Piper SENECA III - Page 367

PIPER
AIRCRAFT CORPORATION SECTION 9
PA-34-220T,
SENECA
III
SUPPLEMENT
18
SECTION 4
-
NORMAL
PROCEDURES
(a)
NORMAL
OPERATING PROCEDURES
NOTE
This
autopilot is
equipped with
an
A; P
"OFF"
warning
horn
that will sound
for
approxi-
mately
4
seconds
anytime
the
autopilot
is
disengaged.
This
will
be
accompainied
by
an
"A/ P"
message
flash
on
the
autopilot
remote
annunciator
for
approximately
5
seconds.
The horn
may
be
silenced before the
4
second
time
limit
is
up
by:
(1)
Pressing "T"
bar
atop
command
trim
switch,
(2)
by
re-engaging the
autopilot.
NOTE
If this
autopilot
is equipped
with
a
Flight
Director
steering horizon
the F/
D
must
be
switched
on
before
the
autopilot
may
be
engaged.
Any
autopilot mode
may
be
pre-
selected
and
will
be
retained
upon
autopilot
engagement,
CAUTIONS
Flight
Director Autopilot
versions
only
are
equipped
with
a
remote
go-around
switch.
When
G A mode
is
selected
the
AUTOPILOT
WILI
DISCONNECT
and
warning
horn will
sound.
Pilot
may
use
Flight Director
steering
for
missed approach
guidance. After
aircraft
is
stabilized
in
a
proper
climb
with
gear
and
flaps
up,
the
autopilot
may
be
re-engaged
and will
retain
G/
A
mode.
Autopilot only
(no
Flight
Director)
versions
do
not
have
a
G/ A
switch.
If glide
slope
coupling
is
not
desired
while
operating
on
the
localizer
use
NAV
or
REV
mode
instead
of
APPR mode.
ISSUED:
APRIL
21,
1981
REPORT:
VB-1110
5
of
12,
9-117
i