Exchange
operator
unit
3
GYRO
FA
IL
Gyro
data
transmission
is
not
plausible. Gyro
in
settling
m
ode
Gyro
in
heating
m
ode
Gyro
’F
ollow
U
p’
disturbed
Gyro
heading
failure

Connecting
cable
brok
en,
GY
R
O
de
fe
ct
iv
e

(in
case
of
step
system)
W
ith
a
short
---
time
ship’s
mains
failure,
the
synchronization
value
gets
lost
System
readiness
for
operation
is
conditional. T
he
last
heading
is
automatically
stored,
the
set
heading
is
caused
to
follow
up.
Autopilot
M
AN
Mode
possible,
Autopilot
A
UT
O
M
ode
not
possible

Select
the
m
agnetic
or
fluxgate
compass
via
the
operator
unit

Check
connecting
cable

Check
G
YRO/Operational
condition

Check
synchronization;
adj
ust,
if
required
(see
Chapter
2.3.5)
4
MAGNET
FA
IL
Magnetic/fluxgate
data
trans-
mission
is
not
plausible.

Connecting
cable
brok
en,
ma
gnetic/fluxga
te
compa
ss
defective

Sonde
operation
is
disturbed

Coursebus
(M
agnet
information
not
available)
System
readiness
for
operation
is
conditional. T
he
last
heading
is
automatically
stored,
the
set
heading
is
caused
to
follow
up.

Set
the
steering
mode
selector
to
position
HAND

Select
the
gyro
compass
via
the
operator
unit

Check
the
connecting
cable

Check
the
magnetic/fluxgate
compass